Note
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Bi-level BCD-based MDO on the Sobieski SSBJ test case#
Note
As described in Bi-level Block Coordinate Descent (Bi-level BCD), there are several variants of the bi-level BCD formulation; this example shows the implementation of the bi-level BCD-MDF (BL-BCD-MDF). For more details about other variants please refer to [DGR24].
from __future__ import annotations
from copy import deepcopy
from gemseo import configuration
from gemseo import execute_post
from gemseo.problems.mdo.sobieski.core.design_space import SobieskiDesignSpace
from gemseo.problems.mdo.sobieski.disciplines import SobieskiAerodynamics
from gemseo.problems.mdo.sobieski.disciplines import SobieskiMission
from gemseo.problems.mdo.sobieski.disciplines import SobieskiPropulsion
from gemseo.problems.mdo.sobieski.disciplines import SobieskiStructure
from gemseo.scenarios.mdo_scenario import MDOScenario
from gemseo.settings.formulations import BiLevel_BCD_Settings
from gemseo.settings.formulations import MDF_Settings
from gemseo.settings.mda import MDAGaussSeidel_Settings
from gemseo.settings.opt import NLOPT_COBYLA_Settings
from gemseo.settings.opt import SLSQP_Settings
configuration.enable_discipline_statistics = True
Instantiate the disciplines#
First, we instantiate the four disciplines of the use case:
SobieskiPropulsion,
SobieskiAerodynamics,
SobieskiMission
and SobieskiStructure.
propulsion_disc = SobieskiPropulsion()
aerodynamics_disc = SobieskiAerodynamics()
structure_disc = SobieskiStructure()
mission_disc = SobieskiMission()
Since they are going to be our disciplines for the sub-scenarios, we'll call them sub-disciplines.
sub_disciplines = [structure_disc, propulsion_disc, aerodynamics_disc, mission_disc]
Build the scenario#
We build the scenario that allows to create the optimization problem from
the disciplines and the formulation.
Here, we use the BiLevelBCD formulation.
We need to define the design space.
design_space = SobieskiDesignSpace()
For this formulation, we need to define the optimization sub-scenarios from all sub-disciplines coupled together. Each sub-scenario optimizes its own design variable according to the corresponding constraint and the objective y_4 (range) which we are maximizing.
Define Sub-scenario settings model#
The setting for all sub-scenarios is the same, so we can define a global, settings model to be used by each sub-scenario.
sub_scenario_settings = MDF_Settings(
main_mda_name="MDAGaussSeidel",
)
sc_algo_settings = SLSQP_Settings(max_iter=50)
Build the Propulsion Sub-scenario#
This sub-scenario will optimize the propulsion's discipline design variable x_3 under the constraint g_3.
propulsion_sc = MDOScenario(
sub_disciplines,
"y_4",
design_space.filter(["x_3"], copy=True),
formulation_settings_model=sub_scenario_settings,
maximize_objective=True,
name="PropulsionScenario",
)
propulsion_sc.set_algorithm(algo_settings_model=sc_algo_settings)
propulsion_sc.formulation.optimization_problem.objective *= 0.001
propulsion_sc.add_constraint("g_3", constraint_type="ineq")
Build the Aerodynamics Sub-scenario#
This sub-scenario will optimize the aerodynamics' discipline design variable x_2 under the constraint g_2.
aerodynamics_sc = MDOScenario(
sub_disciplines,
"y_4",
design_space.filter(["x_2"], copy=True),
formulation_settings_model=sub_scenario_settings,
maximize_objective=True,
name="AerodynamicsScenario",
)
aerodynamics_sc.set_algorithm(algo_settings_model=sc_algo_settings)
aerodynamics_sc.formulation.optimization_problem.objective *= 0.001
aerodynamics_sc.add_constraint("g_2", constraint_type="ineq")
Build the Structure Sub-scenario#
This sub-scenario will optimize the structure's discipline design variable x_1 under the constraint g_1.
structure_sc = MDOScenario(
sub_disciplines,
"y_4",
design_space.filter(["x_1"], copy=True),
formulation_settings_model=sub_scenario_settings,
maximize_objective=True,
name="StructureScenario",
)
structure_sc.set_algorithm(algo_settings_model=sc_algo_settings)
structure_sc.formulation.optimization_problem.objective *= 0.001
structure_sc.add_constraint("g_1", constraint_type="ineq")
System's Scenario Settings#
The bi-level BCD formulation allows to independently define the settings for the BCD MDA, such as shown below.
bcd_mda_settings = MDAGaussSeidel_Settings(tolerance=1e-5, max_mda_iter=10)
Then, you may pass the BCD MDA settings directly to the formulation settings.
Since the system constraints are the same as the constraints that have already been
applied to the sub-scenarios, we set apply_cstr_tosub_scenarios=False to avoid
adding the same constraints twice on the lower level.
system_settings = BiLevel_BCD_Settings(
bcd_mda_settings=bcd_mda_settings,
apply_cstr_tosub_scenarios=False,
)
Tip
When running bi-level scenarios, it is interesting to access the optimization
history of the sub-scenarios for each system iteration. By default, the setting
keep_opt_history is set to True. This allows you to store in memory the
databases of the sub-scenarios (see the last section of this example for more
details).
In some cases, storing the databases in memory can take up too much space and cause
performance issues. In these cases, set keep_opt_history=False and save the
databases to the disk using save_opt_history=True.
Just like for the sub-scenario, we define the algorithm settings for the system scenario.
system_sc_algo_settings = NLOPT_COBYLA_Settings(max_iter=100)
Build the System's Scenario#
The system level scenario is based on the three previous sub-scenarios for which we aim to maximize the range.
sub_scenarios = [propulsion_sc, aerodynamics_sc, structure_sc, mission_disc]
system_scenario = MDOScenario(
sub_scenarios,
"y_4",
design_space.filter(["x_shared"], copy=True),
formulation_settings_model=system_settings,
maximize_objective=True,
)
system_scenario.formulation.optimization_problem.objective *= 0.001
system_scenario.set_algorithm(algo_settings_model=system_sc_algo_settings)
system_scenario.add_constraint("g_1", constraint_type="ineq")
system_scenario.add_constraint("g_2", constraint_type="ineq")
system_scenario.add_constraint("g_3", constraint_type="ineq")
WARNING - 16:23:16: Two disciplines, among which AerodynamicsScenario_adapter, compute the same outputs: {'y_23', 'y_14', 'y_24', 'y_32', 'y_12', 'y_21', 'y_31', 'y_34'}
WARNING - 16:23:16: Self coupling variables in discipline PropulsionScenario_adapter are: ['y_21', 'y_23', 'y_31'].
WARNING - 16:23:16: Self coupling variables in discipline AerodynamicsScenario_adapter are: ['y_21', 'y_23', 'y_31'].
WARNING - 16:23:16: Self coupling variables in discipline StructureScenario_adapter are: ['y_21', 'y_23', 'y_31'].
WARNING - 16:23:16: The following disciplines contain self-couplings and strong couplings: ['AerodynamicsScenario_adapter', 'PropulsionScenario_adapter', 'StructureScenario_adapter']. This is not a problem as long as their self-coupling variables are not strongly coupled to another discipline.
WARNING - 16:23:16: The following outputs are defined multiple times: ['y_12', 'y_12', 'y_14', 'y_14', 'y_21', 'y_21', 'y_23', 'y_23', 'y_24', 'y_24', 'y_31', 'y_31', 'y_32', 'y_32', 'y_34', 'y_34'].
Visualize the XDSM#
Generate the XDSM on the fly:
log_workflow_status=Truewill log the status of the workflow in the console,save_html(defaultTrue) will generate a self-contained HTML file, that can be automatically opened usingshow_html=True.
system_scenario.xdsmize(save_html=False)
Execute the main scenario#
system_scenario.execute()
INFO - 16:23:16: *** Start MDOScenario execution ***
INFO - 16:23:16: MDOScenario
INFO - 16:23:16: Disciplines: AerodynamicsScenario PropulsionScenario SobieskiMission StructureScenario
INFO - 16:23:16: MDO formulation: BiLevelBCD
INFO - 16:23:16: Optimization problem:
INFO - 16:23:16: minimize 0.001*-y_4(x_shared)
INFO - 16:23:16: with respect to x_shared
INFO - 16:23:16: under the inequality constraints
INFO - 16:23:16: g_1(x_shared) <= 0
INFO - 16:23:16: g_2(x_shared) <= 0
INFO - 16:23:16: g_3(x_shared) <= 0
INFO - 16:23:16: over the design space:
INFO - 16:23:16: +-------------+-------------+-------+-------------+-------+
INFO - 16:23:16: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:16: +-------------+-------------+-------+-------------+-------+
INFO - 16:23:16: | x_shared[0] | 0.01 | 0.05 | 0.09 | float |
INFO - 16:23:16: | x_shared[1] | 30000 | 45000 | 60000 | float |
INFO - 16:23:16: | x_shared[2] | 1.4 | 1.6 | 1.8 | float |
INFO - 16:23:16: | x_shared[3] | 2.5 | 5.5 | 8.5 | float |
INFO - 16:23:16: | x_shared[4] | 40 | 55 | 70 | float |
INFO - 16:23:16: | x_shared[5] | 500 | 1000 | 1500 | float |
INFO - 16:23:16: +-------------+-------------+-------+-------------+-------+
INFO - 16:23:16: Solving optimization problem with algorithm NLOPT_COBYLA:
INFO - 16:23:16: *** Start PropulsionScenario execution ***
INFO - 16:23:16: PropulsionScenario
INFO - 16:23:16: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:16: MDO formulation: MDF
INFO - 16:23:16: Optimization problem:
INFO - 16:23:16: minimize 0.001*-y_4(x_3)
INFO - 16:23:16: with respect to x_3
INFO - 16:23:16: under the inequality constraints
INFO - 16:23:16: g_3(x_3) <= 0
INFO - 16:23:16: over the design space:
INFO - 16:23:16: +------+-------------+-------+-------------+-------+
INFO - 16:23:16: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:16: +------+-------------+-------+-------------+-------+
INFO - 16:23:16: | x_3 | 0.1 | 0.5 | 1 | float |
INFO - 16:23:16: +------+-------------+-------+-------------+-------+
INFO - 16:23:16: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:16: 2%|▏ | 1/50 [00:00<00:01, 41.90 it/sec, feas=False, obj=-0.536]
INFO - 16:23:16: 4%|▍ | 2/50 [00:00<00:01, 42.84 it/sec, feas=True, obj=-0.534]
INFO - 16:23:17: 6%|▌ | 3/50 [00:00<00:02, 21.68 it/sec, feas=False, obj=-0.537]
INFO - 16:23:17: Optimization result:
INFO - 16:23:17: Optimizer info:
INFO - 16:23:17: Status: 8
INFO - 16:23:17: Message: Positive directional derivative for linesearch
INFO - 16:23:17: Solution:
INFO - 16:23:17: The solution is feasible.
INFO - 16:23:17: Objective: -0.5340836123856838
INFO - 16:23:17: Standardized constraints:
INFO - 16:23:17: g_3 = [-0.91566801 -0.08433199 0. -0.05794805]
INFO - 16:23:17: Design space:
INFO - 16:23:17: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:17: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:17: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:17: | x_3 | 0.1 | 0.4302702621790957 | 1 | float |
INFO - 16:23:17: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:17: *** End PropulsionScenario execution (time: 0:00:00.141502) ***
INFO - 16:23:17: *** Start AerodynamicsScenario execution ***
INFO - 16:23:17: AerodynamicsScenario
INFO - 16:23:17: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:17: MDO formulation: MDF
INFO - 16:23:17: Optimization problem:
INFO - 16:23:17: minimize 0.001*-y_4(x_2)
INFO - 16:23:17: with respect to x_2
INFO - 16:23:17: under the inequality constraints
INFO - 16:23:17: g_2(x_2) <= 0
INFO - 16:23:17: over the design space:
INFO - 16:23:17: +------+-------------+-------+-------------+-------+
INFO - 16:23:17: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:17: +------+-------------+-------+-------------+-------+
INFO - 16:23:17: | x_2 | 0.75 | 1 | 1.25 | float |
INFO - 16:23:17: +------+-------------+-------+-------------+-------+
INFO - 16:23:17: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:17: 2%|▏ | 1/50 [00:00<00:00, 79.79 it/sec, feas=True, obj=-0.534]
INFO - 16:23:17: 4%|▍ | 2/50 [00:00<00:01, 46.07 it/sec, feas=True, obj=-0.535]
INFO - 16:23:17: 6%|▌ | 3/50 [00:00<00:01, 39.37 it/sec, feas=True, obj=-0.541]
INFO - 16:23:17: 8%|▊ | 4/50 [00:00<00:01, 36.57 it/sec, feas=True, obj=-0.551]
INFO - 16:23:17: Optimization result:
INFO - 16:23:17: Optimizer info:
INFO - 16:23:17: Status: 8
INFO - 16:23:17: Message: Positive directional derivative for linesearch
INFO - 16:23:17: Solution:
INFO - 16:23:17: The solution is feasible.
INFO - 16:23:17: Objective: -0.5514888881552081
INFO - 16:23:17: Standardized constraints:
INFO - 16:23:17: g_2 = -0.040000000000000036
INFO - 16:23:17: Design space:
INFO - 16:23:17: +------+-------------+-------+-------------+-------+
INFO - 16:23:17: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:17: +------+-------------+-------+-------------+-------+
INFO - 16:23:17: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:17: +------+-------------+-------+-------------+-------+
INFO - 16:23:17: *** End AerodynamicsScenario execution (time: 0:00:00.111685) ***
INFO - 16:23:17: *** Start StructureScenario execution ***
INFO - 16:23:17: StructureScenario
INFO - 16:23:17: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:17: MDO formulation: MDF
INFO - 16:23:17: Optimization problem:
INFO - 16:23:17: minimize 0.001*-y_4(x_1)
INFO - 16:23:17: with respect to x_1
INFO - 16:23:17: under the inequality constraints
INFO - 16:23:17: g_1(x_1) <= 0
INFO - 16:23:17: over the design space:
INFO - 16:23:17: +--------+-------------+-------+-------------+-------+
INFO - 16:23:17: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:17: +--------+-------------+-------+-------------+-------+
INFO - 16:23:17: | x_1[0] | 0.1 | 0.25 | 0.4 | float |
INFO - 16:23:17: | x_1[1] | 0.75 | 1 | 1.25 | float |
INFO - 16:23:17: +--------+-------------+-------+-------------+-------+
INFO - 16:23:17: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:17: 2%|▏ | 1/50 [00:00<00:00, 54.82 it/sec, feas=False, obj=-0.551]
INFO - 16:23:17: 4%|▍ | 2/50 [00:00<00:01, 33.29 it/sec, feas=True, obj=-0.548]
INFO - 16:23:17: 6%|▌ | 3/50 [00:00<00:01, 29.78 it/sec, feas=True, obj=-0.548]
INFO - 16:23:17: 8%|▊ | 4/50 [00:00<00:01, 28.04 it/sec, feas=True, obj=-0.549]
INFO - 16:23:17: 10%|█ | 5/50 [00:00<00:01, 27.27 it/sec, feas=True, obj=-0.549]
INFO - 16:23:17: 12%|█▏ | 6/50 [00:00<00:01, 27.21 it/sec, feas=True, obj=-0.552]
INFO - 16:23:17: 14%|█▍ | 7/50 [00:00<00:01, 27.05 it/sec, feas=True, obj=-0.553]
INFO - 16:23:17: 16%|█▌ | 8/50 [00:00<00:01, 27.01 it/sec, feas=True, obj=-0.553]
INFO - 16:23:17: 18%|█▊ | 9/50 [00:00<00:01, 26.97 it/sec, feas=True, obj=-0.553]
INFO - 16:23:17: 20%|██ | 10/50 [00:00<00:01, 28.23 it/sec, feas=True, obj=-0.553]
INFO - 16:23:17: Optimization result:
INFO - 16:23:17: Optimizer info:
INFO - 16:23:17: Status: None
INFO - 16:23:17: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:17: Solution:
INFO - 16:23:17: The solution is feasible.
INFO - 16:23:17: Objective: -0.5527823107565196
INFO - 16:23:17: Standardized constraints:
INFO - 16:23:17: g_1 = [ 8.52806714e-12 -2.99419226e-02 -4.49346629e-02 -5.39372764e-02
INFO - 16:23:17: -5.99419226e-02 -6.61963740e-02 -1.73803626e-01]
INFO - 16:23:17: Design space:
INFO - 16:23:17: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:17: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:17: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:17: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:17: | x_1[1] | 0.75 | 0.9857121415409077 | 1.25 | float |
INFO - 16:23:17: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:17: *** End StructureScenario execution (time: 0:00:00.357781) ***
INFO - 16:23:17: *** Start PropulsionScenario execution ***
INFO - 16:23:17: PropulsionScenario
INFO - 16:23:17: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:17: MDO formulation: MDF
INFO - 16:23:17: Optimization problem:
INFO - 16:23:17: minimize 0.001*-y_4(x_3)
INFO - 16:23:17: with respect to x_3
INFO - 16:23:17: under the inequality constraints
INFO - 16:23:17: g_3(x_3) <= 0
INFO - 16:23:17: over the design space:
INFO - 16:23:17: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:17: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:17: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:17: | x_3 | 0.1 | 0.4302702621790957 | 1 | float |
INFO - 16:23:17: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:17: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:17: 2%|▏ | 1/50 [00:00<00:00, 68.31 it/sec, feas=True, obj=-0.553]
INFO - 16:23:17: Optimization result:
INFO - 16:23:17: Optimizer info:
INFO - 16:23:17: Status: 8
INFO - 16:23:17: Message: Positive directional derivative for linesearch
INFO - 16:23:17: Solution:
INFO - 16:23:17: The solution is feasible.
INFO - 16:23:17: Objective: -0.5527823107565196
INFO - 16:23:17: Standardized constraints:
INFO - 16:23:17: g_3 = [-0.93393523 -0.06606477 0. -0.05794805]
INFO - 16:23:17: Design space:
INFO - 16:23:17: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:17: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:17: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:17: | x_3 | 0.1 | 0.4302702621790957 | 1 | float |
INFO - 16:23:17: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:17: *** End PropulsionScenario execution (time: 0:00:00.016646) ***
INFO - 16:23:17: *** Start AerodynamicsScenario execution ***
INFO - 16:23:17: AerodynamicsScenario
INFO - 16:23:17: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:17: MDO formulation: MDF
INFO - 16:23:17: Optimization problem:
INFO - 16:23:17: minimize 0.001*-y_4(x_2)
INFO - 16:23:17: with respect to x_2
INFO - 16:23:17: under the inequality constraints
INFO - 16:23:17: g_2(x_2) <= 0
INFO - 16:23:17: over the design space:
INFO - 16:23:17: +------+-------------+-------+-------------+-------+
INFO - 16:23:17: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:17: +------+-------------+-------+-------------+-------+
INFO - 16:23:17: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:17: +------+-------------+-------+-------------+-------+
INFO - 16:23:17: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:17: 2%|▏ | 1/50 [00:00<00:00, 82.79 it/sec, feas=True, obj=-0.553]
INFO - 16:23:17: Optimization result:
INFO - 16:23:17: Optimizer info:
INFO - 16:23:17: Status: 8
INFO - 16:23:17: Message: Positive directional derivative for linesearch
INFO - 16:23:17: Solution:
INFO - 16:23:17: The solution is feasible.
INFO - 16:23:17: Objective: -0.5527823107565196
INFO - 16:23:17: Standardized constraints:
INFO - 16:23:17: g_2 = -0.040000000000000036
INFO - 16:23:17: Design space:
INFO - 16:23:17: +------+-------------+-------+-------------+-------+
INFO - 16:23:17: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:17: +------+-------------+-------+-------------+-------+
INFO - 16:23:17: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:17: +------+-------------+-------+-------------+-------+
INFO - 16:23:17: *** End AerodynamicsScenario execution (time: 0:00:00.013828) ***
INFO - 16:23:17: *** Start StructureScenario execution ***
INFO - 16:23:17: StructureScenario
INFO - 16:23:17: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:17: MDO formulation: MDF
INFO - 16:23:17: Optimization problem:
INFO - 16:23:17: minimize 0.001*-y_4(x_1)
INFO - 16:23:17: with respect to x_1
INFO - 16:23:17: under the inequality constraints
INFO - 16:23:17: g_1(x_1) <= 0
INFO - 16:23:17: over the design space:
INFO - 16:23:17: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:17: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:17: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:17: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:17: | x_1[1] | 0.75 | 0.9857121415409077 | 1.25 | float |
INFO - 16:23:17: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:17: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:17: 2%|▏ | 1/50 [00:00<00:00, 79.92 it/sec, feas=True, obj=-0.553]
INFO - 16:23:17: 4%|▍ | 2/50 [00:00<00:00, 97.40 it/sec, feas=True, obj=-0.553]
INFO - 16:23:17: 6%|▌ | 3/50 [00:00<00:00, 75.62 it/sec, feas=True, obj=-0.553]
INFO - 16:23:17: Optimization result:
INFO - 16:23:17: Optimizer info:
INFO - 16:23:17: Status: None
INFO - 16:23:17: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:17: Solution:
INFO - 16:23:17: The solution is feasible.
INFO - 16:23:17: Objective: -0.5527823107565196
INFO - 16:23:17: Standardized constraints:
INFO - 16:23:17: g_1 = [ 8.52806714e-12 -2.99419226e-02 -4.49346629e-02 -5.39372764e-02
INFO - 16:23:17: -5.99419226e-02 -6.61963740e-02 -1.73803626e-01]
INFO - 16:23:17: Design space:
INFO - 16:23:17: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:17: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:17: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:17: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:17: | x_1[1] | 0.75 | 0.9857121415409077 | 1.25 | float |
INFO - 16:23:17: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:17: *** End StructureScenario execution (time: 0:00:00.042054) ***
INFO - 16:23:17: 1%| | 1/100 [00:00<01:10, 1.41 it/sec, feas=True, obj=-0.553]
INFO - 16:23:17: *** Start PropulsionScenario execution ***
INFO - 16:23:17: PropulsionScenario
INFO - 16:23:17: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:17: MDO formulation: MDF
INFO - 16:23:17: Optimization problem:
INFO - 16:23:17: minimize 0.001*-y_4(x_3)
INFO - 16:23:17: with respect to x_3
INFO - 16:23:17: under the inequality constraints
INFO - 16:23:17: g_3(x_3) <= 0
INFO - 16:23:17: over the design space:
INFO - 16:23:17: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:17: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:17: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:17: | x_3 | 0.1 | 0.4302702621790957 | 1 | float |
INFO - 16:23:17: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:17: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:17: 2%|▏ | 1/50 [00:00<00:01, 38.29 it/sec, feas=True, obj=-0.551]
INFO - 16:23:17: Optimization result:
INFO - 16:23:17: Optimizer info:
INFO - 16:23:17: Status: 8
INFO - 16:23:17: Message: Positive directional derivative for linesearch
INFO - 16:23:17: Solution:
INFO - 16:23:17: The solution is feasible.
INFO - 16:23:17: Objective: -0.551442601535279
INFO - 16:23:17: Standardized constraints:
INFO - 16:23:17: g_3 = [-0.75494685 -0.24505315 0. -0.05794805]
INFO - 16:23:17: Design space:
INFO - 16:23:17: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:17: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:17: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:17: | x_3 | 0.1 | 0.4302702621790957 | 1 | float |
INFO - 16:23:17: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:17: *** End PropulsionScenario execution (time: 0:00:00.028168) ***
INFO - 16:23:17: *** Start AerodynamicsScenario execution ***
INFO - 16:23:17: AerodynamicsScenario
INFO - 16:23:17: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:17: MDO formulation: MDF
INFO - 16:23:17: Optimization problem:
INFO - 16:23:17: minimize 0.001*-y_4(x_2)
INFO - 16:23:17: with respect to x_2
INFO - 16:23:17: under the inequality constraints
INFO - 16:23:17: g_2(x_2) <= 0
INFO - 16:23:17: over the design space:
INFO - 16:23:17: +------+-------------+-------+-------------+-------+
INFO - 16:23:17: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:17: +------+-------------+-------+-------------+-------+
INFO - 16:23:17: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:17: +------+-------------+-------+-------------+-------+
INFO - 16:23:17: Solving optimization problem with algorithm SLSQP:
WARNING - 16:23:17: Optimization found no feasible point; the least infeasible point is selected.
INFO - 16:23:17: 2%|▏ | 1/50 [00:00<00:00, 101.45 it/sec, feas=False, obj=-0.551]
INFO - 16:23:17: Optimization result:
INFO - 16:23:17: Optimizer info:
INFO - 16:23:17: Status: 8
INFO - 16:23:17: Message: Positive directional derivative for linesearch
INFO - 16:23:17: Solution:
WARNING - 16:23:17: The solution is not feasible.
INFO - 16:23:17: Objective: -0.551442601535279
INFO - 16:23:17: Standardized constraints:
INFO - 16:23:17: g_2 = 0.010000000000000009
INFO - 16:23:17: Design space:
INFO - 16:23:17: +------+-------------+-------+-------------+-------+
INFO - 16:23:17: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:17: +------+-------------+-------+-------------+-------+
INFO - 16:23:17: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:17: +------+-------------+-------+-------------+-------+
INFO - 16:23:17: *** End AerodynamicsScenario execution (time: 0:00:00.011567) ***
INFO - 16:23:17: *** Start StructureScenario execution ***
INFO - 16:23:17: StructureScenario
INFO - 16:23:17: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:17: MDO formulation: MDF
INFO - 16:23:17: Optimization problem:
INFO - 16:23:17: minimize 0.001*-y_4(x_1)
INFO - 16:23:17: with respect to x_1
INFO - 16:23:17: under the inequality constraints
INFO - 16:23:17: g_1(x_1) <= 0
INFO - 16:23:17: over the design space:
INFO - 16:23:17: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:17: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:17: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:17: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:17: | x_1[1] | 0.75 | 0.9857121415409077 | 1.25 | float |
INFO - 16:23:17: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:17: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:17: 2%|▏ | 1/50 [00:00<00:00, 96.05 it/sec, feas=True, obj=-0.551]
INFO - 16:23:17: 4%|▍ | 2/50 [00:00<00:01, 39.19 it/sec, feas=True, obj=-0.553]
INFO - 16:23:17: 6%|▌ | 3/50 [00:00<00:01, 35.36 it/sec, feas=True, obj=-0.562]
INFO - 16:23:17: 8%|▊ | 4/50 [00:00<00:01, 31.13 it/sec, feas=True, obj=-0.574]
INFO - 16:23:17: 10%|█ | 5/50 [00:00<00:01, 29.73 it/sec, feas=True, obj=-0.574]
INFO - 16:23:17: 12%|█▏ | 6/50 [00:00<00:01, 28.83 it/sec, feas=True, obj=-0.574]
INFO - 16:23:17: 14%|█▍ | 7/50 [00:00<00:01, 28.18 it/sec, feas=True, obj=-0.574]
INFO - 16:23:17: 16%|█▌ | 8/50 [00:00<00:01, 27.63 it/sec, feas=True, obj=-0.574]
INFO - 16:23:17: 18%|█▊ | 9/50 [00:00<00:01, 27.33 it/sec, feas=True, obj=-0.574]
INFO - 16:23:18: 20%|██ | 10/50 [00:00<00:01, 27.17 it/sec, feas=True, obj=-0.574]
INFO - 16:23:18: 22%|██▏ | 11/50 [00:00<00:01, 27.01 it/sec, feas=True, obj=-0.574]
INFO - 16:23:18: 24%|██▍ | 12/50 [00:00<00:01, 26.85 it/sec, feas=True, obj=-0.574]
INFO - 16:23:18: Optimization result:
INFO - 16:23:18: Optimizer info:
INFO - 16:23:18: Status: 8
INFO - 16:23:18: Message: Positive directional derivative for linesearch
INFO - 16:23:18: Solution:
INFO - 16:23:18: The solution is feasible.
INFO - 16:23:18: Objective: -0.5744011122248631
INFO - 16:23:18: Standardized constraints:
INFO - 16:23:18: g_1 = [-0.02505357 -0.02542063 -0.03358482 -0.04103714 -0.04706944 -0.20645898
INFO - 16:23:18: -0.03354102]
INFO - 16:23:18: Design space:
INFO - 16:23:18: +--------+-------------+-------+-------------+-------+
INFO - 16:23:18: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:18: +--------+-------------+-------+-------------+-------+
INFO - 16:23:18: | x_1[0] | 0.1 | 0.4 | 0.4 | float |
INFO - 16:23:18: | x_1[1] | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:18: +--------+-------------+-------+-------------+-------+
INFO - 16:23:18: *** End StructureScenario execution (time: 0:00:00.449284) ***
INFO - 16:23:18: *** Start PropulsionScenario execution ***
INFO - 16:23:18: PropulsionScenario
INFO - 16:23:18: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:18: MDO formulation: MDF
INFO - 16:23:18: Optimization problem:
INFO - 16:23:18: minimize 0.001*-y_4(x_3)
INFO - 16:23:18: with respect to x_3
INFO - 16:23:18: under the inequality constraints
INFO - 16:23:18: g_3(x_3) <= 0
INFO - 16:23:18: over the design space:
INFO - 16:23:18: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:18: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:18: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:18: | x_3 | 0.1 | 0.4302702621790957 | 1 | float |
INFO - 16:23:18: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:18: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:18: 2%|▏ | 1/50 [00:00<00:00, 105.16 it/sec, feas=True, obj=-0.574]
INFO - 16:23:18: Optimization result:
INFO - 16:23:18: Optimizer info:
INFO - 16:23:18: Status: 8
INFO - 16:23:18: Message: Positive directional derivative for linesearch
INFO - 16:23:18: Solution:
INFO - 16:23:18: The solution is feasible.
INFO - 16:23:18: Objective: -0.5744011122248631
INFO - 16:23:18: Standardized constraints:
INFO - 16:23:18: g_3 = [-0.7550343 -0.2449657 0. -0.05794805]
INFO - 16:23:18: Design space:
INFO - 16:23:18: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:18: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:18: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:18: | x_3 | 0.1 | 0.4302702621790957 | 1 | float |
INFO - 16:23:18: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:18: *** End PropulsionScenario execution (time: 0:00:00.011559) ***
INFO - 16:23:18: *** Start AerodynamicsScenario execution ***
INFO - 16:23:18: AerodynamicsScenario
INFO - 16:23:18: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:18: MDO formulation: MDF
INFO - 16:23:18: Optimization problem:
INFO - 16:23:18: minimize 0.001*-y_4(x_2)
INFO - 16:23:18: with respect to x_2
INFO - 16:23:18: under the inequality constraints
INFO - 16:23:18: g_2(x_2) <= 0
INFO - 16:23:18: over the design space:
INFO - 16:23:18: +------+-------------+-------+-------------+-------+
INFO - 16:23:18: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:18: +------+-------------+-------+-------------+-------+
INFO - 16:23:18: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:18: +------+-------------+-------+-------------+-------+
INFO - 16:23:18: Solving optimization problem with algorithm SLSQP:
WARNING - 16:23:18: Optimization found no feasible point; the least infeasible point is selected.
INFO - 16:23:18: 2%|▏ | 1/50 [00:00<00:00, 86.54 it/sec, feas=False, obj=-0.574]
INFO - 16:23:18: Optimization result:
INFO - 16:23:18: Optimizer info:
INFO - 16:23:18: Status: 8
INFO - 16:23:18: Message: Positive directional derivative for linesearch
INFO - 16:23:18: Solution:
WARNING - 16:23:18: The solution is not feasible.
INFO - 16:23:18: Objective: -0.5744011122248631
INFO - 16:23:18: Standardized constraints:
INFO - 16:23:18: g_2 = 0.010000000000000009
INFO - 16:23:18: Design space:
INFO - 16:23:18: +------+-------------+-------+-------------+-------+
INFO - 16:23:18: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:18: +------+-------------+-------+-------------+-------+
INFO - 16:23:18: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:18: +------+-------------+-------+-------------+-------+
INFO - 16:23:18: *** End AerodynamicsScenario execution (time: 0:00:00.013332) ***
INFO - 16:23:18: *** Start StructureScenario execution ***
INFO - 16:23:18: StructureScenario
INFO - 16:23:18: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:18: MDO formulation: MDF
INFO - 16:23:18: Optimization problem:
INFO - 16:23:18: minimize 0.001*-y_4(x_1)
INFO - 16:23:18: with respect to x_1
INFO - 16:23:18: under the inequality constraints
INFO - 16:23:18: g_1(x_1) <= 0
INFO - 16:23:18: over the design space:
INFO - 16:23:18: +--------+-------------+-------+-------------+-------+
INFO - 16:23:18: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:18: +--------+-------------+-------+-------------+-------+
INFO - 16:23:18: | x_1[0] | 0.1 | 0.4 | 0.4 | float |
INFO - 16:23:18: | x_1[1] | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:18: +--------+-------------+-------+-------------+-------+
INFO - 16:23:18: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:18: 2%|▏ | 1/50 [00:00<00:00, 100.12 it/sec, feas=True, obj=-0.574]
INFO - 16:23:18: Optimization result:
INFO - 16:23:18: Optimizer info:
INFO - 16:23:18: Status: 8
INFO - 16:23:18: Message: Positive directional derivative for linesearch
INFO - 16:23:18: Solution:
INFO - 16:23:18: The solution is feasible.
INFO - 16:23:18: Objective: -0.5744011122248631
INFO - 16:23:18: Standardized constraints:
INFO - 16:23:18: g_1 = [-0.02505357 -0.02542063 -0.03358482 -0.04103714 -0.04706944 -0.20645898
INFO - 16:23:18: -0.03354102]
INFO - 16:23:18: Design space:
INFO - 16:23:18: +--------+-------------+-------+-------------+-------+
INFO - 16:23:18: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:18: +--------+-------------+-------+-------------+-------+
INFO - 16:23:18: | x_1[0] | 0.1 | 0.4 | 0.4 | float |
INFO - 16:23:18: | x_1[1] | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:18: +--------+-------------+-------+-------------+-------+
INFO - 16:23:18: *** End StructureScenario execution (time: 0:00:00.012094) ***
INFO - 16:23:18: 2%|▏ | 2/100 [00:01<01:02, 1.58 it/sec, feas=False, obj=-0.574]
INFO - 16:23:18: *** Start PropulsionScenario execution ***
INFO - 16:23:18: PropulsionScenario
INFO - 16:23:18: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:18: MDO formulation: MDF
INFO - 16:23:18: Optimization problem:
INFO - 16:23:18: minimize 0.001*-y_4(x_3)
INFO - 16:23:18: with respect to x_3
INFO - 16:23:18: under the inequality constraints
INFO - 16:23:18: g_3(x_3) <= 0
INFO - 16:23:18: over the design space:
INFO - 16:23:18: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:18: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:18: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:18: | x_3 | 0.1 | 0.4302702621790957 | 1 | float |
INFO - 16:23:18: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:18: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:18: 2%|▏ | 1/50 [00:00<00:01, 39.13 it/sec, feas=False, obj=-0.843]
INFO - 16:23:18: 4%|▍ | 2/50 [00:00<00:01, 39.85 it/sec, feas=True, obj=-0.813]
INFO - 16:23:18: 6%|▌ | 3/50 [00:00<00:01, 32.93 it/sec, feas=False, obj=-0.845]
INFO - 16:23:18: 8%|▊ | 4/50 [00:00<00:01, 30.23 it/sec, feas=True, obj=-0.813]
INFO - 16:23:18: 10%|█ | 5/50 [00:00<00:01, 31.71 it/sec, feas=True, obj=-0.813]
INFO - 16:23:18: 12%|█▏ | 6/50 [00:00<00:01, 32.67 it/sec, feas=True, obj=-0.813]
INFO - 16:23:18: Optimization result:
INFO - 16:23:18: Optimizer info:
INFO - 16:23:18: Status: None
INFO - 16:23:18: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:18: Solution:
INFO - 16:23:18: The solution is feasible.
INFO - 16:23:18: Objective: -0.8130465205349736
INFO - 16:23:18: Standardized constraints:
INFO - 16:23:18: g_3 = [-7.18403565e-01 -2.81596435e-01 1.11022302e-15 -1.27460556e-01]
INFO - 16:23:18: Design space:
INFO - 16:23:18: +------+-------------+-------------------+-------------+-------+
INFO - 16:23:18: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:18: +------+-------------+-------------------+-------------+-------+
INFO - 16:23:18: | x_3 | 0.1 | 0.287100477203897 | 1 | float |
INFO - 16:23:18: +------+-------------+-------------------+-------------+-------+
INFO - 16:23:18: *** End PropulsionScenario execution (time: 0:00:00.186730) ***
INFO - 16:23:18: *** Start AerodynamicsScenario execution ***
INFO - 16:23:18: AerodynamicsScenario
INFO - 16:23:18: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:18: MDO formulation: MDF
INFO - 16:23:18: Optimization problem:
INFO - 16:23:18: minimize 0.001*-y_4(x_2)
INFO - 16:23:18: with respect to x_2
INFO - 16:23:18: under the inequality constraints
INFO - 16:23:18: g_2(x_2) <= 0
INFO - 16:23:18: over the design space:
INFO - 16:23:18: +------+-------------+-------+-------------+-------+
INFO - 16:23:18: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:18: +------+-------------+-------+-------------+-------+
INFO - 16:23:18: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:18: +------+-------------+-------+-------------+-------+
INFO - 16:23:18: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:18: 2%|▏ | 1/50 [00:00<00:00, 88.82 it/sec, feas=False, obj=-0.813]
INFO - 16:23:18: 4%|▍ | 2/50 [00:00<00:00, 142.30 it/sec, feas=False, obj=-0.813]
INFO - 16:23:18: 6%|▌ | 3/50 [00:00<00:00, 176.93 it/sec, feas=False, obj=-0.813]
INFO - 16:23:18: 8%|▊ | 4/50 [00:00<00:00, 202.60 it/sec, feas=False, obj=-0.813]
INFO - 16:23:18: 10%|█ | 5/50 [00:00<00:00, 222.05 it/sec, feas=False, obj=-0.813]
INFO - 16:23:18: 12%|█▏ | 6/50 [00:00<00:00, 236.94 it/sec, feas=False, obj=-0.813]
INFO - 16:23:18: 14%|█▍ | 7/50 [00:00<00:00, 249.32 it/sec, feas=False, obj=-0.813]
INFO - 16:23:18: 16%|█▌ | 8/50 [00:00<00:00, 260.20 it/sec, feas=False, obj=-0.813]
INFO - 16:23:18: 18%|█▊ | 9/50 [00:00<00:00, 271.11 it/sec, feas=False, obj=-0.813]
INFO - 16:23:18: 20%|██ | 10/50 [00:00<00:00, 282.96 it/sec, feas=False, obj=-0.813]
INFO - 16:23:18: 22%|██▏ | 11/50 [00:00<00:00, 292.48 it/sec, feas=False, obj=-0.813]
INFO - 16:23:18: 24%|██▍ | 12/50 [00:00<00:00, 295.76 it/sec, feas=False, obj=-0.813]
INFO - 16:23:18: 26%|██▌ | 13/50 [00:00<00:00, 299.00 it/sec, feas=False, obj=-0.813]
INFO - 16:23:18: 28%|██▊ | 14/50 [00:00<00:00, 302.25 it/sec, feas=False, obj=-0.813]
INFO - 16:23:18: 30%|███ | 15/50 [00:00<00:00, 229.21 it/sec, feas=False, obj=-0.813]
INFO - 16:23:18: 32%|███▏ | 16/50 [00:00<00:00, 233.88 it/sec, feas=False, obj=-0.813]
INFO - 16:23:18: 34%|███▍ | 17/50 [00:00<00:00, 238.71 it/sec, feas=False, obj=-0.813]
INFO - 16:23:18: 36%|███▌ | 18/50 [00:00<00:00, 243.28 it/sec, feas=False, obj=-0.813]
INFO - 16:23:18: 38%|███▊ | 19/50 [00:00<00:00, 247.45 it/sec, feas=False, obj=-0.813]
INFO - 16:23:18: 40%|████ | 20/50 [00:00<00:00, 245.21 it/sec, feas=False, obj=-0.813]
WARNING - 16:23:18: Optimization found no feasible point; the least infeasible point is selected.
INFO - 16:23:18: 42%|████▏ | 21/50 [00:00<00:00, 246.46 it/sec, feas=False, obj=-0.813]
INFO - 16:23:18: Optimization result:
INFO - 16:23:18: Optimizer info:
INFO - 16:23:18: Status: 8
INFO - 16:23:18: Message: Positive directional derivative for linesearch
INFO - 16:23:18: Solution:
WARNING - 16:23:18: The solution is not feasible.
INFO - 16:23:18: Objective: -0.8130465205349736
INFO - 16:23:18: Standardized constraints:
INFO - 16:23:18: g_2 = 0.010000000000000009
INFO - 16:23:18: Design space:
INFO - 16:23:18: +------+-------------+-------+-------------+-------+
INFO - 16:23:18: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:18: +------+-------------+-------+-------------+-------+
INFO - 16:23:18: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:18: +------+-------------+-------+-------------+-------+
INFO - 16:23:18: *** End AerodynamicsScenario execution (time: 0:00:00.086896) ***
INFO - 16:23:18: *** Start StructureScenario execution ***
INFO - 16:23:18: StructureScenario
INFO - 16:23:18: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:18: MDO formulation: MDF
INFO - 16:23:18: Optimization problem:
INFO - 16:23:18: minimize 0.001*-y_4(x_1)
INFO - 16:23:18: with respect to x_1
INFO - 16:23:18: under the inequality constraints
INFO - 16:23:18: g_1(x_1) <= 0
INFO - 16:23:18: over the design space:
INFO - 16:23:18: +--------+-------------+-------+-------------+-------+
INFO - 16:23:18: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:18: +--------+-------------+-------+-------------+-------+
INFO - 16:23:18: | x_1[0] | 0.1 | 0.4 | 0.4 | float |
INFO - 16:23:18: | x_1[1] | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:18: +--------+-------------+-------+-------------+-------+
INFO - 16:23:18: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:18: 2%|▏ | 1/50 [00:00<00:00, 65.67 it/sec, feas=True, obj=-0.813]
INFO - 16:23:18: 4%|▍ | 2/50 [00:00<00:01, 42.11 it/sec, feas=True, obj=-0.813]
INFO - 16:23:18: 6%|▌ | 3/50 [00:00<00:01, 38.14 it/sec, feas=True, obj=-0.813]
INFO - 16:23:18: Optimization result:
INFO - 16:23:18: Optimizer info:
INFO - 16:23:18: Status: None
INFO - 16:23:18: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:18: Solution:
INFO - 16:23:18: The solution is feasible.
INFO - 16:23:18: Objective: -0.8130465227028968
INFO - 16:23:18: Standardized constraints:
INFO - 16:23:18: g_1 = [-0.02505986 -0.02542504 -0.03358821 -0.04103989 -0.04707176 -0.20645248
INFO - 16:23:18: -0.03354752]
INFO - 16:23:18: Design space:
INFO - 16:23:18: +--------+-------------+-------------------+-------------+-------+
INFO - 16:23:18: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:18: +--------+-------------+-------------------+-------------+-------+
INFO - 16:23:18: | x_1[0] | 0.1 | 0.399965782150056 | 0.4 | float |
INFO - 16:23:18: | x_1[1] | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:18: +--------+-------------+-------------------+-------------+-------+
INFO - 16:23:18: *** End StructureScenario execution (time: 0:00:00.081499) ***
INFO - 16:23:18: *** Start PropulsionScenario execution ***
INFO - 16:23:18: PropulsionScenario
INFO - 16:23:18: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:18: MDO formulation: MDF
INFO - 16:23:18: Optimization problem:
INFO - 16:23:18: minimize 0.001*-y_4(x_3)
INFO - 16:23:18: with respect to x_3
INFO - 16:23:18: under the inequality constraints
INFO - 16:23:18: g_3(x_3) <= 0
INFO - 16:23:18: over the design space:
INFO - 16:23:18: +------+-------------+-------------------+-------------+-------+
INFO - 16:23:18: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:18: +------+-------------+-------------------+-------------+-------+
INFO - 16:23:18: | x_3 | 0.1 | 0.287100477203897 | 1 | float |
INFO - 16:23:18: +------+-------------+-------------------+-------------+-------+
INFO - 16:23:18: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:18: 2%|▏ | 1/50 [00:00<00:00, 105.66 it/sec, feas=True, obj=-0.813]
INFO - 16:23:18: 4%|▍ | 2/50 [00:00<00:00, 67.18 it/sec, feas=True, obj=-0.813]
INFO - 16:23:18: 6%|▌ | 3/50 [00:00<00:00, 87.17 it/sec, feas=True, obj=-0.813]
INFO - 16:23:18: Optimization result:
INFO - 16:23:18: Optimizer info:
INFO - 16:23:18: Status: 8
INFO - 16:23:18: Message: Positive directional derivative for linesearch
INFO - 16:23:18: Solution:
INFO - 16:23:18: The solution is feasible.
INFO - 16:23:18: Objective: -0.8130465227028969
INFO - 16:23:18: Standardized constraints:
INFO - 16:23:18: g_3 = [-7.18403601e-01 -2.81596399e-01 2.22044605e-16 -1.27460556e-01]
INFO - 16:23:18: Design space:
INFO - 16:23:18: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:18: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:18: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:18: | x_3 | 0.1 | 0.2871004772038968 | 1 | float |
INFO - 16:23:18: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:18: *** End PropulsionScenario execution (time: 0:00:00.036451) ***
INFO - 16:23:18: *** Start AerodynamicsScenario execution ***
INFO - 16:23:18: AerodynamicsScenario
INFO - 16:23:18: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:18: MDO formulation: MDF
INFO - 16:23:18: Optimization problem:
INFO - 16:23:18: minimize 0.001*-y_4(x_2)
INFO - 16:23:18: with respect to x_2
INFO - 16:23:18: under the inequality constraints
INFO - 16:23:18: g_2(x_2) <= 0
INFO - 16:23:18: over the design space:
INFO - 16:23:18: +------+-------------+-------+-------------+-------+
INFO - 16:23:18: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:18: +------+-------------+-------+-------------+-------+
INFO - 16:23:18: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:18: +------+-------------+-------+-------------+-------+
INFO - 16:23:18: Solving optimization problem with algorithm SLSQP:
WARNING - 16:23:18: Optimization found no feasible point; the least infeasible point is selected.
INFO - 16:23:18: 2%|▏ | 1/50 [00:00<00:00, 84.48 it/sec, feas=False, obj=-0.813]
INFO - 16:23:18: Optimization result:
INFO - 16:23:18: Optimizer info:
INFO - 16:23:18: Status: 8
INFO - 16:23:18: Message: Positive directional derivative for linesearch
INFO - 16:23:18: Solution:
WARNING - 16:23:18: The solution is not feasible.
INFO - 16:23:18: Objective: -0.8130465227028969
INFO - 16:23:18: Standardized constraints:
INFO - 16:23:18: g_2 = 0.010000000000000009
INFO - 16:23:18: Design space:
INFO - 16:23:18: +------+-------------+-------+-------------+-------+
INFO - 16:23:18: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:18: +------+-------------+-------+-------------+-------+
INFO - 16:23:18: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:18: +------+-------------+-------+-------------+-------+
INFO - 16:23:18: *** End AerodynamicsScenario execution (time: 0:00:00.013550) ***
INFO - 16:23:18: *** Start StructureScenario execution ***
INFO - 16:23:18: StructureScenario
INFO - 16:23:18: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:18: MDO formulation: MDF
INFO - 16:23:18: Optimization problem:
INFO - 16:23:18: minimize 0.001*-y_4(x_1)
INFO - 16:23:18: with respect to x_1
INFO - 16:23:18: under the inequality constraints
INFO - 16:23:18: g_1(x_1) <= 0
INFO - 16:23:18: over the design space:
INFO - 16:23:18: +--------+-------------+-------------------+-------------+-------+
INFO - 16:23:18: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:18: +--------+-------------+-------------------+-------------+-------+
INFO - 16:23:18: | x_1[0] | 0.1 | 0.399965782150056 | 0.4 | float |
INFO - 16:23:18: | x_1[1] | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:18: +--------+-------------+-------------------+-------------+-------+
INFO - 16:23:18: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:18: 2%|▏ | 1/50 [00:00<00:00, 101.62 it/sec, feas=True, obj=-0.813]
WARNING - 16:23:18: MDAGaussSeidel has reached its maximum number of unsuccessful iterations, but the normalized residual norm 0.0009157477359807847 is still above the tolerance 1e-06.
INFO - 16:23:18: 4%|▍ | 2/50 [00:00<00:01, 40.13 it/sec, feas=True, obj=-0.813]
INFO - 16:23:18: 6%|▌ | 3/50 [00:00<00:01, 37.85 it/sec, feas=True, obj=-0.813]
INFO - 16:23:18: Optimization result:
INFO - 16:23:18: Optimizer info:
INFO - 16:23:18: Status: None
INFO - 16:23:18: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:18: Solution:
INFO - 16:23:18: The solution is feasible.
INFO - 16:23:18: Objective: -0.81304652486895
INFO - 16:23:18: Standardized constraints:
INFO - 16:23:18: g_1 = [-0.02506614 -0.02542945 -0.0335916 -0.04104264 -0.04707407 -0.20644599
INFO - 16:23:18: -0.03355401]
INFO - 16:23:18: Design space:
INFO - 16:23:18: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:18: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:18: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:18: | x_1[0] | 0.1 | 0.3999315790669682 | 0.4 | float |
INFO - 16:23:18: | x_1[1] | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:18: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:18: *** End StructureScenario execution (time: 0:00:00.082064) ***
INFO - 16:23:18: *** Start PropulsionScenario execution ***
INFO - 16:23:18: PropulsionScenario
INFO - 16:23:18: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:18: MDO formulation: MDF
INFO - 16:23:18: Optimization problem:
INFO - 16:23:18: minimize 0.001*-y_4(x_3)
INFO - 16:23:18: with respect to x_3
INFO - 16:23:18: under the inequality constraints
INFO - 16:23:18: g_3(x_3) <= 0
INFO - 16:23:18: over the design space:
INFO - 16:23:18: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:18: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:18: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:18: | x_3 | 0.1 | 0.2871004772038968 | 1 | float |
INFO - 16:23:18: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:18: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:18: 2%|▏ | 1/50 [00:00<00:00, 108.34 it/sec, feas=True, obj=-0.813]
INFO - 16:23:18: 4%|▍ | 2/50 [00:00<00:00, 128.43 it/sec, feas=True, obj=-0.813]
INFO - 16:23:18: Optimization result:
INFO - 16:23:18: Optimizer info:
INFO - 16:23:18: Status: 8
INFO - 16:23:18: Message: Positive directional derivative for linesearch
INFO - 16:23:18: Solution:
INFO - 16:23:18: The solution is feasible.
INFO - 16:23:18: Objective: -0.81304652486895
INFO - 16:23:18: Standardized constraints:
INFO - 16:23:18: g_3 = [-7.18403636e-01 -2.81596364e-01 2.22044605e-16 -1.27460556e-01]
INFO - 16:23:18: Design space:
INFO - 16:23:18: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:18: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:18: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:18: | x_3 | 0.1 | 0.2871004772038968 | 1 | float |
INFO - 16:23:18: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:18: *** End PropulsionScenario execution (time: 0:00:00.017592) ***
INFO - 16:23:18: *** Start AerodynamicsScenario execution ***
INFO - 16:23:18: AerodynamicsScenario
INFO - 16:23:18: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:18: MDO formulation: MDF
INFO - 16:23:18: Optimization problem:
INFO - 16:23:18: minimize 0.001*-y_4(x_2)
INFO - 16:23:18: with respect to x_2
INFO - 16:23:18: under the inequality constraints
INFO - 16:23:18: g_2(x_2) <= 0
INFO - 16:23:18: over the design space:
INFO - 16:23:18: +------+-------------+-------+-------------+-------+
INFO - 16:23:18: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:18: +------+-------------+-------+-------------+-------+
INFO - 16:23:18: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:18: +------+-------------+-------+-------------+-------+
INFO - 16:23:18: Solving optimization problem with algorithm SLSQP:
WARNING - 16:23:18: Optimization found no feasible point; the least infeasible point is selected.
INFO - 16:23:18: 2%|▏ | 1/50 [00:00<00:00, 67.35 it/sec, feas=False, obj=-0.813]
INFO - 16:23:18: Optimization result:
INFO - 16:23:18: Optimizer info:
INFO - 16:23:18: Status: 8
INFO - 16:23:18: Message: Positive directional derivative for linesearch
INFO - 16:23:18: Solution:
WARNING - 16:23:18: The solution is not feasible.
INFO - 16:23:18: Objective: -0.81304652486895
INFO - 16:23:18: Standardized constraints:
INFO - 16:23:18: g_2 = 0.010000000000000009
INFO - 16:23:18: Design space:
INFO - 16:23:18: +------+-------------+-------+-------------+-------+
INFO - 16:23:18: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:18: +------+-------------+-------+-------------+-------+
INFO - 16:23:18: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:18: +------+-------------+-------+-------------+-------+
INFO - 16:23:18: *** End AerodynamicsScenario execution (time: 0:00:00.016534) ***
INFO - 16:23:18: *** Start StructureScenario execution ***
INFO - 16:23:18: StructureScenario
INFO - 16:23:18: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:18: MDO formulation: MDF
INFO - 16:23:18: Optimization problem:
INFO - 16:23:18: minimize 0.001*-y_4(x_1)
INFO - 16:23:18: with respect to x_1
INFO - 16:23:18: under the inequality constraints
INFO - 16:23:18: g_1(x_1) <= 0
INFO - 16:23:18: over the design space:
INFO - 16:23:18: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:18: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:18: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:18: | x_1[0] | 0.1 | 0.3999315790669682 | 0.4 | float |
INFO - 16:23:18: | x_1[1] | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:18: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:18: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:18: 2%|▏ | 1/50 [00:00<00:00, 96.44 it/sec, feas=True, obj=-0.813]
INFO - 16:23:18: 4%|▍ | 2/50 [00:00<00:00, 50.37 it/sec, feas=True, obj=-0.813]
WARNING - 16:23:18: MDAGaussSeidel has reached its maximum number of unsuccessful iterations, but the normalized residual norm 0.0009157477359807847 is still above the tolerance 1e-06.
INFO - 16:23:18: 6%|▌ | 3/50 [00:00<00:01, 37.78 it/sec, feas=True, obj=-0.813]
INFO - 16:23:18: Optimization result:
INFO - 16:23:18: Optimizer info:
INFO - 16:23:18: Status: None
INFO - 16:23:18: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:18: Solution:
INFO - 16:23:18: The solution is feasible.
INFO - 16:23:18: Objective: -0.8130465270331332
INFO - 16:23:18: Standardized constraints:
INFO - 16:23:18: g_1 = [-0.02507242 -0.02543386 -0.03359499 -0.04104539 -0.04707639 -0.20643949
INFO - 16:23:18: -0.03356051]
INFO - 16:23:18: Design space:
INFO - 16:23:18: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:18: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:18: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:18: | x_1[0] | 0.1 | 0.3998973907465287 | 0.4 | float |
INFO - 16:23:18: | x_1[1] | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:18: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:18: *** End StructureScenario execution (time: 0:00:00.083796) ***
INFO - 16:23:18: *** Start PropulsionScenario execution ***
INFO - 16:23:18: PropulsionScenario
INFO - 16:23:18: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:18: MDO formulation: MDF
INFO - 16:23:18: Optimization problem:
INFO - 16:23:18: minimize 0.001*-y_4(x_3)
INFO - 16:23:18: with respect to x_3
INFO - 16:23:18: under the inequality constraints
INFO - 16:23:18: g_3(x_3) <= 0
INFO - 16:23:18: over the design space:
INFO - 16:23:18: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:18: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:18: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:18: | x_3 | 0.1 | 0.2871004772038968 | 1 | float |
INFO - 16:23:18: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:18: Solving optimization problem with algorithm SLSQP:
WARNING - 16:23:18: MDAGaussSeidel has reached its maximum number of unsuccessful iterations, but the normalized residual norm 6.724932466608626e-05 is still above the tolerance 1e-06.
INFO - 16:23:18: 2%|▏ | 1/50 [00:00<00:00, 53.37 it/sec, feas=True, obj=-0.813]
INFO - 16:23:18: Optimization result:
INFO - 16:23:18: Optimizer info:
INFO - 16:23:18: Status: 8
INFO - 16:23:18: Message: Positive directional derivative for linesearch
INFO - 16:23:18: Solution:
INFO - 16:23:18: The solution is feasible.
INFO - 16:23:18: Objective: -0.8130465270331335
INFO - 16:23:18: Standardized constraints:
INFO - 16:23:18: g_3 = [-7.18403672e-01 -2.81596328e-01 2.22044605e-16 -1.27460556e-01]
INFO - 16:23:18: Design space:
INFO - 16:23:18: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:18: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:18: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:18: | x_3 | 0.1 | 0.2871004772038968 | 1 | float |
INFO - 16:23:18: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:18: *** End PropulsionScenario execution (time: 0:00:00.020520) ***
INFO - 16:23:18: *** Start AerodynamicsScenario execution ***
INFO - 16:23:18: AerodynamicsScenario
INFO - 16:23:18: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:18: MDO formulation: MDF
INFO - 16:23:18: Optimization problem:
INFO - 16:23:18: minimize 0.001*-y_4(x_2)
INFO - 16:23:18: with respect to x_2
INFO - 16:23:18: under the inequality constraints
INFO - 16:23:18: g_2(x_2) <= 0
INFO - 16:23:18: over the design space:
INFO - 16:23:18: +------+-------------+-------+-------------+-------+
INFO - 16:23:18: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:18: +------+-------------+-------+-------------+-------+
INFO - 16:23:18: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:18: +------+-------------+-------+-------------+-------+
INFO - 16:23:18: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:18: 2%|▏ | 1/50 [00:00<00:00, 80.35 it/sec, feas=False, obj=-0.813]
INFO - 16:23:18: 4%|▍ | 2/50 [00:00<00:00, 131.68 it/sec, feas=False, obj=-0.813]
INFO - 16:23:18: 6%|▌ | 3/50 [00:00<00:00, 163.74 it/sec, feas=False, obj=-0.813]
INFO - 16:23:18: 8%|▊ | 4/50 [00:00<00:00, 185.66 it/sec, feas=False, obj=-0.813]
INFO - 16:23:18: 10%|█ | 5/50 [00:00<00:00, 201.44 it/sec, feas=False, obj=-0.813]
INFO - 16:23:18: 12%|█▏ | 6/50 [00:00<00:00, 213.95 it/sec, feas=False, obj=-0.813]
INFO - 16:23:18: 14%|█▍ | 7/50 [00:00<00:00, 223.55 it/sec, feas=False, obj=-0.813]
INFO - 16:23:18: 16%|█▌ | 8/50 [00:00<00:00, 231.69 it/sec, feas=False, obj=-0.813]
INFO - 16:23:18: 18%|█▊ | 9/50 [00:00<00:00, 238.75 it/sec, feas=False, obj=-0.813]
INFO - 16:23:18: 20%|██ | 10/50 [00:00<00:00, 245.87 it/sec, feas=False, obj=-0.813]
INFO - 16:23:18: 22%|██▏ | 11/50 [00:00<00:00, 175.17 it/sec, feas=False, obj=-0.813]
INFO - 16:23:18: 24%|██▍ | 12/50 [00:00<00:00, 181.92 it/sec, feas=False, obj=-0.813]
INFO - 16:23:18: 26%|██▌ | 13/50 [00:00<00:00, 186.99 it/sec, feas=False, obj=-0.813]
INFO - 16:23:18: 28%|██▊ | 14/50 [00:00<00:00, 192.17 it/sec, feas=False, obj=-0.813]
INFO - 16:23:18: 30%|███ | 15/50 [00:00<00:00, 197.08 it/sec, feas=False, obj=-0.813]
INFO - 16:23:18: 32%|███▏ | 16/50 [00:00<00:00, 199.44 it/sec, feas=False, obj=-0.813]
INFO - 16:23:18: 34%|███▍ | 17/50 [00:00<00:00, 204.00 it/sec, feas=False, obj=-0.813]
INFO - 16:23:18: 36%|███▌ | 18/50 [00:00<00:00, 207.76 it/sec, feas=False, obj=-0.813]
INFO - 16:23:18: 38%|███▊ | 19/50 [00:00<00:00, 211.18 it/sec, feas=False, obj=-0.813]
INFO - 16:23:18: 40%|████ | 20/50 [00:00<00:00, 169.35 it/sec, feas=False, obj=-0.813]
INFO - 16:23:18: 42%|████▏ | 21/50 [00:00<00:00, 173.46 it/sec, feas=False, obj=-0.813]
INFO - 16:23:18: 44%|████▍ | 22/50 [00:00<00:00, 176.72 it/sec, feas=False, obj=-0.813]
INFO - 16:23:18: 46%|████▌ | 23/50 [00:00<00:00, 180.02 it/sec, feas=False, obj=-0.813]
INFO - 16:23:18: 48%|████▊ | 24/50 [00:00<00:00, 180.89 it/sec, feas=False, obj=-0.813]
INFO - 16:23:18: 50%|█████ | 25/50 [00:00<00:00, 183.89 it/sec, feas=False, obj=-0.813]
INFO - 16:23:18: 52%|█████▏ | 26/50 [00:00<00:00, 186.76 it/sec, feas=False, obj=-0.813]
INFO - 16:23:18: 54%|█████▍ | 27/50 [00:00<00:00, 189.52 it/sec, feas=False, obj=-0.813]
INFO - 16:23:18: 56%|█████▌ | 28/50 [00:00<00:00, 192.24 it/sec, feas=False, obj=-0.813]
INFO - 16:23:18: 58%|█████▊ | 29/50 [00:00<00:00, 194.82 it/sec, feas=False, obj=-0.813]
INFO - 16:23:18: 60%|██████ | 30/50 [00:00<00:00, 197.32 it/sec, feas=False, obj=-0.813]
INFO - 16:23:18: 62%|██████▏ | 31/50 [00:00<00:00, 199.73 it/sec, feas=False, obj=-0.813]
INFO - 16:23:18: 64%|██████▍ | 32/50 [00:00<00:00, 201.94 it/sec, feas=False, obj=-0.813]
INFO - 16:23:18: 66%|██████▌ | 33/50 [00:00<00:00, 204.16 it/sec, feas=False, obj=-0.813]
INFO - 16:23:18: 68%|██████▊ | 34/50 [00:00<00:00, 206.28 it/sec, feas=False, obj=-0.813]
WARNING - 16:23:18: Optimization found no feasible point; the least infeasible point is selected.
INFO - 16:23:18: 70%|███████ | 35/50 [00:00<00:00, 187.82 it/sec, feas=False, obj=-0.813]
INFO - 16:23:18: Optimization result:
INFO - 16:23:18: Optimizer info:
INFO - 16:23:18: Status: 8
INFO - 16:23:18: Message: Positive directional derivative for linesearch
INFO - 16:23:18: Solution:
WARNING - 16:23:18: The solution is not feasible.
INFO - 16:23:18: Objective: -0.8130465270331335
INFO - 16:23:18: Standardized constraints:
INFO - 16:23:18: g_2 = 0.010000000000000009
INFO - 16:23:18: Design space:
INFO - 16:23:18: +------+-------------+-------+-------------+-------+
INFO - 16:23:18: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:18: +------+-------------+-------+-------------+-------+
INFO - 16:23:18: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:18: +------+-------------+-------+-------------+-------+
INFO - 16:23:18: *** End AerodynamicsScenario execution (time: 0:00:00.188301) ***
INFO - 16:23:18: *** Start StructureScenario execution ***
INFO - 16:23:18: StructureScenario
INFO - 16:23:18: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:18: MDO formulation: MDF
INFO - 16:23:18: Optimization problem:
INFO - 16:23:18: minimize 0.001*-y_4(x_1)
INFO - 16:23:18: with respect to x_1
INFO - 16:23:18: under the inequality constraints
INFO - 16:23:18: g_1(x_1) <= 0
INFO - 16:23:18: over the design space:
INFO - 16:23:18: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:18: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:18: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:18: | x_1[0] | 0.1 | 0.3998973907465287 | 0.4 | float |
INFO - 16:23:18: | x_1[1] | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:18: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:18: Solving optimization problem with algorithm SLSQP:
WARNING - 16:23:19: MDAGaussSeidel has reached its maximum number of unsuccessful iterations, but the normalized residual norm 0.0009157477359807847 is still above the tolerance 1e-06.
INFO - 16:23:19: 2%|▏ | 1/50 [00:00<00:01, 43.04 it/sec, feas=True, obj=-0.813]
INFO - 16:23:19: 4%|▍ | 2/50 [00:00<00:01, 38.02 it/sec, feas=True, obj=-0.813]
INFO - 16:23:19: 6%|▌ | 3/50 [00:00<00:01, 36.13 it/sec, feas=True, obj=-0.813]
INFO - 16:23:19: Optimization result:
INFO - 16:23:19: Optimizer info:
INFO - 16:23:19: Status: None
INFO - 16:23:19: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:19: Solution:
INFO - 16:23:19: The solution is feasible.
INFO - 16:23:19: Objective: -0.813046529195449
INFO - 16:23:19: Standardized constraints:
INFO - 16:23:19: g_1 = [-0.02507869 -0.02543826 -0.03359837 -0.04104814 -0.0470787 -0.206433
INFO - 16:23:19: -0.033567 ]
INFO - 16:23:19: Design space:
INFO - 16:23:19: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:19: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:19: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:19: | x_1[0] | 0.1 | 0.3998632171845288 | 0.4 | float |
INFO - 16:23:19: | x_1[1] | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:19: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:19: *** End StructureScenario execution (time: 0:00:00.085777) ***
INFO - 16:23:19: *** Start PropulsionScenario execution ***
INFO - 16:23:19: PropulsionScenario
INFO - 16:23:19: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:19: MDO formulation: MDF
INFO - 16:23:19: Optimization problem:
INFO - 16:23:19: minimize 0.001*-y_4(x_3)
INFO - 16:23:19: with respect to x_3
INFO - 16:23:19: under the inequality constraints
INFO - 16:23:19: g_3(x_3) <= 0
INFO - 16:23:19: over the design space:
INFO - 16:23:19: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:19: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:19: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:19: | x_3 | 0.1 | 0.2871004772038968 | 1 | float |
INFO - 16:23:19: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:19: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:19: 2%|▏ | 1/50 [00:00<00:00, 107.41 it/sec, feas=True, obj=-0.813]
INFO - 16:23:19: Optimization result:
INFO - 16:23:19: Optimizer info:
INFO - 16:23:19: Status: 8
INFO - 16:23:19: Message: Positive directional derivative for linesearch
INFO - 16:23:19: Solution:
INFO - 16:23:19: The solution is feasible.
INFO - 16:23:19: Objective: -0.813046529195449
INFO - 16:23:19: Standardized constraints:
INFO - 16:23:19: g_3 = [-7.18403708e-01 -2.81596292e-01 2.22044605e-16 -1.27460556e-01]
INFO - 16:23:19: Design space:
INFO - 16:23:19: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:19: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:19: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:19: | x_3 | 0.1 | 0.2871004772038968 | 1 | float |
INFO - 16:23:19: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:19: *** End PropulsionScenario execution (time: 0:00:00.011238) ***
INFO - 16:23:19: *** Start AerodynamicsScenario execution ***
INFO - 16:23:19: AerodynamicsScenario
INFO - 16:23:19: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:19: MDO formulation: MDF
INFO - 16:23:19: Optimization problem:
INFO - 16:23:19: minimize 0.001*-y_4(x_2)
INFO - 16:23:19: with respect to x_2
INFO - 16:23:19: under the inequality constraints
INFO - 16:23:19: g_2(x_2) <= 0
INFO - 16:23:19: over the design space:
INFO - 16:23:19: +------+-------------+-------+-------------+-------+
INFO - 16:23:19: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:19: +------+-------------+-------+-------------+-------+
INFO - 16:23:19: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:19: +------+-------------+-------+-------------+-------+
INFO - 16:23:19: Solving optimization problem with algorithm SLSQP:
WARNING - 16:23:19: Optimization found no feasible point; the least infeasible point is selected.
INFO - 16:23:19: 2%|▏ | 1/50 [00:00<00:00, 86.99 it/sec, feas=False, obj=-0.813]
INFO - 16:23:19: Optimization result:
INFO - 16:23:19: Optimizer info:
INFO - 16:23:19: Status: 8
INFO - 16:23:19: Message: Positive directional derivative for linesearch
INFO - 16:23:19: Solution:
WARNING - 16:23:19: The solution is not feasible.
INFO - 16:23:19: Objective: -0.813046529195449
INFO - 16:23:19: Standardized constraints:
INFO - 16:23:19: g_2 = 0.010000000000000009
INFO - 16:23:19: Design space:
INFO - 16:23:19: +------+-------------+-------+-------------+-------+
INFO - 16:23:19: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:19: +------+-------------+-------+-------------+-------+
INFO - 16:23:19: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:19: +------+-------------+-------+-------------+-------+
INFO - 16:23:19: *** End AerodynamicsScenario execution (time: 0:00:00.013204) ***
INFO - 16:23:19: *** Start StructureScenario execution ***
INFO - 16:23:19: StructureScenario
INFO - 16:23:19: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:19: MDO formulation: MDF
INFO - 16:23:19: Optimization problem:
INFO - 16:23:19: minimize 0.001*-y_4(x_1)
INFO - 16:23:19: with respect to x_1
INFO - 16:23:19: under the inequality constraints
INFO - 16:23:19: g_1(x_1) <= 0
INFO - 16:23:19: over the design space:
INFO - 16:23:19: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:19: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:19: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:19: | x_1[0] | 0.1 | 0.3998632171845288 | 0.4 | float |
INFO - 16:23:19: | x_1[1] | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:19: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:19: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:19: 2%|▏ | 1/50 [00:00<00:00, 101.47 it/sec, feas=True, obj=-0.813]
INFO - 16:23:19: 4%|▍ | 2/50 [00:00<00:00, 51.05 it/sec, feas=True, obj=-0.813]
INFO - 16:23:19: 6%|▌ | 3/50 [00:00<00:01, 43.53 it/sec, feas=True, obj=-0.813]
INFO - 16:23:19: Optimization result:
INFO - 16:23:19: Optimizer info:
INFO - 16:23:19: Status: None
INFO - 16:23:19: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:19: Solution:
INFO - 16:23:19: The solution is feasible.
INFO - 16:23:19: Objective: -0.8130465313558969
INFO - 16:23:19: Standardized constraints:
INFO - 16:23:19: g_1 = [-0.02508497 -0.02544267 -0.03360176 -0.04105089 -0.04708101 -0.20642651
INFO - 16:23:19: -0.03357349]
INFO - 16:23:19: Design space:
INFO - 16:23:19: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:19: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:19: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:19: | x_1[0] | 0.1 | 0.3998290583767585 | 0.4 | float |
INFO - 16:23:19: | x_1[1] | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:19: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:19: *** End StructureScenario execution (time: 0:00:00.071609) ***
INFO - 16:23:19: *** Start PropulsionScenario execution ***
INFO - 16:23:19: PropulsionScenario
INFO - 16:23:19: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:19: MDO formulation: MDF
INFO - 16:23:19: Optimization problem:
INFO - 16:23:19: minimize 0.001*-y_4(x_3)
INFO - 16:23:19: with respect to x_3
INFO - 16:23:19: under the inequality constraints
INFO - 16:23:19: g_3(x_3) <= 0
INFO - 16:23:19: over the design space:
INFO - 16:23:19: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:19: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:19: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:19: | x_3 | 0.1 | 0.2871004772038968 | 1 | float |
INFO - 16:23:19: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:19: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:19: 2%|▏ | 1/50 [00:00<00:00, 105.90 it/sec, feas=True, obj=-0.813]
INFO - 16:23:19: Optimization result:
INFO - 16:23:19: Optimizer info:
INFO - 16:23:19: Status: 8
INFO - 16:23:19: Message: Positive directional derivative for linesearch
INFO - 16:23:19: Solution:
INFO - 16:23:19: The solution is feasible.
INFO - 16:23:19: Objective: -0.8130465313558969
INFO - 16:23:19: Standardized constraints:
INFO - 16:23:19: g_3 = [-7.18403744e-01 -2.81596256e-01 2.22044605e-16 -1.27460556e-01]
INFO - 16:23:19: Design space:
INFO - 16:23:19: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:19: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:19: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:19: | x_3 | 0.1 | 0.2871004772038968 | 1 | float |
INFO - 16:23:19: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:19: *** End PropulsionScenario execution (time: 0:00:00.011430) ***
INFO - 16:23:19: *** Start AerodynamicsScenario execution ***
INFO - 16:23:19: AerodynamicsScenario
INFO - 16:23:19: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:19: MDO formulation: MDF
INFO - 16:23:19: Optimization problem:
INFO - 16:23:19: minimize 0.001*-y_4(x_2)
INFO - 16:23:19: with respect to x_2
INFO - 16:23:19: under the inequality constraints
INFO - 16:23:19: g_2(x_2) <= 0
INFO - 16:23:19: over the design space:
INFO - 16:23:19: +------+-------------+-------+-------------+-------+
INFO - 16:23:19: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:19: +------+-------------+-------+-------------+-------+
INFO - 16:23:19: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:19: +------+-------------+-------+-------------+-------+
INFO - 16:23:19: Solving optimization problem with algorithm SLSQP:
WARNING - 16:23:19: Optimization found no feasible point; the least infeasible point is selected.
INFO - 16:23:19: 2%|▏ | 1/50 [00:00<00:00, 104.50 it/sec, feas=False, obj=-0.813]
INFO - 16:23:19: Optimization result:
INFO - 16:23:19: Optimizer info:
INFO - 16:23:19: Status: 8
INFO - 16:23:19: Message: Positive directional derivative for linesearch
INFO - 16:23:19: Solution:
WARNING - 16:23:19: The solution is not feasible.
INFO - 16:23:19: Objective: -0.8130465313558969
INFO - 16:23:19: Standardized constraints:
INFO - 16:23:19: g_2 = 0.010000000000000009
INFO - 16:23:19: Design space:
INFO - 16:23:19: +------+-------------+-------+-------------+-------+
INFO - 16:23:19: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:19: +------+-------------+-------+-------------+-------+
INFO - 16:23:19: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:19: +------+-------------+-------+-------------+-------+
INFO - 16:23:19: *** End AerodynamicsScenario execution (time: 0:00:00.011114) ***
INFO - 16:23:19: *** Start StructureScenario execution ***
INFO - 16:23:19: StructureScenario
INFO - 16:23:19: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:19: MDO formulation: MDF
INFO - 16:23:19: Optimization problem:
INFO - 16:23:19: minimize 0.001*-y_4(x_1)
INFO - 16:23:19: with respect to x_1
INFO - 16:23:19: under the inequality constraints
INFO - 16:23:19: g_1(x_1) <= 0
INFO - 16:23:19: over the design space:
INFO - 16:23:19: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:19: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:19: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:19: | x_1[0] | 0.1 | 0.3998290583767585 | 0.4 | float |
INFO - 16:23:19: | x_1[1] | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:19: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:19: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:19: 2%|▏ | 1/50 [00:00<00:00, 87.02 it/sec, feas=True, obj=-0.813]
INFO - 16:23:19: 4%|▍ | 2/50 [00:00<00:00, 49.30 it/sec, feas=True, obj=-0.813]
INFO - 16:23:19: 6%|▌ | 3/50 [00:00<00:01, 42.82 it/sec, feas=True, obj=-0.813]
INFO - 16:23:19: Optimization result:
INFO - 16:23:19: Optimizer info:
INFO - 16:23:19: Status: None
INFO - 16:23:19: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:19: Solution:
INFO - 16:23:19: The solution is feasible.
INFO - 16:23:19: Objective: -0.8130465335144801
INFO - 16:23:19: Standardized constraints:
INFO - 16:23:19: g_1 = [-0.02509124 -0.02544707 -0.03360514 -0.04105363 -0.04708332 -0.20642003
INFO - 16:23:19: -0.03357997]
INFO - 16:23:19: Design space:
INFO - 16:23:19: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:19: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:19: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:19: | x_1[0] | 0.1 | 0.3997949143190079 | 0.4 | float |
INFO - 16:23:19: | x_1[1] | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:19: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:19: *** End StructureScenario execution (time: 0:00:00.072548) ***
INFO - 16:23:19: *** Start PropulsionScenario execution ***
INFO - 16:23:19: PropulsionScenario
INFO - 16:23:19: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:19: MDO formulation: MDF
INFO - 16:23:19: Optimization problem:
INFO - 16:23:19: minimize 0.001*-y_4(x_3)
INFO - 16:23:19: with respect to x_3
INFO - 16:23:19: under the inequality constraints
INFO - 16:23:19: g_3(x_3) <= 0
INFO - 16:23:19: over the design space:
INFO - 16:23:19: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:19: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:19: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:19: | x_3 | 0.1 | 0.2871004772038968 | 1 | float |
INFO - 16:23:19: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:19: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:19: 2%|▏ | 1/50 [00:00<00:00, 106.25 it/sec, feas=True, obj=-0.813]
INFO - 16:23:19: 4%|▍ | 2/50 [00:00<00:00, 66.61 it/sec, feas=True, obj=-0.813]
INFO - 16:23:19: Optimization result:
INFO - 16:23:19: Optimizer info:
INFO - 16:23:19: Status: 8
INFO - 16:23:19: Message: Positive directional derivative for linesearch
INFO - 16:23:19: Solution:
INFO - 16:23:19: The solution is feasible.
INFO - 16:23:19: Objective: -0.8130465335144808
INFO - 16:23:19: Standardized constraints:
INFO - 16:23:19: g_3 = [-7.18403780e-01 -2.81596220e-01 1.33226763e-15 -1.27460556e-01]
INFO - 16:23:19: Design space:
INFO - 16:23:19: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:19: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:19: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:19: | x_3 | 0.1 | 0.2871004772038971 | 1 | float |
INFO - 16:23:19: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:19: *** End PropulsionScenario execution (time: 0:00:00.031805) ***
INFO - 16:23:19: *** Start AerodynamicsScenario execution ***
INFO - 16:23:19: AerodynamicsScenario
INFO - 16:23:19: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:19: MDO formulation: MDF
INFO - 16:23:19: Optimization problem:
INFO - 16:23:19: minimize 0.001*-y_4(x_2)
INFO - 16:23:19: with respect to x_2
INFO - 16:23:19: under the inequality constraints
INFO - 16:23:19: g_2(x_2) <= 0
INFO - 16:23:19: over the design space:
INFO - 16:23:19: +------+-------------+-------+-------------+-------+
INFO - 16:23:19: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:19: +------+-------------+-------+-------------+-------+
INFO - 16:23:19: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:19: +------+-------------+-------+-------------+-------+
INFO - 16:23:19: Solving optimization problem with algorithm SLSQP:
WARNING - 16:23:19: Optimization found no feasible point; the least infeasible point is selected.
INFO - 16:23:19: 2%|▏ | 1/50 [00:00<00:00, 87.75 it/sec, feas=False, obj=-0.813]
INFO - 16:23:19: Optimization result:
INFO - 16:23:19: Optimizer info:
INFO - 16:23:19: Status: 8
INFO - 16:23:19: Message: Positive directional derivative for linesearch
INFO - 16:23:19: Solution:
WARNING - 16:23:19: The solution is not feasible.
INFO - 16:23:19: Objective: -0.8130465335144808
INFO - 16:23:19: Standardized constraints:
INFO - 16:23:19: g_2 = 0.010000000000000009
INFO - 16:23:19: Design space:
INFO - 16:23:19: +------+-------------+-------+-------------+-------+
INFO - 16:23:19: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:19: +------+-------------+-------+-------------+-------+
INFO - 16:23:19: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:19: +------+-------------+-------+-------------+-------+
INFO - 16:23:19: *** End AerodynamicsScenario execution (time: 0:00:00.012849) ***
INFO - 16:23:19: *** Start StructureScenario execution ***
INFO - 16:23:19: StructureScenario
INFO - 16:23:19: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:19: MDO formulation: MDF
INFO - 16:23:19: Optimization problem:
INFO - 16:23:19: minimize 0.001*-y_4(x_1)
INFO - 16:23:19: with respect to x_1
INFO - 16:23:19: under the inequality constraints
INFO - 16:23:19: g_1(x_1) <= 0
INFO - 16:23:19: over the design space:
INFO - 16:23:19: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:19: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:19: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:19: | x_1[0] | 0.1 | 0.3997949143190079 | 0.4 | float |
INFO - 16:23:19: | x_1[1] | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:19: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:19: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:19: 2%|▏ | 1/50 [00:00<00:00, 102.75 it/sec, feas=True, obj=-0.813]
INFO - 16:23:19: 4%|▍ | 2/50 [00:00<00:00, 51.38 it/sec, feas=True, obj=-0.813]
INFO - 16:23:19: 6%|▌ | 3/50 [00:00<00:01, 43.41 it/sec, feas=True, obj=-0.813]
INFO - 16:23:19: Optimization result:
INFO - 16:23:19: Optimizer info:
INFO - 16:23:19: Status: None
INFO - 16:23:19: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:19: Solution:
INFO - 16:23:19: The solution is feasible.
INFO - 16:23:19: Objective: -0.8130465356711993
INFO - 16:23:19: Standardized constraints:
INFO - 16:23:19: g_1 = [-0.02509751 -0.02545147 -0.03360852 -0.04105638 -0.04708563 -0.20641355
INFO - 16:23:19: -0.03358645]
INFO - 16:23:19: Design space:
INFO - 16:23:19: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:19: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:19: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:19: | x_1[0] | 0.1 | 0.3997607850070658 | 0.4 | float |
INFO - 16:23:19: | x_1[1] | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:19: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:19: *** End StructureScenario execution (time: 0:00:00.071443) ***
INFO - 16:23:19: *** Start PropulsionScenario execution ***
INFO - 16:23:19: PropulsionScenario
INFO - 16:23:19: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:19: MDO formulation: MDF
INFO - 16:23:19: Optimization problem:
INFO - 16:23:19: minimize 0.001*-y_4(x_3)
INFO - 16:23:19: with respect to x_3
INFO - 16:23:19: under the inequality constraints
INFO - 16:23:19: g_3(x_3) <= 0
INFO - 16:23:19: over the design space:
INFO - 16:23:19: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:19: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:19: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:19: | x_3 | 0.1 | 0.2871004772038971 | 1 | float |
INFO - 16:23:19: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:19: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:19: 2%|▏ | 1/50 [00:00<00:00, 108.88 it/sec, feas=True, obj=-0.813]
INFO - 16:23:19: Optimization result:
INFO - 16:23:19: Optimizer info:
INFO - 16:23:19: Status: 8
INFO - 16:23:19: Message: Positive directional derivative for linesearch
INFO - 16:23:19: Solution:
INFO - 16:23:19: The solution is feasible.
INFO - 16:23:19: Objective: -0.8130465356711993
INFO - 16:23:19: Standardized constraints:
INFO - 16:23:19: g_3 = [-7.18403815e-01 -2.81596185e-01 1.33226763e-15 -1.27460556e-01]
INFO - 16:23:19: Design space:
INFO - 16:23:19: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:19: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:19: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:19: | x_3 | 0.1 | 0.2871004772038971 | 1 | float |
INFO - 16:23:19: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:19: *** End PropulsionScenario execution (time: 0:00:00.010863) ***
INFO - 16:23:19: *** Start AerodynamicsScenario execution ***
INFO - 16:23:19: AerodynamicsScenario
INFO - 16:23:19: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:19: MDO formulation: MDF
INFO - 16:23:19: Optimization problem:
INFO - 16:23:19: minimize 0.001*-y_4(x_2)
INFO - 16:23:19: with respect to x_2
INFO - 16:23:19: under the inequality constraints
INFO - 16:23:19: g_2(x_2) <= 0
INFO - 16:23:19: over the design space:
INFO - 16:23:19: +------+-------------+-------+-------------+-------+
INFO - 16:23:19: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:19: +------+-------------+-------+-------------+-------+
INFO - 16:23:19: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:19: +------+-------------+-------+-------------+-------+
INFO - 16:23:19: Solving optimization problem with algorithm SLSQP:
WARNING - 16:23:19: Optimization found no feasible point; the least infeasible point is selected.
INFO - 16:23:19: 2%|▏ | 1/50 [00:00<00:00, 107.57 it/sec, feas=False, obj=-0.813]
INFO - 16:23:19: Optimization result:
INFO - 16:23:19: Optimizer info:
INFO - 16:23:19: Status: 8
INFO - 16:23:19: Message: Positive directional derivative for linesearch
INFO - 16:23:19: Solution:
WARNING - 16:23:19: The solution is not feasible.
INFO - 16:23:19: Objective: -0.8130465356711993
INFO - 16:23:19: Standardized constraints:
INFO - 16:23:19: g_2 = 0.010000000000000009
INFO - 16:23:19: Design space:
INFO - 16:23:19: +------+-------------+-------+-------------+-------+
INFO - 16:23:19: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:19: +------+-------------+-------+-------------+-------+
INFO - 16:23:19: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:19: +------+-------------+-------+-------------+-------+
INFO - 16:23:19: *** End AerodynamicsScenario execution (time: 0:00:00.010756) ***
INFO - 16:23:19: *** Start StructureScenario execution ***
INFO - 16:23:19: StructureScenario
INFO - 16:23:19: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:19: MDO formulation: MDF
INFO - 16:23:19: Optimization problem:
INFO - 16:23:19: minimize 0.001*-y_4(x_1)
INFO - 16:23:19: with respect to x_1
INFO - 16:23:19: under the inequality constraints
INFO - 16:23:19: g_1(x_1) <= 0
INFO - 16:23:19: over the design space:
INFO - 16:23:19: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:19: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:19: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:19: | x_1[0] | 0.1 | 0.3997607850070658 | 0.4 | float |
INFO - 16:23:19: | x_1[1] | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:19: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:19: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:19: 2%|▏ | 1/50 [00:00<00:00, 83.29 it/sec, feas=True, obj=-0.813]
INFO - 16:23:19: 4%|▍ | 2/50 [00:00<00:01, 47.54 it/sec, feas=True, obj=-0.813]
INFO - 16:23:19: 6%|▌ | 3/50 [00:00<00:01, 41.98 it/sec, feas=True, obj=-0.813]
INFO - 16:23:19: Optimization result:
INFO - 16:23:19: Optimizer info:
INFO - 16:23:19: Status: None
INFO - 16:23:19: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:19: Solution:
INFO - 16:23:19: The solution is feasible.
INFO - 16:23:19: Objective: -0.8130465378260557
INFO - 16:23:19: Standardized constraints:
INFO - 16:23:19: g_1 = [-0.02510378 -0.02545586 -0.0336119 -0.04105912 -0.04708794 -0.20640706
INFO - 16:23:19: -0.03359294]
INFO - 16:23:19: Design space:
INFO - 16:23:19: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:19: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:19: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:19: | x_1[0] | 0.1 | 0.3997266704367207 | 0.4 | float |
INFO - 16:23:19: | x_1[1] | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:19: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:19: *** End StructureScenario execution (time: 0:00:00.073805) ***
INFO - 16:23:19: *** Start PropulsionScenario execution ***
INFO - 16:23:19: PropulsionScenario
INFO - 16:23:19: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:19: MDO formulation: MDF
INFO - 16:23:19: Optimization problem:
INFO - 16:23:19: minimize 0.001*-y_4(x_3)
INFO - 16:23:19: with respect to x_3
INFO - 16:23:19: under the inequality constraints
INFO - 16:23:19: g_3(x_3) <= 0
INFO - 16:23:19: over the design space:
INFO - 16:23:19: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:19: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:19: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:19: | x_3 | 0.1 | 0.2871004772038971 | 1 | float |
INFO - 16:23:19: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:19: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:19: 2%|▏ | 1/50 [00:00<00:00, 108.33 it/sec, feas=True, obj=-0.813]
INFO - 16:23:19: Optimization result:
INFO - 16:23:19: Optimizer info:
INFO - 16:23:19: Status: 8
INFO - 16:23:19: Message: Positive directional derivative for linesearch
INFO - 16:23:19: Solution:
INFO - 16:23:19: The solution is feasible.
INFO - 16:23:19: Objective: -0.8130465378260557
INFO - 16:23:19: Standardized constraints:
INFO - 16:23:19: g_3 = [-7.18403851e-01 -2.81596149e-01 1.33226763e-15 -1.27460556e-01]
INFO - 16:23:19: Design space:
INFO - 16:23:19: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:19: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:19: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:19: | x_3 | 0.1 | 0.2871004772038971 | 1 | float |
INFO - 16:23:19: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:19: *** End PropulsionScenario execution (time: 0:00:00.010905) ***
INFO - 16:23:19: *** Start AerodynamicsScenario execution ***
INFO - 16:23:19: AerodynamicsScenario
INFO - 16:23:19: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:19: MDO formulation: MDF
INFO - 16:23:19: Optimization problem:
INFO - 16:23:19: minimize 0.001*-y_4(x_2)
INFO - 16:23:19: with respect to x_2
INFO - 16:23:19: under the inequality constraints
INFO - 16:23:19: g_2(x_2) <= 0
INFO - 16:23:19: over the design space:
INFO - 16:23:19: +------+-------------+-------+-------------+-------+
INFO - 16:23:19: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:19: +------+-------------+-------+-------------+-------+
INFO - 16:23:19: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:19: +------+-------------+-------+-------------+-------+
INFO - 16:23:19: Solving optimization problem with algorithm SLSQP:
WARNING - 16:23:19: Optimization found no feasible point; the least infeasible point is selected.
INFO - 16:23:19: 2%|▏ | 1/50 [00:00<00:00, 105.25 it/sec, feas=False, obj=-0.813]
INFO - 16:23:19: Optimization result:
INFO - 16:23:19: Optimizer info:
INFO - 16:23:19: Status: 8
INFO - 16:23:19: Message: Positive directional derivative for linesearch
INFO - 16:23:19: Solution:
WARNING - 16:23:19: The solution is not feasible.
INFO - 16:23:19: Objective: -0.8130465378260557
INFO - 16:23:19: Standardized constraints:
INFO - 16:23:19: g_2 = 0.010000000000000009
INFO - 16:23:19: Design space:
INFO - 16:23:19: +------+-------------+-------+-------------+-------+
INFO - 16:23:19: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:19: +------+-------------+-------+-------------+-------+
INFO - 16:23:19: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:19: +------+-------------+-------+-------------+-------+
INFO - 16:23:19: *** End AerodynamicsScenario execution (time: 0:00:00.010924) ***
INFO - 16:23:19: *** Start StructureScenario execution ***
INFO - 16:23:19: StructureScenario
INFO - 16:23:19: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:19: MDO formulation: MDF
INFO - 16:23:19: Optimization problem:
INFO - 16:23:19: minimize 0.001*-y_4(x_1)
INFO - 16:23:19: with respect to x_1
INFO - 16:23:19: under the inequality constraints
INFO - 16:23:19: g_1(x_1) <= 0
INFO - 16:23:19: over the design space:
INFO - 16:23:19: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:19: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:19: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:19: | x_1[0] | 0.1 | 0.3997266704367207 | 0.4 | float |
INFO - 16:23:19: | x_1[1] | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:19: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:19: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:19: 2%|▏ | 1/50 [00:00<00:00, 102.94 it/sec, feas=True, obj=-0.813]
INFO - 16:23:19: 4%|▍ | 2/50 [00:00<00:00, 49.92 it/sec, feas=True, obj=-0.813]
INFO - 16:23:19: 6%|▌ | 3/50 [00:00<00:01, 42.67 it/sec, feas=True, obj=-0.813]
INFO - 16:23:19: Optimization result:
INFO - 16:23:19: Optimizer info:
INFO - 16:23:19: Status: None
INFO - 16:23:19: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:19: Solution:
INFO - 16:23:19: The solution is feasible.
INFO - 16:23:19: Objective: -0.8130465399790507
INFO - 16:23:19: Standardized constraints:
INFO - 16:23:19: g_1 = [-0.02511004 -0.02546026 -0.03361528 -0.04106187 -0.04709025 -0.20640059
INFO - 16:23:19: -0.03359941]
INFO - 16:23:19: Design space:
INFO - 16:23:19: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:19: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:19: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:19: | x_1[0] | 0.1 | 0.3996925706037598 | 0.4 | float |
INFO - 16:23:19: | x_1[1] | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:19: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:19: *** End StructureScenario execution (time: 0:00:00.072741) ***
INFO - 16:23:19: *** Start PropulsionScenario execution ***
INFO - 16:23:19: PropulsionScenario
INFO - 16:23:19: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:19: MDO formulation: MDF
INFO - 16:23:19: Optimization problem:
INFO - 16:23:19: minimize 0.001*-y_4(x_3)
INFO - 16:23:19: with respect to x_3
INFO - 16:23:19: under the inequality constraints
INFO - 16:23:19: g_3(x_3) <= 0
INFO - 16:23:19: over the design space:
INFO - 16:23:19: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:19: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:19: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:19: | x_3 | 0.1 | 0.2871004772038971 | 1 | float |
INFO - 16:23:19: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:19: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:19: 2%|▏ | 1/50 [00:00<00:00, 105.38 it/sec, feas=True, obj=-0.813]
INFO - 16:23:19: 4%|▍ | 2/50 [00:00<00:00, 145.75 it/sec, feas=True, obj=-0.813]
INFO - 16:23:19: 6%|▌ | 3/50 [00:00<00:00, 169.62 it/sec, feas=True, obj=-0.813]
INFO - 16:23:19: Optimization result:
INFO - 16:23:19: Optimizer info:
INFO - 16:23:19: Status: None
INFO - 16:23:19: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:19: Solution:
INFO - 16:23:19: The solution is feasible.
INFO - 16:23:19: Objective: -0.8130465399790509
INFO - 16:23:19: Standardized constraints:
INFO - 16:23:19: g_3 = [-7.18403887e-01 -2.81596113e-01 2.88657986e-15 -1.27460556e-01]
INFO - 16:23:19: Design space:
INFO - 16:23:19: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:19: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:19: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:19: | x_3 | 0.1 | 0.2871004772038975 | 1 | float |
INFO - 16:23:19: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:19: *** End PropulsionScenario execution (time: 0:00:00.019711) ***
INFO - 16:23:19: *** Start AerodynamicsScenario execution ***
INFO - 16:23:19: AerodynamicsScenario
INFO - 16:23:19: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:19: MDO formulation: MDF
INFO - 16:23:19: Optimization problem:
INFO - 16:23:19: minimize 0.001*-y_4(x_2)
INFO - 16:23:19: with respect to x_2
INFO - 16:23:19: under the inequality constraints
INFO - 16:23:19: g_2(x_2) <= 0
INFO - 16:23:19: over the design space:
INFO - 16:23:19: +------+-------------+-------+-------------+-------+
INFO - 16:23:19: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:19: +------+-------------+-------+-------------+-------+
INFO - 16:23:19: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:19: +------+-------------+-------+-------------+-------+
INFO - 16:23:19: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:19: 2%|▏ | 1/50 [00:00<00:00, 77.30 it/sec, feas=False, obj=-0.813]
INFO - 16:23:19: 4%|▍ | 2/50 [00:00<00:00, 95.18 it/sec, feas=False, obj=-0.813]
INFO - 16:23:19: 6%|▌ | 3/50 [00:00<00:00, 128.26 it/sec, feas=False, obj=-0.813]
INFO - 16:23:19: 8%|▊ | 4/50 [00:00<00:00, 153.94 it/sec, feas=False, obj=-0.813]
INFO - 16:23:19: 10%|█ | 5/50 [00:00<00:00, 175.06 it/sec, feas=False, obj=-0.813]
INFO - 16:23:19: 12%|█▏ | 6/50 [00:00<00:00, 192.36 it/sec, feas=False, obj=-0.813]
INFO - 16:23:19: 14%|█▍ | 7/50 [00:00<00:00, 207.26 it/sec, feas=False, obj=-0.813]
INFO - 16:23:19: 16%|█▌ | 8/50 [00:00<00:00, 220.24 it/sec, feas=False, obj=-0.813]
INFO - 16:23:19: 18%|█▊ | 9/50 [00:00<00:00, 231.42 it/sec, feas=False, obj=-0.813]
INFO - 16:23:19: 20%|██ | 10/50 [00:00<00:00, 241.12 it/sec, feas=False, obj=-0.813]
INFO - 16:23:19: 22%|██▏ | 11/50 [00:00<00:00, 249.92 it/sec, feas=False, obj=-0.813]
INFO - 16:23:19: 24%|██▍ | 12/50 [00:00<00:00, 259.19 it/sec, feas=False, obj=-0.813]
INFO - 16:23:19: 26%|██▌ | 13/50 [00:00<00:00, 201.40 it/sec, feas=False, obj=-0.813]
INFO - 16:23:19: 28%|██▊ | 14/50 [00:00<00:00, 208.65 it/sec, feas=False, obj=-0.813]
INFO - 16:23:19: 30%|███ | 15/50 [00:00<00:00, 215.48 it/sec, feas=False, obj=-0.813]
INFO - 16:23:19: 32%|███▏ | 16/50 [00:00<00:00, 221.59 it/sec, feas=False, obj=-0.813]
INFO - 16:23:19: 34%|███▍ | 17/50 [00:00<00:00, 227.72 it/sec, feas=False, obj=-0.813]
INFO - 16:23:19: 36%|███▌ | 18/50 [00:00<00:00, 233.50 it/sec, feas=False, obj=-0.813]
INFO - 16:23:19: 38%|███▊ | 19/50 [00:00<00:00, 240.29 it/sec, feas=False, obj=-0.813]
WARNING - 16:23:19: Optimization found no feasible point; the least infeasible point is selected.
INFO - 16:23:19: 40%|████ | 20/50 [00:00<00:00, 204.47 it/sec, feas=False, obj=-0.813]
INFO - 16:23:19: Optimization result:
INFO - 16:23:19: Optimizer info:
INFO - 16:23:19: Status: 8
INFO - 16:23:19: Message: Positive directional derivative for linesearch
INFO - 16:23:19: Solution:
WARNING - 16:23:19: The solution is not feasible.
INFO - 16:23:19: Objective: -0.8130465399790509
INFO - 16:23:19: Standardized constraints:
INFO - 16:23:19: g_2 = 0.010000000000000009
INFO - 16:23:19: Design space:
INFO - 16:23:19: +------+-------------+-------+-------------+-------+
INFO - 16:23:19: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:19: +------+-------------+-------+-------------+-------+
INFO - 16:23:19: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:19: +------+-------------+-------+-------------+-------+
INFO - 16:23:19: *** End AerodynamicsScenario execution (time: 0:00:00.099315) ***
INFO - 16:23:19: *** Start StructureScenario execution ***
INFO - 16:23:19: StructureScenario
INFO - 16:23:19: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:19: MDO formulation: MDF
INFO - 16:23:19: Optimization problem:
INFO - 16:23:19: minimize 0.001*-y_4(x_1)
INFO - 16:23:19: with respect to x_1
INFO - 16:23:19: under the inequality constraints
INFO - 16:23:19: g_1(x_1) <= 0
INFO - 16:23:19: over the design space:
INFO - 16:23:19: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:19: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:19: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:19: | x_1[0] | 0.1 | 0.3996925706037598 | 0.4 | float |
INFO - 16:23:19: | x_1[1] | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:19: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:19: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:19: 2%|▏ | 1/50 [00:00<00:00, 82.90 it/sec, feas=True, obj=-0.813]
WARNING - 16:23:19: MDAGaussSeidel has reached its maximum number of unsuccessful iterations, but the normalized residual norm 0.0009157477359807847 is still above the tolerance 1e-06.
INFO - 16:23:19: 4%|▍ | 2/50 [00:00<00:01, 40.13 it/sec, feas=True, obj=-0.813]
INFO - 16:23:19: 6%|▌ | 3/50 [00:00<00:01, 36.03 it/sec, feas=True, obj=-0.813]
INFO - 16:23:19: Optimization result:
INFO - 16:23:19: Optimizer info:
INFO - 16:23:19: Status: None
INFO - 16:23:19: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:19: Solution:
INFO - 16:23:19: The solution is feasible.
INFO - 16:23:19: Objective: -0.8130465421301855
INFO - 16:23:19: Standardized constraints:
INFO - 16:23:19: g_1 = [-0.0251163 -0.02546465 -0.03361866 -0.04106461 -0.04709255 -0.20639411
INFO - 16:23:19: -0.03360589]
INFO - 16:23:19: Design space:
INFO - 16:23:19: +--------+-------------+------------------+-------------+-------+
INFO - 16:23:19: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:19: +--------+-------------+------------------+-------------+-------+
INFO - 16:23:19: | x_1[0] | 0.1 | 0.39965848550397 | 0.4 | float |
INFO - 16:23:19: | x_1[1] | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:19: +--------+-------------+------------------+-------------+-------+
INFO - 16:23:19: *** End StructureScenario execution (time: 0:00:00.085914) ***
INFO - 16:23:19: *** Start PropulsionScenario execution ***
INFO - 16:23:19: PropulsionScenario
INFO - 16:23:19: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:19: MDO formulation: MDF
INFO - 16:23:19: Optimization problem:
INFO - 16:23:19: minimize 0.001*-y_4(x_3)
INFO - 16:23:19: with respect to x_3
INFO - 16:23:19: under the inequality constraints
INFO - 16:23:19: g_3(x_3) <= 0
INFO - 16:23:19: over the design space:
INFO - 16:23:19: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:19: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:19: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:19: | x_3 | 0.1 | 0.2871004772038975 | 1 | float |
INFO - 16:23:19: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:19: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:19: 2%|▏ | 1/50 [00:00<00:00, 107.87 it/sec, feas=True, obj=-0.813]
INFO - 16:23:19: Optimization result:
INFO - 16:23:19: Optimizer info:
INFO - 16:23:19: Status: 8
INFO - 16:23:19: Message: Positive directional derivative for linesearch
INFO - 16:23:19: Solution:
INFO - 16:23:19: The solution is feasible.
INFO - 16:23:19: Objective: -0.8130465421301855
INFO - 16:23:19: Standardized constraints:
INFO - 16:23:19: g_3 = [-7.18403922e-01 -2.81596078e-01 2.88657986e-15 -1.27460556e-01]
INFO - 16:23:19: Design space:
INFO - 16:23:19: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:19: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:19: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:19: | x_3 | 0.1 | 0.2871004772038975 | 1 | float |
INFO - 16:23:19: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:19: *** End PropulsionScenario execution (time: 0:00:00.010976) ***
INFO - 16:23:19: *** Start AerodynamicsScenario execution ***
INFO - 16:23:19: AerodynamicsScenario
INFO - 16:23:19: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:19: MDO formulation: MDF
INFO - 16:23:19: Optimization problem:
INFO - 16:23:19: minimize 0.001*-y_4(x_2)
INFO - 16:23:19: with respect to x_2
INFO - 16:23:19: under the inequality constraints
INFO - 16:23:19: g_2(x_2) <= 0
INFO - 16:23:19: over the design space:
INFO - 16:23:19: +------+-------------+-------+-------------+-------+
INFO - 16:23:19: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:19: +------+-------------+-------+-------------+-------+
INFO - 16:23:19: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:19: +------+-------------+-------+-------------+-------+
INFO - 16:23:19: Solving optimization problem with algorithm SLSQP:
WARNING - 16:23:19: Optimization found no feasible point; the least infeasible point is selected.
INFO - 16:23:19: 2%|▏ | 1/50 [00:00<00:00, 104.34 it/sec, feas=False, obj=-0.813]
INFO - 16:23:19: Optimization result:
INFO - 16:23:19: Optimizer info:
INFO - 16:23:19: Status: 8
INFO - 16:23:19: Message: Positive directional derivative for linesearch
INFO - 16:23:19: Solution:
WARNING - 16:23:19: The solution is not feasible.
INFO - 16:23:19: Objective: -0.8130465421301855
INFO - 16:23:19: Standardized constraints:
INFO - 16:23:19: g_2 = 0.010000000000000009
INFO - 16:23:19: Design space:
INFO - 16:23:19: +------+-------------+-------+-------------+-------+
INFO - 16:23:19: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:19: +------+-------------+-------+-------------+-------+
INFO - 16:23:19: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:19: +------+-------------+-------+-------------+-------+
INFO - 16:23:19: *** End AerodynamicsScenario execution (time: 0:00:00.010998) ***
INFO - 16:23:19: *** Start StructureScenario execution ***
INFO - 16:23:19: StructureScenario
INFO - 16:23:19: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:19: MDO formulation: MDF
INFO - 16:23:19: Optimization problem:
INFO - 16:23:19: minimize 0.001*-y_4(x_1)
INFO - 16:23:19: with respect to x_1
INFO - 16:23:19: under the inequality constraints
INFO - 16:23:19: g_1(x_1) <= 0
INFO - 16:23:19: over the design space:
INFO - 16:23:19: +--------+-------------+------------------+-------------+-------+
INFO - 16:23:19: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:19: +--------+-------------+------------------+-------------+-------+
INFO - 16:23:19: | x_1[0] | 0.1 | 0.39965848550397 | 0.4 | float |
INFO - 16:23:19: | x_1[1] | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:19: +--------+-------------+------------------+-------------+-------+
INFO - 16:23:19: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:19: 2%|▏ | 1/50 [00:00<00:00, 102.45 it/sec, feas=True, obj=-0.813]
INFO - 16:23:19: 4%|▍ | 2/50 [00:00<00:00, 51.41 it/sec, feas=True, obj=-0.813]
INFO - 16:23:19: 6%|▌ | 3/50 [00:00<00:01, 43.40 it/sec, feas=True, obj=-0.813]
INFO - 16:23:19: Optimization result:
INFO - 16:23:19: Optimizer info:
INFO - 16:23:19: Status: None
INFO - 16:23:19: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:19: Solution:
INFO - 16:23:19: The solution is feasible.
INFO - 16:23:19: Objective: -0.8130465442794614
INFO - 16:23:19: Standardized constraints:
INFO - 16:23:19: g_1 = [-0.02512256 -0.02546905 -0.03362204 -0.04106735 -0.04709486 -0.20638764
INFO - 16:23:19: -0.03361236]
INFO - 16:23:19: Design space:
INFO - 16:23:19: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:19: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:19: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:19: | x_1[0] | 0.1 | 0.3996244151331375 | 0.4 | float |
INFO - 16:23:19: | x_1[1] | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:19: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:19: *** End StructureScenario execution (time: 0:00:00.071555) ***
WARNING - 16:23:19: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 0.01128577122184398 is still above the tolerance 1e-05.
INFO - 16:23:19: 3%|▎ | 3/100 [00:03<01:37, 59.63 it/min, feas=False, obj=-0.813]
INFO - 16:23:19: *** Start PropulsionScenario execution ***
INFO - 16:23:19: PropulsionScenario
INFO - 16:23:19: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:19: MDO formulation: MDF
INFO - 16:23:19: Optimization problem:
INFO - 16:23:19: minimize 0.001*-y_4(x_3)
INFO - 16:23:19: with respect to x_3
INFO - 16:23:19: under the inequality constraints
INFO - 16:23:19: g_3(x_3) <= 0
INFO - 16:23:19: over the design space:
INFO - 16:23:19: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:19: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:19: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:19: | x_3 | 0.1 | 0.2871004772038975 | 1 | float |
INFO - 16:23:19: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:19: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:19: 2%|▏ | 1/50 [00:00<00:01, 39.97 it/sec, feas=True, obj=-0.725]
INFO - 16:23:19: 4%|▍ | 2/50 [00:00<00:01, 31.34 it/sec, feas=True, obj=-0.751]
INFO - 16:23:20: 6%|▌ | 3/50 [00:00<00:01, 28.94 it/sec, feas=True, obj=-0.751]
INFO - 16:23:20: 8%|▊ | 4/50 [00:00<00:01, 31.54 it/sec, feas=True, obj=-0.751]
INFO - 16:23:20: Optimization result:
INFO - 16:23:20: Optimizer info:
INFO - 16:23:20: Status: None
INFO - 16:23:20: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:20: Solution:
INFO - 16:23:20: The solution is feasible.
INFO - 16:23:20: Objective: -0.7513757269999946
INFO - 16:23:20: Standardized constraints:
INFO - 16:23:20: g_3 = [-7.19068690e-01 -2.80931310e-01 4.44089210e-16 -1.11370139e-01]
INFO - 16:23:20: Design space:
INFO - 16:23:20: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:20: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:20: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:20: | x_3 | 0.1 | 0.3243399096603404 | 1 | float |
INFO - 16:23:20: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:20: *** End PropulsionScenario execution (time: 0:00:00.129162) ***
INFO - 16:23:20: *** Start AerodynamicsScenario execution ***
INFO - 16:23:20: AerodynamicsScenario
INFO - 16:23:20: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:20: MDO formulation: MDF
INFO - 16:23:20: Optimization problem:
INFO - 16:23:20: minimize 0.001*-y_4(x_2)
INFO - 16:23:20: with respect to x_2
INFO - 16:23:20: under the inequality constraints
INFO - 16:23:20: g_2(x_2) <= 0
INFO - 16:23:20: over the design space:
INFO - 16:23:20: +------+-------------+-------+-------------+-------+
INFO - 16:23:20: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:20: +------+-------------+-------+-------------+-------+
INFO - 16:23:20: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:20: +------+-------------+-------+-------------+-------+
INFO - 16:23:20: Solving optimization problem with algorithm SLSQP:
WARNING - 16:23:20: Optimization found no feasible point; the least infeasible point is selected.
INFO - 16:23:20: 2%|▏ | 1/50 [00:00<00:00, 89.89 it/sec, feas=False, obj=-0.751]
INFO - 16:23:20: Optimization result:
INFO - 16:23:20: Optimizer info:
INFO - 16:23:20: Status: 8
INFO - 16:23:20: Message: Positive directional derivative for linesearch
INFO - 16:23:20: Solution:
WARNING - 16:23:20: The solution is not feasible.
INFO - 16:23:20: Objective: -0.7513757269999946
INFO - 16:23:20: Standardized constraints:
INFO - 16:23:20: g_2 = 0.010000000000000009
INFO - 16:23:20: Design space:
INFO - 16:23:20: +------+-------------+-------+-------------+-------+
INFO - 16:23:20: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:20: +------+-------------+-------+-------------+-------+
INFO - 16:23:20: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:20: +------+-------------+-------+-------------+-------+
INFO - 16:23:20: *** End AerodynamicsScenario execution (time: 0:00:00.012681) ***
INFO - 16:23:20: *** Start StructureScenario execution ***
INFO - 16:23:20: StructureScenario
INFO - 16:23:20: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:20: MDO formulation: MDF
INFO - 16:23:20: Optimization problem:
INFO - 16:23:20: minimize 0.001*-y_4(x_1)
INFO - 16:23:20: with respect to x_1
INFO - 16:23:20: under the inequality constraints
INFO - 16:23:20: g_1(x_1) <= 0
INFO - 16:23:20: over the design space:
INFO - 16:23:20: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:20: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:20: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:20: | x_1[0] | 0.1 | 0.3996244151331375 | 0.4 | float |
INFO - 16:23:20: | x_1[1] | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:20: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:20: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:20: 2%|▏ | 1/50 [00:00<00:00, 95.61 it/sec, feas=True, obj=-0.751]
INFO - 16:23:20: 4%|▍ | 2/50 [00:00<00:00, 49.26 it/sec, feas=True, obj=-0.751]
INFO - 16:23:20: 6%|▌ | 3/50 [00:00<00:01, 41.39 it/sec, feas=True, obj=-0.751]
INFO - 16:23:20: Optimization result:
INFO - 16:23:20: Optimizer info:
INFO - 16:23:20: Status: None
INFO - 16:23:20: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:20: Solution:
INFO - 16:23:20: The solution is feasible.
INFO - 16:23:20: Objective: -0.7513757288743564
INFO - 16:23:20: Standardized constraints:
INFO - 16:23:20: g_1 = [-0.02512841 -0.02547315 -0.03362519 -0.04106991 -0.04709701 -0.20638159
INFO - 16:23:20: -0.03361841]
INFO - 16:23:20: Design space:
INFO - 16:23:20: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:20: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:20: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:20: | x_1[0] | 0.1 | 0.3995925984429094 | 0.4 | float |
INFO - 16:23:20: | x_1[1] | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:20: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:20: *** End StructureScenario execution (time: 0:00:00.074775) ***
INFO - 16:23:20: *** Start PropulsionScenario execution ***
INFO - 16:23:20: PropulsionScenario
INFO - 16:23:20: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:20: MDO formulation: MDF
INFO - 16:23:20: Optimization problem:
INFO - 16:23:20: minimize 0.001*-y_4(x_3)
INFO - 16:23:20: with respect to x_3
INFO - 16:23:20: under the inequality constraints
INFO - 16:23:20: g_3(x_3) <= 0
INFO - 16:23:20: over the design space:
INFO - 16:23:20: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:20: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:20: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:20: | x_3 | 0.1 | 0.3243399096603404 | 1 | float |
INFO - 16:23:20: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:20: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:20: 2%|▏ | 1/50 [00:00<00:00, 88.89 it/sec, feas=True, obj=-0.751]
INFO - 16:23:20: Optimization result:
INFO - 16:23:20: Optimizer info:
INFO - 16:23:20: Status: 8
INFO - 16:23:20: Message: Positive directional derivative for linesearch
INFO - 16:23:20: Solution:
INFO - 16:23:20: The solution is feasible.
INFO - 16:23:20: Objective: -0.7513757288743564
INFO - 16:23:20: Standardized constraints:
INFO - 16:23:20: g_3 = [-7.19068723e-01 -2.80931277e-01 4.44089210e-16 -1.11370139e-01]
INFO - 16:23:20: Design space:
INFO - 16:23:20: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:20: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:20: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:20: | x_3 | 0.1 | 0.3243399096603404 | 1 | float |
INFO - 16:23:20: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:20: *** End PropulsionScenario execution (time: 0:00:00.013224) ***
INFO - 16:23:20: *** Start AerodynamicsScenario execution ***
INFO - 16:23:20: AerodynamicsScenario
INFO - 16:23:20: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:20: MDO formulation: MDF
INFO - 16:23:20: Optimization problem:
INFO - 16:23:20: minimize 0.001*-y_4(x_2)
INFO - 16:23:20: with respect to x_2
INFO - 16:23:20: under the inequality constraints
INFO - 16:23:20: g_2(x_2) <= 0
INFO - 16:23:20: over the design space:
INFO - 16:23:20: +------+-------------+-------+-------------+-------+
INFO - 16:23:20: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:20: +------+-------------+-------+-------------+-------+
INFO - 16:23:20: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:20: +------+-------------+-------+-------------+-------+
INFO - 16:23:20: Solving optimization problem with algorithm SLSQP:
WARNING - 16:23:20: Optimization found no feasible point; the least infeasible point is selected.
INFO - 16:23:20: 2%|▏ | 1/50 [00:00<00:00, 106.81 it/sec, feas=False, obj=-0.751]
INFO - 16:23:20: Optimization result:
INFO - 16:23:20: Optimizer info:
INFO - 16:23:20: Status: 8
INFO - 16:23:20: Message: Positive directional derivative for linesearch
INFO - 16:23:20: Solution:
WARNING - 16:23:20: The solution is not feasible.
INFO - 16:23:20: Objective: -0.7513757288743564
INFO - 16:23:20: Standardized constraints:
INFO - 16:23:20: g_2 = 0.010000000000000009
INFO - 16:23:20: Design space:
INFO - 16:23:20: +------+-------------+-------+-------------+-------+
INFO - 16:23:20: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:20: +------+-------------+-------+-------------+-------+
INFO - 16:23:20: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:20: +------+-------------+-------+-------------+-------+
INFO - 16:23:20: *** End AerodynamicsScenario execution (time: 0:00:00.010951) ***
INFO - 16:23:20: *** Start StructureScenario execution ***
INFO - 16:23:20: StructureScenario
INFO - 16:23:20: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:20: MDO formulation: MDF
INFO - 16:23:20: Optimization problem:
INFO - 16:23:20: minimize 0.001*-y_4(x_1)
INFO - 16:23:20: with respect to x_1
INFO - 16:23:20: under the inequality constraints
INFO - 16:23:20: g_1(x_1) <= 0
INFO - 16:23:20: over the design space:
INFO - 16:23:20: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:20: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:20: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:20: | x_1[0] | 0.1 | 0.3995925984429094 | 0.4 | float |
INFO - 16:23:20: | x_1[1] | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:20: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:20: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:20: 2%|▏ | 1/50 [00:00<00:00, 101.48 it/sec, feas=True, obj=-0.751]
INFO - 16:23:20: 4%|▍ | 2/50 [00:00<00:00, 52.05 it/sec, feas=True, obj=-0.751]
INFO - 16:23:20: 6%|▌ | 3/50 [00:00<00:01, 43.91 it/sec, feas=True, obj=-0.751]
INFO - 16:23:20: Optimization result:
INFO - 16:23:20: Optimizer info:
INFO - 16:23:20: Status: None
INFO - 16:23:20: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:20: Solution:
INFO - 16:23:20: The solution is feasible.
INFO - 16:23:20: Objective: -0.7513757307472231
INFO - 16:23:20: Standardized constraints:
INFO - 16:23:20: g_1 = [-0.02513426 -0.02547725 -0.03362834 -0.04107247 -0.04709916 -0.20637555
INFO - 16:23:20: -0.03362445]
INFO - 16:23:20: Design space:
INFO - 16:23:20: +--------+-------------+-------------------+-------------+-------+
INFO - 16:23:20: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:20: +--------+-------------+-------------------+-------------+-------+
INFO - 16:23:20: | x_1[0] | 0.1 | 0.399560794453231 | 0.4 | float |
INFO - 16:23:20: | x_1[1] | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:20: +--------+-------------+-------------------+-------------+-------+
INFO - 16:23:20: *** End StructureScenario execution (time: 0:00:00.070859) ***
INFO - 16:23:20: *** Start PropulsionScenario execution ***
INFO - 16:23:20: PropulsionScenario
INFO - 16:23:20: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:20: MDO formulation: MDF
INFO - 16:23:20: Optimization problem:
INFO - 16:23:20: minimize 0.001*-y_4(x_3)
INFO - 16:23:20: with respect to x_3
INFO - 16:23:20: under the inequality constraints
INFO - 16:23:20: g_3(x_3) <= 0
INFO - 16:23:20: over the design space:
INFO - 16:23:20: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:20: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:20: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:20: | x_3 | 0.1 | 0.3243399096603404 | 1 | float |
INFO - 16:23:20: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:20: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:20: 2%|▏ | 1/50 [00:00<00:00, 107.65 it/sec, feas=True, obj=-0.751]
INFO - 16:23:20: 4%|▍ | 2/50 [00:00<00:00, 149.08 it/sec, feas=True, obj=-0.751]
INFO - 16:23:20: 6%|▌ | 3/50 [00:00<00:00, 88.14 it/sec, feas=True, obj=-0.751]
INFO - 16:23:20: Optimization result:
INFO - 16:23:20: Optimizer info:
INFO - 16:23:20: Status: None
INFO - 16:23:20: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:20: Solution:
INFO - 16:23:20: The solution is feasible.
INFO - 16:23:20: Objective: -0.7513757307472239
INFO - 16:23:20: Standardized constraints:
INFO - 16:23:20: g_3 = [-7.19068756e-01 -2.80931244e-01 3.10862447e-15 -1.11370139e-01]
INFO - 16:23:20: Design space:
INFO - 16:23:20: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:20: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:20: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:20: | x_3 | 0.1 | 0.3243399096603413 | 1 | float |
INFO - 16:23:20: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:20: *** End PropulsionScenario execution (time: 0:00:00.036567) ***
INFO - 16:23:20: *** Start AerodynamicsScenario execution ***
INFO - 16:23:20: AerodynamicsScenario
INFO - 16:23:20: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:20: MDO formulation: MDF
INFO - 16:23:20: Optimization problem:
INFO - 16:23:20: minimize 0.001*-y_4(x_2)
INFO - 16:23:20: with respect to x_2
INFO - 16:23:20: under the inequality constraints
INFO - 16:23:20: g_2(x_2) <= 0
INFO - 16:23:20: over the design space:
INFO - 16:23:20: +------+-------------+-------+-------------+-------+
INFO - 16:23:20: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:20: +------+-------------+-------+-------------+-------+
INFO - 16:23:20: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:20: +------+-------------+-------+-------------+-------+
INFO - 16:23:20: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:20: 2%|▏ | 1/50 [00:00<00:00, 109.23 it/sec, feas=False, obj=-0.751]
INFO - 16:23:20: 4%|▍ | 2/50 [00:00<00:00, 174.29 it/sec, feas=False, obj=-0.751]
INFO - 16:23:20: 6%|▌ | 3/50 [00:00<00:00, 214.36 it/sec, feas=False, obj=-0.751]
INFO - 16:23:20: 8%|▊ | 4/50 [00:00<00:00, 242.25 it/sec, feas=False, obj=-0.751]
INFO - 16:23:20: 10%|█ | 5/50 [00:00<00:00, 266.22 it/sec, feas=False, obj=-0.751]
INFO - 16:23:20: 12%|█▏ | 6/50 [00:00<00:00, 289.29 it/sec, feas=False, obj=-0.751]
INFO - 16:23:20: 14%|█▍ | 7/50 [00:00<00:00, 308.30 it/sec, feas=False, obj=-0.751]
INFO - 16:23:20: 16%|█▌ | 8/50 [00:00<00:00, 311.54 it/sec, feas=False, obj=-0.751]
INFO - 16:23:20: 18%|█▊ | 9/50 [00:00<00:00, 320.46 it/sec, feas=False, obj=-0.751]
INFO - 16:23:20: 20%|██ | 10/50 [00:00<00:00, 327.10 it/sec, feas=False, obj=-0.751]
INFO - 16:23:20: 22%|██▏ | 11/50 [00:00<00:00, 332.97 it/sec, feas=False, obj=-0.751]
INFO - 16:23:20: 24%|██▍ | 12/50 [00:00<00:00, 336.36 it/sec, feas=False, obj=-0.751]
INFO - 16:23:20: 26%|██▌ | 13/50 [00:00<00:00, 340.99 it/sec, feas=False, obj=-0.751]
INFO - 16:23:20: 28%|██▊ | 14/50 [00:00<00:00, 344.51 it/sec, feas=False, obj=-0.751]
INFO - 16:23:20: 30%|███ | 15/50 [00:00<00:00, 347.66 it/sec, feas=False, obj=-0.751]
INFO - 16:23:20: 32%|███▏ | 16/50 [00:00<00:00, 350.86 it/sec, feas=False, obj=-0.751]
INFO - 16:23:20: 34%|███▍ | 17/50 [00:00<00:00, 355.48 it/sec, feas=False, obj=-0.751]
INFO - 16:23:20: 36%|███▌ | 18/50 [00:00<00:00, 261.44 it/sec, feas=False, obj=-0.751]
INFO - 16:23:20: 38%|███▊ | 19/50 [00:00<00:00, 266.13 it/sec, feas=False, obj=-0.751]
INFO - 16:23:20: 40%|████ | 20/50 [00:00<00:00, 270.40 it/sec, feas=False, obj=-0.751]
INFO - 16:23:20: 42%|████▏ | 21/50 [00:00<00:00, 274.50 it/sec, feas=False, obj=-0.751]
INFO - 16:23:20: 44%|████▍ | 22/50 [00:00<00:00, 279.10 it/sec, feas=False, obj=-0.751]
INFO - 16:23:20: 46%|████▌ | 23/50 [00:00<00:00, 232.30 it/sec, feas=False, obj=-0.751]
INFO - 16:23:20: 48%|████▊ | 24/50 [00:00<00:00, 236.41 it/sec, feas=False, obj=-0.751]
INFO - 16:23:20: 50%|█████ | 25/50 [00:00<00:00, 240.34 it/sec, feas=False, obj=-0.751]
INFO - 16:23:20: 52%|█████▏ | 26/50 [00:00<00:00, 243.86 it/sec, feas=False, obj=-0.751]
INFO - 16:23:20: 54%|█████▍ | 27/50 [00:00<00:00, 247.46 it/sec, feas=False, obj=-0.751]
INFO - 16:23:20: 56%|█████▌ | 28/50 [00:00<00:00, 250.88 it/sec, feas=False, obj=-0.751]
INFO - 16:23:20: 58%|█████▊ | 29/50 [00:00<00:00, 253.99 it/sec, feas=False, obj=-0.751]
INFO - 16:23:20: 60%|██████ | 30/50 [00:00<00:00, 257.11 it/sec, feas=False, obj=-0.751]
INFO - 16:23:20: 62%|██████▏ | 31/50 [00:00<00:00, 222.55 it/sec, feas=False, obj=-0.751]
INFO - 16:23:20: 64%|██████▍ | 32/50 [00:00<00:00, 224.21 it/sec, feas=False, obj=-0.751]
INFO - 16:23:20: 66%|██████▌ | 33/50 [00:00<00:00, 227.38 it/sec, feas=False, obj=-0.751]
INFO - 16:23:20: 68%|██████▊ | 34/50 [00:00<00:00, 230.24 it/sec, feas=False, obj=-0.751]
INFO - 16:23:20: 70%|███████ | 35/50 [00:00<00:00, 232.91 it/sec, feas=False, obj=-0.751]
INFO - 16:23:20: 72%|███████▏ | 36/50 [00:00<00:00, 235.63 it/sec, feas=False, obj=-0.751]
INFO - 16:23:20: 74%|███████▍ | 37/50 [00:00<00:00, 238.26 it/sec, feas=False, obj=-0.751]
INFO - 16:23:20: 76%|███████▌ | 38/50 [00:00<00:00, 240.80 it/sec, feas=False, obj=-0.751]
INFO - 16:23:20: 78%|███████▊ | 39/50 [00:00<00:00, 243.30 it/sec, feas=False, obj=-0.751]
INFO - 16:23:20: 80%|████████ | 40/50 [00:00<00:00, 245.74 it/sec, feas=False, obj=-0.751]
INFO - 16:23:20: 82%|████████▏ | 41/50 [00:00<00:00, 248.08 it/sec, feas=False, obj=-0.751]
INFO - 16:23:20: 84%|████████▍ | 42/50 [00:00<00:00, 223.79 it/sec, feas=False, obj=-0.751]
INFO - 16:23:20: 86%|████████▌ | 43/50 [00:00<00:00, 225.45 it/sec, feas=False, obj=-0.751]
INFO - 16:23:20: 88%|████████▊ | 44/50 [00:00<00:00, 227.84 it/sec, feas=False, obj=-0.751]
INFO - 16:23:20: 90%|█████████ | 45/50 [00:00<00:00, 230.10 it/sec, feas=False, obj=-0.751]
INFO - 16:23:20: 92%|█████████▏| 46/50 [00:00<00:00, 232.26 it/sec, feas=False, obj=-0.751]
INFO - 16:23:20: 94%|█████████▍| 47/50 [00:00<00:00, 233.29 it/sec, feas=False, obj=-0.751]
INFO - 16:23:20: 96%|█████████▌| 48/50 [00:00<00:00, 235.19 it/sec, feas=False, obj=-0.751]
INFO - 16:23:20: 98%|█████████▊| 49/50 [00:00<00:00, 237.13 it/sec, feas=False, obj=-0.751]
INFO - 16:23:20: 100%|██████████| 50/50 [00:00<00:00, 239.12 it/sec, feas=False, obj=-0.751]
WARNING - 16:23:20: Optimization found no feasible point; the least infeasible point is selected.
INFO - 16:23:20: Optimization result:
INFO - 16:23:20: Optimizer info:
INFO - 16:23:20: Status: None
INFO - 16:23:20: Message: Maximum number of iterations reached. GEMSEO stopped the driver.
INFO - 16:23:20: Solution:
WARNING - 16:23:20: The solution is not feasible.
INFO - 16:23:20: Objective: -0.7513757307472239
INFO - 16:23:20: Standardized constraints:
INFO - 16:23:20: g_2 = 0.010000000000000009
INFO - 16:23:20: Design space:
INFO - 16:23:20: +------+-------------+-------+-------------+-------+
INFO - 16:23:20: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:20: +------+-------------+-------+-------------+-------+
INFO - 16:23:20: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:20: +------+-------------+-------+-------------+-------+
INFO - 16:23:20: *** End AerodynamicsScenario execution (time: 0:00:00.211914) ***
INFO - 16:23:20: *** Start StructureScenario execution ***
INFO - 16:23:20: StructureScenario
INFO - 16:23:20: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:20: MDO formulation: MDF
INFO - 16:23:20: Optimization problem:
INFO - 16:23:20: minimize 0.001*-y_4(x_1)
INFO - 16:23:20: with respect to x_1
INFO - 16:23:20: under the inequality constraints
INFO - 16:23:20: g_1(x_1) <= 0
INFO - 16:23:20: over the design space:
INFO - 16:23:20: +--------+-------------+-------------------+-------------+-------+
INFO - 16:23:20: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:20: +--------+-------------+-------------------+-------------+-------+
INFO - 16:23:20: | x_1[0] | 0.1 | 0.399560794453231 | 0.4 | float |
INFO - 16:23:20: | x_1[1] | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:20: +--------+-------------+-------------------+-------------+-------+
INFO - 16:23:20: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:20: 2%|▏ | 1/50 [00:00<00:00, 68.09 it/sec, feas=True, obj=-0.751]
INFO - 16:23:20: 4%|▍ | 2/50 [00:00<00:01, 45.46 it/sec, feas=True, obj=-0.751]
INFO - 16:23:20: 6%|▌ | 3/50 [00:00<00:01, 40.56 it/sec, feas=True, obj=-0.751]
INFO - 16:23:20: Optimization result:
INFO - 16:23:20: Optimizer info:
INFO - 16:23:20: Status: None
INFO - 16:23:20: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:20: Solution:
INFO - 16:23:20: The solution is feasible.
INFO - 16:23:20: Objective: -0.7513757326185954
INFO - 16:23:20: Standardized constraints:
INFO - 16:23:20: g_1 = [-0.0251401 -0.02548135 -0.03363149 -0.04107503 -0.04710132 -0.20636951
INFO - 16:23:20: -0.03363049]
INFO - 16:23:20: Design space:
INFO - 16:23:20: +--------+-------------+-------------------+-------------+-------+
INFO - 16:23:20: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:20: +--------+-------------+-------------------+-------------+-------+
INFO - 16:23:20: | x_1[0] | 0.1 | 0.399529003160764 | 0.4 | float |
INFO - 16:23:20: | x_1[1] | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:20: +--------+-------------+-------------------+-------------+-------+
INFO - 16:23:20: *** End StructureScenario execution (time: 0:00:00.076507) ***
INFO - 16:23:20: *** Start PropulsionScenario execution ***
INFO - 16:23:20: PropulsionScenario
INFO - 16:23:20: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:20: MDO formulation: MDF
INFO - 16:23:20: Optimization problem:
INFO - 16:23:20: minimize 0.001*-y_4(x_3)
INFO - 16:23:20: with respect to x_3
INFO - 16:23:20: under the inequality constraints
INFO - 16:23:20: g_3(x_3) <= 0
INFO - 16:23:20: over the design space:
INFO - 16:23:20: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:20: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:20: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:20: | x_3 | 0.1 | 0.3243399096603413 | 1 | float |
INFO - 16:23:20: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:20: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:20: 2%|▏ | 1/50 [00:00<00:00, 109.25 it/sec, feas=True, obj=-0.751]
INFO - 16:23:20: Optimization result:
INFO - 16:23:20: Optimizer info:
INFO - 16:23:20: Status: 8
INFO - 16:23:20: Message: Positive directional derivative for linesearch
INFO - 16:23:20: Solution:
INFO - 16:23:20: The solution is feasible.
INFO - 16:23:20: Objective: -0.7513757326185954
INFO - 16:23:20: Standardized constraints:
INFO - 16:23:20: g_3 = [-7.19068790e-01 -2.80931210e-01 3.10862447e-15 -1.11370139e-01]
INFO - 16:23:20: Design space:
INFO - 16:23:20: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:20: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:20: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:20: | x_3 | 0.1 | 0.3243399096603413 | 1 | float |
INFO - 16:23:20: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:20: *** End PropulsionScenario execution (time: 0:00:00.010960) ***
INFO - 16:23:20: *** Start AerodynamicsScenario execution ***
INFO - 16:23:20: AerodynamicsScenario
INFO - 16:23:20: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:20: MDO formulation: MDF
INFO - 16:23:20: Optimization problem:
INFO - 16:23:20: minimize 0.001*-y_4(x_2)
INFO - 16:23:20: with respect to x_2
INFO - 16:23:20: under the inequality constraints
INFO - 16:23:20: g_2(x_2) <= 0
INFO - 16:23:20: over the design space:
INFO - 16:23:20: +------+-------------+-------+-------------+-------+
INFO - 16:23:20: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:20: +------+-------------+-------+-------------+-------+
INFO - 16:23:20: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:20: +------+-------------+-------+-------------+-------+
INFO - 16:23:20: Solving optimization problem with algorithm SLSQP:
WARNING - 16:23:20: Optimization found no feasible point; the least infeasible point is selected.
INFO - 16:23:20: 2%|▏ | 1/50 [00:00<00:00, 107.67 it/sec, feas=False, obj=-0.751]
INFO - 16:23:20: Optimization result:
INFO - 16:23:20: Optimizer info:
INFO - 16:23:20: Status: 8
INFO - 16:23:20: Message: Positive directional derivative for linesearch
INFO - 16:23:20: Solution:
WARNING - 16:23:20: The solution is not feasible.
INFO - 16:23:20: Objective: -0.7513757326185954
INFO - 16:23:20: Standardized constraints:
INFO - 16:23:20: g_2 = 0.010000000000000009
INFO - 16:23:20: Design space:
INFO - 16:23:20: +------+-------------+-------+-------------+-------+
INFO - 16:23:20: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:20: +------+-------------+-------+-------------+-------+
INFO - 16:23:20: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:20: +------+-------------+-------+-------------+-------+
INFO - 16:23:20: *** End AerodynamicsScenario execution (time: 0:00:00.010732) ***
INFO - 16:23:20: *** Start StructureScenario execution ***
INFO - 16:23:20: StructureScenario
INFO - 16:23:20: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:20: MDO formulation: MDF
INFO - 16:23:20: Optimization problem:
INFO - 16:23:20: minimize 0.001*-y_4(x_1)
INFO - 16:23:20: with respect to x_1
INFO - 16:23:20: under the inequality constraints
INFO - 16:23:20: g_1(x_1) <= 0
INFO - 16:23:20: over the design space:
INFO - 16:23:20: +--------+-------------+-------------------+-------------+-------+
INFO - 16:23:20: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:20: +--------+-------------+-------------------+-------------+-------+
INFO - 16:23:20: | x_1[0] | 0.1 | 0.399529003160764 | 0.4 | float |
INFO - 16:23:20: | x_1[1] | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:20: +--------+-------------+-------------------+-------------+-------+
INFO - 16:23:20: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:20: 2%|▏ | 1/50 [00:00<00:00, 102.51 it/sec, feas=True, obj=-0.751]
INFO - 16:23:20: 4%|▍ | 2/50 [00:00<00:00, 49.80 it/sec, feas=True, obj=-0.751]
INFO - 16:23:20: 6%|▌ | 3/50 [00:00<00:01, 42.37 it/sec, feas=True, obj=-0.751]
INFO - 16:23:20: Optimization result:
INFO - 16:23:20: Optimizer info:
INFO - 16:23:20: Status: None
INFO - 16:23:20: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:20: Solution:
INFO - 16:23:20: The solution is feasible.
INFO - 16:23:20: Objective: -0.7513757344884728
INFO - 16:23:20: Standardized constraints:
INFO - 16:23:20: g_1 = [-0.02514594 -0.02548545 -0.03363464 -0.04107758 -0.04710347 -0.20636347
INFO - 16:23:20: -0.03363653]
INFO - 16:23:20: Design space:
INFO - 16:23:20: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:20: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:20: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:20: | x_1[0] | 0.1 | 0.3994972245621691 | 0.4 | float |
INFO - 16:23:20: | x_1[1] | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:20: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:20: *** End StructureScenario execution (time: 0:00:00.073313) ***
INFO - 16:23:20: *** Start PropulsionScenario execution ***
INFO - 16:23:20: PropulsionScenario
INFO - 16:23:20: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:20: MDO formulation: MDF
INFO - 16:23:20: Optimization problem:
INFO - 16:23:20: minimize 0.001*-y_4(x_3)
INFO - 16:23:20: with respect to x_3
INFO - 16:23:20: under the inequality constraints
INFO - 16:23:20: g_3(x_3) <= 0
INFO - 16:23:20: over the design space:
INFO - 16:23:20: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:20: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:20: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:20: | x_3 | 0.1 | 0.3243399096603413 | 1 | float |
INFO - 16:23:20: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:20: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:20: 2%|▏ | 1/50 [00:00<00:00, 108.33 it/sec, feas=True, obj=-0.751]
INFO - 16:23:20: 4%|▍ | 2/50 [00:00<00:00, 153.78 it/sec, feas=True, obj=-0.751]
INFO - 16:23:20: 6%|▌ | 3/50 [00:00<00:00, 89.44 it/sec, feas=True, obj=-0.751]
INFO - 16:23:20: Optimization result:
INFO - 16:23:20: Optimizer info:
INFO - 16:23:20: Status: None
INFO - 16:23:20: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:20: Solution:
INFO - 16:23:20: The solution is feasible.
INFO - 16:23:20: Objective: -0.7513757344884728
INFO - 16:23:20: Standardized constraints:
INFO - 16:23:20: g_3 = [-7.19068823e-01 -2.80931177e-01 3.10862447e-15 -1.11370139e-01]
INFO - 16:23:20: Design space:
INFO - 16:23:20: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:20: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:20: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:20: | x_3 | 0.1 | 0.3243399096603413 | 1 | float |
INFO - 16:23:20: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:20: *** End PropulsionScenario execution (time: 0:00:00.035969) ***
INFO - 16:23:20: *** Start AerodynamicsScenario execution ***
INFO - 16:23:20: AerodynamicsScenario
INFO - 16:23:20: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:20: MDO formulation: MDF
INFO - 16:23:20: Optimization problem:
INFO - 16:23:20: minimize 0.001*-y_4(x_2)
INFO - 16:23:20: with respect to x_2
INFO - 16:23:20: under the inequality constraints
INFO - 16:23:20: g_2(x_2) <= 0
INFO - 16:23:20: over the design space:
INFO - 16:23:20: +------+-------------+-------+-------------+-------+
INFO - 16:23:20: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:20: +------+-------------+-------+-------------+-------+
INFO - 16:23:20: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:20: +------+-------------+-------+-------------+-------+
INFO - 16:23:20: Solving optimization problem with algorithm SLSQP:
WARNING - 16:23:20: Optimization found no feasible point; the least infeasible point is selected.
INFO - 16:23:20: 2%|▏ | 1/50 [00:00<00:00, 79.12 it/sec, feas=False, obj=-0.751]
INFO - 16:23:20: Optimization result:
INFO - 16:23:20: Optimizer info:
INFO - 16:23:20: Status: 8
INFO - 16:23:20: Message: Positive directional derivative for linesearch
INFO - 16:23:20: Solution:
WARNING - 16:23:20: The solution is not feasible.
INFO - 16:23:20: Objective: -0.7513757344884728
INFO - 16:23:20: Standardized constraints:
INFO - 16:23:20: g_2 = 0.010000000000000009
INFO - 16:23:20: Design space:
INFO - 16:23:20: +------+-------------+-------+-------------+-------+
INFO - 16:23:20: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:20: +------+-------------+-------+-------------+-------+
INFO - 16:23:20: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:20: +------+-------------+-------+-------------+-------+
INFO - 16:23:20: *** End AerodynamicsScenario execution (time: 0:00:00.014075) ***
INFO - 16:23:20: *** Start StructureScenario execution ***
INFO - 16:23:20: StructureScenario
INFO - 16:23:20: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:20: MDO formulation: MDF
INFO - 16:23:20: Optimization problem:
INFO - 16:23:20: minimize 0.001*-y_4(x_1)
INFO - 16:23:20: with respect to x_1
INFO - 16:23:20: under the inequality constraints
INFO - 16:23:20: g_1(x_1) <= 0
INFO - 16:23:20: over the design space:
INFO - 16:23:20: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:20: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:20: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:20: | x_1[0] | 0.1 | 0.3994972245621691 | 0.4 | float |
INFO - 16:23:20: | x_1[1] | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:20: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:20: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:20: 2%|▏ | 1/50 [00:00<00:00, 101.07 it/sec, feas=True, obj=-0.751]
INFO - 16:23:20: 4%|▍ | 2/50 [00:00<00:00, 51.71 it/sec, feas=True, obj=-0.751]
INFO - 16:23:20: 6%|▌ | 3/50 [00:00<00:01, 42.63 it/sec, feas=True, obj=-0.751]
INFO - 16:23:20: Optimization result:
INFO - 16:23:20: Optimizer info:
INFO - 16:23:20: Status: None
INFO - 16:23:20: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:20: Solution:
INFO - 16:23:20: The solution is feasible.
INFO - 16:23:20: Objective: -0.7513757363568567
INFO - 16:23:20: Standardized constraints:
INFO - 16:23:20: g_1 = [-0.02515178 -0.02548954 -0.03363779 -0.04108014 -0.04710562 -0.20635744
INFO - 16:23:20: -0.03364256]
INFO - 16:23:20: Design space:
INFO - 16:23:20: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:20: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:20: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:20: | x_1[0] | 0.1 | 0.3994654586541068 | 0.4 | float |
INFO - 16:23:20: | x_1[1] | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:20: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:20: *** End StructureScenario execution (time: 0:00:00.072900) ***
INFO - 16:23:20: *** Start PropulsionScenario execution ***
INFO - 16:23:20: PropulsionScenario
INFO - 16:23:20: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:20: MDO formulation: MDF
INFO - 16:23:20: Optimization problem:
INFO - 16:23:20: minimize 0.001*-y_4(x_3)
INFO - 16:23:20: with respect to x_3
INFO - 16:23:20: under the inequality constraints
INFO - 16:23:20: g_3(x_3) <= 0
INFO - 16:23:20: over the design space:
INFO - 16:23:20: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:20: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:20: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:20: | x_3 | 0.1 | 0.3243399096603413 | 1 | float |
INFO - 16:23:20: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:20: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:20: 2%|▏ | 1/50 [00:00<00:00, 108.76 it/sec, feas=True, obj=-0.751]
INFO - 16:23:20: Optimization result:
INFO - 16:23:20: Optimizer info:
INFO - 16:23:20: Status: 8
INFO - 16:23:20: Message: Positive directional derivative for linesearch
INFO - 16:23:20: Solution:
INFO - 16:23:20: The solution is feasible.
INFO - 16:23:20: Objective: -0.7513757363568567
INFO - 16:23:20: Standardized constraints:
INFO - 16:23:20: g_3 = [-7.19068856e-01 -2.80931144e-01 3.10862447e-15 -1.11370139e-01]
INFO - 16:23:20: Design space:
INFO - 16:23:20: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:20: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:20: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:20: | x_3 | 0.1 | 0.3243399096603413 | 1 | float |
INFO - 16:23:20: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:20: *** End PropulsionScenario execution (time: 0:00:00.010943) ***
INFO - 16:23:20: *** Start AerodynamicsScenario execution ***
INFO - 16:23:20: AerodynamicsScenario
INFO - 16:23:20: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:20: MDO formulation: MDF
INFO - 16:23:20: Optimization problem:
INFO - 16:23:20: minimize 0.001*-y_4(x_2)
INFO - 16:23:20: with respect to x_2
INFO - 16:23:20: under the inequality constraints
INFO - 16:23:20: g_2(x_2) <= 0
INFO - 16:23:20: over the design space:
INFO - 16:23:20: +------+-------------+-------+-------------+-------+
INFO - 16:23:20: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:20: +------+-------------+-------+-------------+-------+
INFO - 16:23:20: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:20: +------+-------------+-------+-------------+-------+
INFO - 16:23:20: Solving optimization problem with algorithm SLSQP:
WARNING - 16:23:20: Optimization found no feasible point; the least infeasible point is selected.
INFO - 16:23:20: 2%|▏ | 1/50 [00:00<00:00, 105.53 it/sec, feas=False, obj=-0.751]
INFO - 16:23:20: Optimization result:
INFO - 16:23:20: Optimizer info:
INFO - 16:23:20: Status: 8
INFO - 16:23:20: Message: Positive directional derivative for linesearch
INFO - 16:23:20: Solution:
WARNING - 16:23:20: The solution is not feasible.
INFO - 16:23:20: Objective: -0.7513757363568567
INFO - 16:23:20: Standardized constraints:
INFO - 16:23:20: g_2 = 0.010000000000000009
INFO - 16:23:20: Design space:
INFO - 16:23:20: +------+-------------+-------+-------------+-------+
INFO - 16:23:20: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:20: +------+-------------+-------+-------------+-------+
INFO - 16:23:20: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:20: +------+-------------+-------+-------------+-------+
INFO - 16:23:20: *** End AerodynamicsScenario execution (time: 0:00:00.010874) ***
INFO - 16:23:20: *** Start StructureScenario execution ***
INFO - 16:23:20: StructureScenario
INFO - 16:23:20: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:20: MDO formulation: MDF
INFO - 16:23:20: Optimization problem:
INFO - 16:23:20: minimize 0.001*-y_4(x_1)
INFO - 16:23:20: with respect to x_1
INFO - 16:23:20: under the inequality constraints
INFO - 16:23:20: g_1(x_1) <= 0
INFO - 16:23:20: over the design space:
INFO - 16:23:20: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:20: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:20: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:20: | x_1[0] | 0.1 | 0.3994654586541068 | 0.4 | float |
INFO - 16:23:20: | x_1[1] | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:20: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:20: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:20: 2%|▏ | 1/50 [00:00<00:00, 102.08 it/sec, feas=True, obj=-0.751]
INFO - 16:23:20: 4%|▍ | 2/50 [00:00<00:00, 52.22 it/sec, feas=True, obj=-0.751]
INFO - 16:23:20: 6%|▌ | 3/50 [00:00<00:01, 43.83 it/sec, feas=True, obj=-0.751]
INFO - 16:23:20: Optimization result:
INFO - 16:23:20: Optimizer info:
INFO - 16:23:20: Status: None
INFO - 16:23:20: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:20: Solution:
INFO - 16:23:20: The solution is feasible.
INFO - 16:23:20: Objective: -0.7513757382237481
INFO - 16:23:20: Standardized constraints:
INFO - 16:23:20: g_1 = [-0.02515761 -0.02549364 -0.03364094 -0.04108269 -0.04710777 -0.2063514
INFO - 16:23:20: -0.0336486 ]
INFO - 16:23:20: Design space:
INFO - 16:23:20: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:20: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:20: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:20: | x_1[0] | 0.1 | 0.3994337054332372 | 0.4 | float |
INFO - 16:23:20: | x_1[1] | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:20: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:20: *** End StructureScenario execution (time: 0:00:00.070737) ***
INFO - 16:23:20: *** Start PropulsionScenario execution ***
INFO - 16:23:20: PropulsionScenario
INFO - 16:23:20: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:20: MDO formulation: MDF
INFO - 16:23:20: Optimization problem:
INFO - 16:23:20: minimize 0.001*-y_4(x_3)
INFO - 16:23:20: with respect to x_3
INFO - 16:23:20: under the inequality constraints
INFO - 16:23:20: g_3(x_3) <= 0
INFO - 16:23:20: over the design space:
INFO - 16:23:20: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:20: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:20: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:20: | x_3 | 0.1 | 0.3243399096603413 | 1 | float |
INFO - 16:23:20: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:20: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:20: 2%|▏ | 1/50 [00:00<00:00, 106.51 it/sec, feas=True, obj=-0.751]
INFO - 16:23:20: 4%|▍ | 2/50 [00:00<00:00, 67.57 it/sec, feas=True, obj=-0.751]
INFO - 16:23:20: 6%|▌ | 3/50 [00:00<00:00, 58.65 it/sec, feas=True, obj=-0.751]
INFO - 16:23:20: Optimization result:
INFO - 16:23:20: Optimizer info:
INFO - 16:23:20: Status: 8
INFO - 16:23:20: Message: Positive directional derivative for linesearch
INFO - 16:23:20: Solution:
INFO - 16:23:20: The solution is feasible.
INFO - 16:23:20: Objective: -0.7513757382237481
INFO - 16:23:20: Standardized constraints:
INFO - 16:23:20: g_3 = [-7.19068890e-01 -2.80931110e-01 3.10862447e-15 -1.11370139e-01]
INFO - 16:23:20: Design space:
INFO - 16:23:20: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:20: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:20: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:20: | x_3 | 0.1 | 0.3243399096603413 | 1 | float |
INFO - 16:23:20: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:20: *** End PropulsionScenario execution (time: 0:00:00.053125) ***
INFO - 16:23:20: *** Start AerodynamicsScenario execution ***
INFO - 16:23:20: AerodynamicsScenario
INFO - 16:23:20: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:20: MDO formulation: MDF
INFO - 16:23:20: Optimization problem:
INFO - 16:23:20: minimize 0.001*-y_4(x_2)
INFO - 16:23:20: with respect to x_2
INFO - 16:23:20: under the inequality constraints
INFO - 16:23:20: g_2(x_2) <= 0
INFO - 16:23:20: over the design space:
INFO - 16:23:20: +------+-------------+-------+-------------+-------+
INFO - 16:23:20: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:20: +------+-------------+-------+-------------+-------+
INFO - 16:23:20: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:20: +------+-------------+-------+-------------+-------+
INFO - 16:23:20: Solving optimization problem with algorithm SLSQP:
WARNING - 16:23:20: Optimization found no feasible point; the least infeasible point is selected.
INFO - 16:23:20: 2%|▏ | 1/50 [00:00<00:00, 79.07 it/sec, feas=False, obj=-0.751]
INFO - 16:23:20: Optimization result:
INFO - 16:23:20: Optimizer info:
INFO - 16:23:20: Status: 8
INFO - 16:23:20: Message: Positive directional derivative for linesearch
INFO - 16:23:20: Solution:
WARNING - 16:23:20: The solution is not feasible.
INFO - 16:23:20: Objective: -0.7513757382237481
INFO - 16:23:20: Standardized constraints:
INFO - 16:23:20: g_2 = 0.010000000000000009
INFO - 16:23:20: Design space:
INFO - 16:23:20: +------+-------------+-------+-------------+-------+
INFO - 16:23:20: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:20: +------+-------------+-------+-------------+-------+
INFO - 16:23:20: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:20: +------+-------------+-------+-------------+-------+
INFO - 16:23:20: *** End AerodynamicsScenario execution (time: 0:00:00.014167) ***
INFO - 16:23:20: *** Start StructureScenario execution ***
INFO - 16:23:20: StructureScenario
INFO - 16:23:20: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:20: MDO formulation: MDF
INFO - 16:23:20: Optimization problem:
INFO - 16:23:20: minimize 0.001*-y_4(x_1)
INFO - 16:23:20: with respect to x_1
INFO - 16:23:20: under the inequality constraints
INFO - 16:23:20: g_1(x_1) <= 0
INFO - 16:23:20: over the design space:
INFO - 16:23:20: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:20: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:20: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:20: | x_1[0] | 0.1 | 0.3994337054332372 | 0.4 | float |
INFO - 16:23:20: | x_1[1] | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:20: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:20: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:20: 2%|▏ | 1/50 [00:00<00:00, 84.15 it/sec, feas=True, obj=-0.751]
WARNING - 16:23:20: MDAGaussSeidel has reached its maximum number of unsuccessful iterations, but the normalized residual norm 0.0009157477359807847 is still above the tolerance 1e-06.
INFO - 16:23:21: 4%|▍ | 2/50 [00:00<00:01, 40.56 it/sec, feas=True, obj=-0.751]
WARNING - 16:23:21: MDAGaussSeidel has reached its maximum number of unsuccessful iterations, but the normalized residual norm 0.0009157477359807847 is still above the tolerance 1e-06.
INFO - 16:23:21: 6%|▌ | 3/50 [00:00<00:01, 34.61 it/sec, feas=True, obj=-0.751]
INFO - 16:23:21: Optimization result:
INFO - 16:23:21: Optimizer info:
INFO - 16:23:21: Status: None
INFO - 16:23:21: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:21: Solution:
INFO - 16:23:21: The solution is feasible.
INFO - 16:23:21: Objective: -0.7513757400891489
INFO - 16:23:21: Standardized constraints:
INFO - 16:23:21: g_1 = [-0.02516345 -0.02549773 -0.03364409 -0.04108525 -0.04710992 -0.20634537
INFO - 16:23:21: -0.03365463]
INFO - 16:23:21: Design space:
INFO - 16:23:21: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:21: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:21: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:21: | x_1[0] | 0.1 | 0.3994019648962196 | 0.4 | float |
INFO - 16:23:21: | x_1[1] | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:21: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:21: *** End StructureScenario execution (time: 0:00:00.089093) ***
INFO - 16:23:21: *** Start PropulsionScenario execution ***
INFO - 16:23:21: PropulsionScenario
INFO - 16:23:21: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:21: MDO formulation: MDF
INFO - 16:23:21: Optimization problem:
INFO - 16:23:21: minimize 0.001*-y_4(x_3)
INFO - 16:23:21: with respect to x_3
INFO - 16:23:21: under the inequality constraints
INFO - 16:23:21: g_3(x_3) <= 0
INFO - 16:23:21: over the design space:
INFO - 16:23:21: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:21: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:21: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:21: | x_3 | 0.1 | 0.3243399096603413 | 1 | float |
INFO - 16:23:21: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:21: Solving optimization problem with algorithm SLSQP:
WARNING - 16:23:21: MDAGaussSeidel has reached its maximum number of unsuccessful iterations, but the normalized residual norm 6.724932466608626e-05 is still above the tolerance 1e-06.
INFO - 16:23:21: 2%|▏ | 1/50 [00:00<00:00, 54.21 it/sec, feas=True, obj=-0.751]
INFO - 16:23:21: 4%|▍ | 2/50 [00:00<00:00, 51.66 it/sec, feas=True, obj=-0.751]
WARNING - 16:23:21: MDAGaussSeidel has reached its maximum number of unsuccessful iterations, but the normalized residual norm 6.724932466608626e-05 is still above the tolerance 1e-06.
INFO - 16:23:21: 6%|▌ | 3/50 [00:00<00:00, 58.57 it/sec, feas=True, obj=-0.751]
INFO - 16:23:21: Optimization result:
INFO - 16:23:21: Optimizer info:
INFO - 16:23:21: Status: None
INFO - 16:23:21: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:21: Solution:
INFO - 16:23:21: The solution is feasible.
INFO - 16:23:21: Objective: -0.751375740089149
INFO - 16:23:21: Standardized constraints:
INFO - 16:23:21: g_3 = [-7.19068923e-01 -2.80931077e-01 3.10862447e-15 -1.11370139e-01]
INFO - 16:23:21: Design space:
INFO - 16:23:21: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:21: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:21: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:21: | x_3 | 0.1 | 0.3243399096603413 | 1 | float |
INFO - 16:23:21: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:21: *** End PropulsionScenario execution (time: 0:00:00.053399) ***
INFO - 16:23:21: *** Start AerodynamicsScenario execution ***
INFO - 16:23:21: AerodynamicsScenario
INFO - 16:23:21: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:21: MDO formulation: MDF
INFO - 16:23:21: Optimization problem:
INFO - 16:23:21: minimize 0.001*-y_4(x_2)
INFO - 16:23:21: with respect to x_2
INFO - 16:23:21: under the inequality constraints
INFO - 16:23:21: g_2(x_2) <= 0
INFO - 16:23:21: over the design space:
INFO - 16:23:21: +------+-------------+-------+-------------+-------+
INFO - 16:23:21: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:21: +------+-------------+-------+-------------+-------+
INFO - 16:23:21: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:21: +------+-------------+-------+-------------+-------+
INFO - 16:23:21: Solving optimization problem with algorithm SLSQP:
WARNING - 16:23:21: Optimization found no feasible point; the least infeasible point is selected.
INFO - 16:23:21: 2%|▏ | 1/50 [00:00<00:00, 74.98 it/sec, feas=False, obj=-0.751]
INFO - 16:23:21: Optimization result:
INFO - 16:23:21: Optimizer info:
INFO - 16:23:21: Status: 8
INFO - 16:23:21: Message: Positive directional derivative for linesearch
INFO - 16:23:21: Solution:
WARNING - 16:23:21: The solution is not feasible.
INFO - 16:23:21: Objective: -0.7513757400891489
INFO - 16:23:21: Standardized constraints:
INFO - 16:23:21: g_2 = 0.010000000000000009
INFO - 16:23:21: Design space:
INFO - 16:23:21: +------+-------------+-------+-------------+-------+
INFO - 16:23:21: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:21: +------+-------------+-------+-------------+-------+
INFO - 16:23:21: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:21: +------+-------------+-------+-------------+-------+
INFO - 16:23:21: *** End AerodynamicsScenario execution (time: 0:00:00.014874) ***
INFO - 16:23:21: *** Start StructureScenario execution ***
INFO - 16:23:21: StructureScenario
INFO - 16:23:21: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:21: MDO formulation: MDF
INFO - 16:23:21: Optimization problem:
INFO - 16:23:21: minimize 0.001*-y_4(x_1)
INFO - 16:23:21: with respect to x_1
INFO - 16:23:21: under the inequality constraints
INFO - 16:23:21: g_1(x_1) <= 0
INFO - 16:23:21: over the design space:
INFO - 16:23:21: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:21: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:21: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:21: | x_1[0] | 0.1 | 0.3994019648962196 | 0.4 | float |
INFO - 16:23:21: | x_1[1] | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:21: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:21: Solving optimization problem with algorithm SLSQP:
WARNING - 16:23:21: MDAGaussSeidel has reached its maximum number of unsuccessful iterations, but the normalized residual norm 0.0009157477359807847 is still above the tolerance 1e-06.
INFO - 16:23:21: 2%|▏ | 1/50 [00:00<00:00, 52.36 it/sec, feas=True, obj=-0.751]
INFO - 16:23:21: 4%|▍ | 2/50 [00:00<00:01, 42.08 it/sec, feas=True, obj=-0.751]
INFO - 16:23:21: 6%|▌ | 3/50 [00:00<00:01, 39.17 it/sec, feas=True, obj=-0.751]
INFO - 16:23:21: Optimization result:
INFO - 16:23:21: Optimizer info:
INFO - 16:23:21: Status: None
INFO - 16:23:21: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:21: Solution:
INFO - 16:23:21: The solution is feasible.
INFO - 16:23:21: Objective: -0.7513757419530595
INFO - 16:23:21: Standardized constraints:
INFO - 16:23:21: g_1 = [-0.02516928 -0.02550182 -0.03364723 -0.0410878 -0.04711206 -0.20633934
INFO - 16:23:21: -0.03366066]
INFO - 16:23:21: Design space:
INFO - 16:23:21: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:21: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:21: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:21: | x_1[0] | 0.1 | 0.3993702370397127 | 0.4 | float |
INFO - 16:23:21: | x_1[1] | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:21: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:21: *** End StructureScenario execution (time: 0:00:00.079377) ***
INFO - 16:23:21: *** Start PropulsionScenario execution ***
INFO - 16:23:21: PropulsionScenario
INFO - 16:23:21: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:21: MDO formulation: MDF
INFO - 16:23:21: Optimization problem:
INFO - 16:23:21: minimize 0.001*-y_4(x_3)
INFO - 16:23:21: with respect to x_3
INFO - 16:23:21: under the inequality constraints
INFO - 16:23:21: g_3(x_3) <= 0
INFO - 16:23:21: over the design space:
INFO - 16:23:21: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:21: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:21: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:21: | x_3 | 0.1 | 0.3243399096603413 | 1 | float |
INFO - 16:23:21: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:21: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:21: 2%|▏ | 1/50 [00:00<00:00, 101.23 it/sec, feas=True, obj=-0.751]
INFO - 16:23:21: Optimization result:
INFO - 16:23:21: Optimizer info:
INFO - 16:23:21: Status: 8
INFO - 16:23:21: Message: Positive directional derivative for linesearch
INFO - 16:23:21: Solution:
INFO - 16:23:21: The solution is feasible.
INFO - 16:23:21: Objective: -0.7513757419530595
INFO - 16:23:21: Standardized constraints:
INFO - 16:23:21: g_3 = [-7.19068956e-01 -2.80931044e-01 3.10862447e-15 -1.11370139e-01]
INFO - 16:23:21: Design space:
INFO - 16:23:21: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:21: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:21: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:21: | x_3 | 0.1 | 0.3243399096603413 | 1 | float |
INFO - 16:23:21: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:21: *** End PropulsionScenario execution (time: 0:00:00.012123) ***
INFO - 16:23:21: *** Start AerodynamicsScenario execution ***
INFO - 16:23:21: AerodynamicsScenario
INFO - 16:23:21: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:21: MDO formulation: MDF
INFO - 16:23:21: Optimization problem:
INFO - 16:23:21: minimize 0.001*-y_4(x_2)
INFO - 16:23:21: with respect to x_2
INFO - 16:23:21: under the inequality constraints
INFO - 16:23:21: g_2(x_2) <= 0
INFO - 16:23:21: over the design space:
INFO - 16:23:21: +------+-------------+-------+-------------+-------+
INFO - 16:23:21: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:21: +------+-------------+-------+-------------+-------+
INFO - 16:23:21: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:21: +------+-------------+-------+-------------+-------+
INFO - 16:23:21: Solving optimization problem with algorithm SLSQP:
WARNING - 16:23:21: Optimization found no feasible point; the least infeasible point is selected.
INFO - 16:23:21: 2%|▏ | 1/50 [00:00<00:00, 99.55 it/sec, feas=False, obj=-0.751]
INFO - 16:23:21: Optimization result:
INFO - 16:23:21: Optimizer info:
INFO - 16:23:21: Status: 8
INFO - 16:23:21: Message: Positive directional derivative for linesearch
INFO - 16:23:21: Solution:
WARNING - 16:23:21: The solution is not feasible.
INFO - 16:23:21: Objective: -0.7513757419530595
INFO - 16:23:21: Standardized constraints:
INFO - 16:23:21: g_2 = 0.010000000000000009
INFO - 16:23:21: Design space:
INFO - 16:23:21: +------+-------------+-------+-------------+-------+
INFO - 16:23:21: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:21: +------+-------------+-------+-------------+-------+
INFO - 16:23:21: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:21: +------+-------------+-------+-------------+-------+
INFO - 16:23:21: *** End AerodynamicsScenario execution (time: 0:00:00.011666) ***
INFO - 16:23:21: *** Start StructureScenario execution ***
INFO - 16:23:21: StructureScenario
INFO - 16:23:21: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:21: MDO formulation: MDF
INFO - 16:23:21: Optimization problem:
INFO - 16:23:21: minimize 0.001*-y_4(x_1)
INFO - 16:23:21: with respect to x_1
INFO - 16:23:21: under the inequality constraints
INFO - 16:23:21: g_1(x_1) <= 0
INFO - 16:23:21: over the design space:
INFO - 16:23:21: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:21: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:21: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:21: | x_1[0] | 0.1 | 0.3993702370397127 | 0.4 | float |
INFO - 16:23:21: | x_1[1] | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:21: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:21: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:21: 2%|▏ | 1/50 [00:00<00:00, 76.22 it/sec, feas=True, obj=-0.751]
INFO - 16:23:21: 4%|▍ | 2/50 [00:00<00:01, 44.65 it/sec, feas=True, obj=-0.751]
INFO - 16:23:21: 6%|▌ | 3/50 [00:00<00:01, 39.73 it/sec, feas=True, obj=-0.751]
INFO - 16:23:21: Optimization result:
INFO - 16:23:21: Optimizer info:
INFO - 16:23:21: Status: None
INFO - 16:23:21: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:21: Solution:
INFO - 16:23:21: The solution is feasible.
INFO - 16:23:21: Objective: -0.7513757438154803
INFO - 16:23:21: Standardized constraints:
INFO - 16:23:21: g_1 = [-0.02517511 -0.02550591 -0.03365038 -0.04109035 -0.04711421 -0.20633332
INFO - 16:23:21: -0.03366668]
INFO - 16:23:21: Design space:
INFO - 16:23:21: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:21: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:21: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:21: | x_1[0] | 0.1 | 0.3993385218603746 | 0.4 | float |
INFO - 16:23:21: | x_1[1] | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:21: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:21: *** End StructureScenario execution (time: 0:00:00.078227) ***
INFO - 16:23:21: *** Start PropulsionScenario execution ***
INFO - 16:23:21: PropulsionScenario
INFO - 16:23:21: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:21: MDO formulation: MDF
INFO - 16:23:21: Optimization problem:
INFO - 16:23:21: minimize 0.001*-y_4(x_3)
INFO - 16:23:21: with respect to x_3
INFO - 16:23:21: under the inequality constraints
INFO - 16:23:21: g_3(x_3) <= 0
INFO - 16:23:21: over the design space:
INFO - 16:23:21: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:21: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:21: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:21: | x_3 | 0.1 | 0.3243399096603413 | 1 | float |
INFO - 16:23:21: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:21: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:21: 2%|▏ | 1/50 [00:00<00:00, 103.28 it/sec, feas=True, obj=-0.751]
INFO - 16:23:21: 4%|▍ | 2/50 [00:00<00:00, 63.91 it/sec, feas=True, obj=-0.751]
INFO - 16:23:21: Optimization result:
INFO - 16:23:21: Optimizer info:
INFO - 16:23:21: Status: 8
INFO - 16:23:21: Message: Positive directional derivative for linesearch
INFO - 16:23:21: Solution:
INFO - 16:23:21: The solution is feasible.
INFO - 16:23:21: Objective: -0.7513757438154803
INFO - 16:23:21: Standardized constraints:
INFO - 16:23:21: g_3 = [-7.19068989e-01 -2.80931011e-01 3.10862447e-15 -1.11370139e-01]
INFO - 16:23:21: Design space:
INFO - 16:23:21: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:21: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:21: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:21: | x_3 | 0.1 | 0.3243399096603413 | 1 | float |
INFO - 16:23:21: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:21: *** End PropulsionScenario execution (time: 0:00:00.033430) ***
INFO - 16:23:21: *** Start AerodynamicsScenario execution ***
INFO - 16:23:21: AerodynamicsScenario
INFO - 16:23:21: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:21: MDO formulation: MDF
INFO - 16:23:21: Optimization problem:
INFO - 16:23:21: minimize 0.001*-y_4(x_2)
INFO - 16:23:21: with respect to x_2
INFO - 16:23:21: under the inequality constraints
INFO - 16:23:21: g_2(x_2) <= 0
INFO - 16:23:21: over the design space:
INFO - 16:23:21: +------+-------------+-------+-------------+-------+
INFO - 16:23:21: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:21: +------+-------------+-------+-------------+-------+
INFO - 16:23:21: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:21: +------+-------------+-------+-------------+-------+
INFO - 16:23:21: Solving optimization problem with algorithm SLSQP:
WARNING - 16:23:21: Optimization found no feasible point; the least infeasible point is selected.
INFO - 16:23:21: 2%|▏ | 1/50 [00:00<00:00, 65.80 it/sec, feas=False, obj=-0.751]
INFO - 16:23:21: Optimization result:
INFO - 16:23:21: Optimizer info:
INFO - 16:23:21: Status: 8
INFO - 16:23:21: Message: Positive directional derivative for linesearch
INFO - 16:23:21: Solution:
WARNING - 16:23:21: The solution is not feasible.
INFO - 16:23:21: Objective: -0.7513757438154803
INFO - 16:23:21: Standardized constraints:
INFO - 16:23:21: g_2 = 0.010000000000000009
INFO - 16:23:21: Design space:
INFO - 16:23:21: +------+-------------+-------+-------------+-------+
INFO - 16:23:21: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:21: +------+-------------+-------+-------------+-------+
INFO - 16:23:21: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:21: +------+-------------+-------+-------------+-------+
INFO - 16:23:21: *** End AerodynamicsScenario execution (time: 0:00:00.016892) ***
INFO - 16:23:21: *** Start StructureScenario execution ***
INFO - 16:23:21: StructureScenario
INFO - 16:23:21: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:21: MDO formulation: MDF
INFO - 16:23:21: Optimization problem:
INFO - 16:23:21: minimize 0.001*-y_4(x_1)
INFO - 16:23:21: with respect to x_1
INFO - 16:23:21: under the inequality constraints
INFO - 16:23:21: g_1(x_1) <= 0
INFO - 16:23:21: over the design space:
INFO - 16:23:21: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:21: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:21: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:21: | x_1[0] | 0.1 | 0.3993385218603746 | 0.4 | float |
INFO - 16:23:21: | x_1[1] | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:21: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:21: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:21: 2%|▏ | 1/50 [00:00<00:00, 98.54 it/sec, feas=True, obj=-0.751]
INFO - 16:23:21: 4%|▍ | 2/50 [00:00<00:00, 49.05 it/sec, feas=True, obj=-0.751]
WARNING - 16:23:21: MDAGaussSeidel has reached its maximum number of unsuccessful iterations, but the normalized residual norm 0.0009157477359807847 is still above the tolerance 1e-06.
INFO - 16:23:21: 6%|▌ | 3/50 [00:00<00:01, 37.42 it/sec, feas=True, obj=-0.751]
INFO - 16:23:21: Optimization result:
INFO - 16:23:21: Optimizer info:
INFO - 16:23:21: Status: None
INFO - 16:23:21: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:21: Solution:
INFO - 16:23:21: The solution is feasible.
INFO - 16:23:21: Objective: -0.7513757456764137
INFO - 16:23:21: Standardized constraints:
INFO - 16:23:21: g_1 = [-0.02518093 -0.02551 -0.03365352 -0.0410929 -0.04711636 -0.20632729
INFO - 16:23:21: -0.03367271]
INFO - 16:23:21: Design space:
INFO - 16:23:21: +--------+-------------+-------------------+-------------+-------+
INFO - 16:23:21: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:21: +--------+-------------+-------------------+-------------+-------+
INFO - 16:23:21: | x_1[0] | 0.1 | 0.399306819354863 | 0.4 | float |
INFO - 16:23:21: | x_1[1] | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:21: +--------+-------------+-------------------+-------------+-------+
INFO - 16:23:21: *** End StructureScenario execution (time: 0:00:00.082709) ***
INFO - 16:23:21: *** Start PropulsionScenario execution ***
INFO - 16:23:21: PropulsionScenario
INFO - 16:23:21: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:21: MDO formulation: MDF
INFO - 16:23:21: Optimization problem:
INFO - 16:23:21: minimize 0.001*-y_4(x_3)
INFO - 16:23:21: with respect to x_3
INFO - 16:23:21: under the inequality constraints
INFO - 16:23:21: g_3(x_3) <= 0
INFO - 16:23:21: over the design space:
INFO - 16:23:21: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:21: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:21: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:21: | x_3 | 0.1 | 0.3243399096603413 | 1 | float |
INFO - 16:23:21: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:21: Solving optimization problem with algorithm SLSQP:
WARNING - 16:23:21: MDAGaussSeidel has reached its maximum number of unsuccessful iterations, but the normalized residual norm 6.724932466608626e-05 is still above the tolerance 1e-06.
INFO - 16:23:21: 2%|▏ | 1/50 [00:00<00:00, 52.04 it/sec, feas=True, obj=-0.751]
INFO - 16:23:21: 4%|▍ | 2/50 [00:00<00:00, 85.43 it/sec, feas=True, obj=-0.751]
INFO - 16:23:21: 6%|▌ | 3/50 [00:00<00:00, 109.13 it/sec, feas=True, obj=-0.751]
INFO - 16:23:21: Optimization result:
INFO - 16:23:21: Optimizer info:
INFO - 16:23:21: Status: None
INFO - 16:23:21: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:21: Solution:
INFO - 16:23:21: The solution is feasible.
INFO - 16:23:21: Objective: -0.7513757456764136
INFO - 16:23:21: Standardized constraints:
INFO - 16:23:21: g_3 = [-7.19069023e-01 -2.80930977e-01 3.10862447e-15 -1.11370139e-01]
INFO - 16:23:21: Design space:
INFO - 16:23:21: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:21: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:21: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:21: | x_3 | 0.1 | 0.3243399096603413 | 1 | float |
INFO - 16:23:21: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:21: *** End PropulsionScenario execution (time: 0:00:00.029928) ***
INFO - 16:23:21: *** Start AerodynamicsScenario execution ***
INFO - 16:23:21: AerodynamicsScenario
INFO - 16:23:21: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:21: MDO formulation: MDF
INFO - 16:23:21: Optimization problem:
INFO - 16:23:21: minimize 0.001*-y_4(x_2)
INFO - 16:23:21: with respect to x_2
INFO - 16:23:21: under the inequality constraints
INFO - 16:23:21: g_2(x_2) <= 0
INFO - 16:23:21: over the design space:
INFO - 16:23:21: +------+-------------+-------+-------------+-------+
INFO - 16:23:21: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:21: +------+-------------+-------+-------------+-------+
INFO - 16:23:21: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:21: +------+-------------+-------+-------------+-------+
INFO - 16:23:21: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:21: 2%|▏ | 1/50 [00:00<00:00, 78.13 it/sec, feas=False, obj=-0.751]
INFO - 16:23:21: 4%|▍ | 2/50 [00:00<00:00, 124.68 it/sec, feas=False, obj=-0.751]
INFO - 16:23:21: 6%|▌ | 3/50 [00:00<00:00, 155.84 it/sec, feas=False, obj=-0.751]
INFO - 16:23:21: 8%|▊ | 4/50 [00:00<00:00, 178.22 it/sec, feas=False, obj=-0.751]
INFO - 16:23:21: 10%|█ | 5/50 [00:00<00:00, 195.77 it/sec, feas=False, obj=-0.751]
INFO - 16:23:21: 12%|█▏ | 6/50 [00:00<00:00, 210.49 it/sec, feas=False, obj=-0.751]
INFO - 16:23:21: 14%|█▍ | 7/50 [00:00<00:00, 221.64 it/sec, feas=False, obj=-0.751]
INFO - 16:23:21: 16%|█▌ | 8/50 [00:00<00:00, 229.95 it/sec, feas=False, obj=-0.751]
WARNING - 16:23:21: Optimization found no feasible point; the least infeasible point is selected.
INFO - 16:23:21: 18%|█▊ | 9/50 [00:00<00:00, 190.03 it/sec, feas=False, obj=-0.751]
INFO - 16:23:21: Optimization result:
INFO - 16:23:21: Optimizer info:
INFO - 16:23:21: Status: 8
INFO - 16:23:21: Message: Positive directional derivative for linesearch
INFO - 16:23:21: Solution:
WARNING - 16:23:21: The solution is not feasible.
INFO - 16:23:21: Objective: -0.7513757456764136
INFO - 16:23:21: Standardized constraints:
INFO - 16:23:21: g_2 = 0.010000000000000009
INFO - 16:23:21: Design space:
INFO - 16:23:21: +------+-------------+-------+-------------+-------+
INFO - 16:23:21: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:21: +------+-------------+-------+-------------+-------+
INFO - 16:23:21: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:21: +------+-------------+-------+-------------+-------+
INFO - 16:23:21: *** End AerodynamicsScenario execution (time: 0:00:00.048980) ***
INFO - 16:23:21: *** Start StructureScenario execution ***
INFO - 16:23:21: StructureScenario
INFO - 16:23:21: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:21: MDO formulation: MDF
INFO - 16:23:21: Optimization problem:
INFO - 16:23:21: minimize 0.001*-y_4(x_1)
INFO - 16:23:21: with respect to x_1
INFO - 16:23:21: under the inequality constraints
INFO - 16:23:21: g_1(x_1) <= 0
INFO - 16:23:21: over the design space:
INFO - 16:23:21: +--------+-------------+-------------------+-------------+-------+
INFO - 16:23:21: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:21: +--------+-------------+-------------------+-------------+-------+
INFO - 16:23:21: | x_1[0] | 0.1 | 0.399306819354863 | 0.4 | float |
INFO - 16:23:21: | x_1[1] | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:21: +--------+-------------+-------------------+-------------+-------+
INFO - 16:23:21: Solving optimization problem with algorithm SLSQP:
WARNING - 16:23:21: MDAGaussSeidel has reached its maximum number of unsuccessful iterations, but the normalized residual norm 0.0009157477359807847 is still above the tolerance 1e-06.
INFO - 16:23:21: 2%|▏ | 1/50 [00:00<00:01, 48.75 it/sec, feas=True, obj=-0.751]
INFO - 16:23:21: 4%|▍ | 2/50 [00:00<00:01, 39.96 it/sec, feas=True, obj=-0.751]
INFO - 16:23:21: 6%|▌ | 3/50 [00:00<00:01, 37.23 it/sec, feas=True, obj=-0.751]
INFO - 16:23:21: Optimization result:
INFO - 16:23:21: Optimizer info:
INFO - 16:23:21: Status: None
INFO - 16:23:21: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:21: Solution:
INFO - 16:23:21: The solution is feasible.
INFO - 16:23:21: Objective: -0.7513757475358592
INFO - 16:23:21: Standardized constraints:
INFO - 16:23:21: g_1 = [-0.02518676 -0.02551409 -0.03365666 -0.04109546 -0.0471185 -0.20632127
INFO - 16:23:21: -0.03367873]
INFO - 16:23:21: Design space:
INFO - 16:23:21: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:21: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:21: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:21: | x_1[0] | 0.1 | 0.3992751295198352 | 0.4 | float |
INFO - 16:23:21: | x_1[1] | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:21: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:21: *** End StructureScenario execution (time: 0:00:00.083320) ***
WARNING - 16:23:21: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 0.01050114956139681 is still above the tolerance 1e-05.
INFO - 16:23:21: 4%|▍ | 4/100 [00:04<01:53, 50.66 it/min, feas=False, obj=-0.751]
INFO - 16:23:21: *** Start PropulsionScenario execution ***
INFO - 16:23:21: PropulsionScenario
INFO - 16:23:21: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:21: MDO formulation: MDF
INFO - 16:23:21: Optimization problem:
INFO - 16:23:21: minimize 0.001*-y_4(x_3)
INFO - 16:23:21: with respect to x_3
INFO - 16:23:21: under the inequality constraints
INFO - 16:23:21: g_3(x_3) <= 0
INFO - 16:23:21: over the design space:
INFO - 16:23:21: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:21: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:21: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:21: | x_3 | 0.1 | 0.3243399096603413 | 1 | float |
INFO - 16:23:21: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:21: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:21: 2%|▏ | 1/50 [00:00<00:01, 37.59 it/sec, feas=False, obj=-0.75]
INFO - 16:23:21: 4%|▍ | 2/50 [00:00<00:01, 38.14 it/sec, feas=True, obj=-0.734]
INFO - 16:23:21: 6%|▌ | 3/50 [00:00<00:01, 32.08 it/sec, feas=False, obj=-0.748]
WARNING - 16:23:21: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 6.724932466608626e-05 is still above the tolerance 1e-06.
INFO - 16:23:21: 8%|▊ | 4/50 [00:00<00:01, 32.35 it/sec, feas=True, obj=-0.734]
INFO - 16:23:21: 10%|█ | 5/50 [00:00<00:01, 30.11 it/sec, feas=False, obj=-0.743]
INFO - 16:23:21: 12%|█▏ | 6/50 [00:00<00:01, 29.04 it/sec, feas=False, obj=-0.742]
WARNING - 16:23:21: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 6.724932466608626e-05 is still above the tolerance 1e-06.
INFO - 16:23:21: 14%|█▍ | 7/50 [00:00<00:01, 29.55 it/sec, feas=True, obj=-0.734]
INFO - 16:23:21: 16%|█▌ | 8/50 [00:00<00:01, 28.68 it/sec, feas=False, obj=-0.741]
INFO - 16:23:21: 18%|█▊ | 9/50 [00:00<00:01, 29.50 it/sec, feas=True, obj=-0.734]
WARNING - 16:23:21: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 0.00013449864933217252 is still above the tolerance 1e-06.
INFO - 16:23:21: 20%|██ | 10/50 [00:00<00:01, 29.80 it/sec, feas=False, obj=-0.741]
INFO - 16:23:22: 22%|██▏ | 11/50 [00:00<00:01, 29.20 it/sec, feas=False, obj=-0.741]
WARNING - 16:23:22: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 6.724932466608626e-05 is still above the tolerance 1e-06.
INFO - 16:23:22: 24%|██▍ | 12/50 [00:00<00:01, 29.47 it/sec, feas=False, obj=-0.741]
INFO - 16:23:22: 26%|██▌ | 13/50 [00:00<00:01, 28.93 it/sec, feas=False, obj=-0.741]
INFO - 16:23:22: 28%|██▊ | 14/50 [00:00<00:01, 29.45 it/sec, feas=False, obj=-0.74]
WARNING - 16:23:22: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 6.724932466608626e-05 is still above the tolerance 1e-06.
INFO - 16:23:22: 30%|███ | 15/50 [00:00<00:01, 28.72 it/sec, feas=False, obj=-0.741]
INFO - 16:23:22: 32%|███▏ | 16/50 [00:00<00:01, 29.27 it/sec, feas=False, obj=-0.74]
WARNING - 16:23:22: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 6.724932466608626e-05 is still above the tolerance 1e-06.
INFO - 16:23:22: 34%|███▍ | 17/50 [00:00<00:01, 29.47 it/sec, feas=False, obj=-0.741]
INFO - 16:23:22: 36%|███▌ | 18/50 [00:00<00:01, 29.14 it/sec, feas=False, obj=-0.741]
WARNING - 16:23:22: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 6.724932466608626e-05 is still above the tolerance 1e-06.
INFO - 16:23:22: 38%|███▊ | 19/50 [00:00<00:01, 29.34 it/sec, feas=False, obj=-0.74]
INFO - 16:23:22: 40%|████ | 20/50 [00:00<00:01, 29.77 it/sec, feas=False, obj=-0.741]
INFO - 16:23:22: 42%|████▏ | 21/50 [00:00<00:00, 30.19 it/sec, feas=False, obj=-0.741]
INFO - 16:23:22: 44%|████▍ | 22/50 [00:00<00:00, 29.91 it/sec, feas=False, obj=-0.741]
INFO - 16:23:22: 46%|████▌ | 23/50 [00:00<00:00, 30.29 it/sec, feas=False, obj=-0.74]
INFO - 16:23:22: 48%|████▊ | 24/50 [00:00<00:00, 30.59 it/sec, feas=False, obj=-0.741]
INFO - 16:23:22: 50%|█████ | 25/50 [00:00<00:00, 30.87 it/sec, feas=False, obj=-0.741]
INFO - 16:23:22: 52%|█████▏ | 26/50 [00:00<00:00, 30.59 it/sec, feas=False, obj=-0.741]
INFO - 16:23:22: 54%|█████▍ | 27/50 [00:00<00:00, 30.90 it/sec, feas=False, obj=-0.74]
INFO - 16:23:22: 56%|█████▌ | 28/50 [00:00<00:00, 31.20 it/sec, feas=False, obj=-0.741]
INFO - 16:23:22: 58%|█████▊ | 29/50 [00:00<00:00, 31.48 it/sec, feas=False, obj=-0.741]
INFO - 16:23:22: 60%|██████ | 30/50 [00:00<00:00, 31.22 it/sec, feas=False, obj=-0.741]
INFO - 16:23:22: 62%|██████▏ | 31/50 [00:00<00:00, 31.38 it/sec, feas=True, obj=-0.734]
WARNING - 16:23:22: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 6.724932466608626e-05 is still above the tolerance 1e-06.
INFO - 16:23:22: 64%|██████▍ | 32/50 [00:01<00:00, 31.45 it/sec, feas=False, obj=-0.74]
INFO - 16:23:22: 66%|██████▌ | 33/50 [00:01<00:00, 31.68 it/sec, feas=False, obj=-0.741]
INFO - 16:23:22: 68%|██████▊ | 34/50 [00:01<00:00, 31.90 it/sec, feas=False, obj=-0.741]
WARNING - 16:23:22: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 6.724932466608626e-05 is still above the tolerance 1e-06.
INFO - 16:23:22: 70%|███████ | 35/50 [00:01<00:00, 31.97 it/sec, feas=False, obj=-0.741]
INFO - 16:23:22: 72%|███████▏ | 36/50 [00:01<00:00, 31.73 it/sec, feas=False, obj=-0.741]
INFO - 16:23:22: 74%|███████▍ | 37/50 [00:01<00:00, 31.84 it/sec, feas=False, obj=-0.74]
INFO - 16:23:22: 76%|███████▌ | 38/50 [00:01<00:00, 32.04 it/sec, feas=False, obj=-0.741]
INFO - 16:23:22: 78%|███████▊ | 39/50 [00:01<00:00, 32.20 it/sec, feas=False, obj=-0.741]
INFO - 16:23:22: 80%|████████ | 40/50 [00:01<00:00, 32.38 it/sec, feas=False, obj=-0.741]
INFO - 16:23:22: 82%|████████▏ | 41/50 [00:01<00:00, 32.12 it/sec, feas=False, obj=-0.741]
INFO - 16:23:22: 84%|████████▍ | 42/50 [00:01<00:00, 32.30 it/sec, feas=False, obj=-0.74]
INFO - 16:23:22: 86%|████████▌ | 43/50 [00:01<00:00, 32.48 it/sec, feas=False, obj=-0.741]
INFO - 16:23:22: 88%|████████▊ | 44/50 [00:01<00:00, 32.65 it/sec, feas=False, obj=-0.741]
INFO - 16:23:23: 90%|█████████ | 45/50 [00:01<00:00, 32.82 it/sec, feas=False, obj=-0.741]
INFO - 16:23:23: 92%|█████████▏| 46/50 [00:01<00:00, 32.61 it/sec, feas=False, obj=-0.741]
INFO - 16:23:23: 94%|█████████▍| 47/50 [00:01<00:00, 32.76 it/sec, feas=False, obj=-0.74]
INFO - 16:23:23: 96%|█████████▌| 48/50 [00:01<00:00, 32.91 it/sec, feas=False, obj=-0.741]
INFO - 16:23:23: 98%|█████████▊| 49/50 [00:01<00:00, 33.05 it/sec, feas=False, obj=-0.741]
INFO - 16:23:23: 100%|██████████| 50/50 [00:01<00:00, 33.20 it/sec, feas=False, obj=-0.741]
INFO - 16:23:23: Optimization result:
INFO - 16:23:23: Optimizer info:
INFO - 16:23:23: Status: None
INFO - 16:23:23: Message: Maximum number of iterations reached. GEMSEO stopped the driver.
INFO - 16:23:23: Solution:
INFO - 16:23:23: The solution is feasible.
INFO - 16:23:23: Objective: -0.733809832534251
INFO - 16:23:23: Standardized constraints:
INFO - 16:23:23: g_3 = [-7.18105100e-01 -2.81894900e-01 2.22044605e-16 -1.27460556e-01]
INFO - 16:23:23: Design space:
INFO - 16:23:23: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:23: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:23: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:23: | x_3 | 0.1 | 0.2871004772038968 | 1 | float |
INFO - 16:23:23: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:23: *** End PropulsionScenario execution (time: 0:00:01.509051) ***
INFO - 16:23:23: *** Start AerodynamicsScenario execution ***
INFO - 16:23:23: AerodynamicsScenario
INFO - 16:23:23: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:23: MDO formulation: MDF
INFO - 16:23:23: Optimization problem:
INFO - 16:23:23: minimize 0.001*-y_4(x_2)
INFO - 16:23:23: with respect to x_2
INFO - 16:23:23: under the inequality constraints
INFO - 16:23:23: g_2(x_2) <= 0
INFO - 16:23:23: over the design space:
INFO - 16:23:23: +------+-------------+-------+-------------+-------+
INFO - 16:23:23: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:23: +------+-------------+-------+-------------+-------+
INFO - 16:23:23: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:23: +------+-------------+-------+-------------+-------+
INFO - 16:23:23: Solving optimization problem with algorithm SLSQP:
WARNING - 16:23:23: Optimization found no feasible point; the least infeasible point is selected.
INFO - 16:23:23: 2%|▏ | 1/50 [00:00<00:00, 73.84 it/sec, feas=False, obj=-0.734]
INFO - 16:23:23: Optimization result:
INFO - 16:23:23: Optimizer info:
INFO - 16:23:23: Status: 8
INFO - 16:23:23: Message: Positive directional derivative for linesearch
INFO - 16:23:23: Solution:
WARNING - 16:23:23: The solution is not feasible.
INFO - 16:23:23: Objective: -0.733809832534251
INFO - 16:23:23: Standardized constraints:
INFO - 16:23:23: g_2 = 0.010000000000000009
INFO - 16:23:23: Design space:
INFO - 16:23:23: +------+-------------+-------+-------------+-------+
INFO - 16:23:23: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:23: +------+-------------+-------+-------------+-------+
INFO - 16:23:23: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:23: +------+-------------+-------+-------------+-------+
INFO - 16:23:23: *** End AerodynamicsScenario execution (time: 0:00:00.015474) ***
INFO - 16:23:23: *** Start StructureScenario execution ***
INFO - 16:23:23: StructureScenario
INFO - 16:23:23: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:23: MDO formulation: MDF
INFO - 16:23:23: Optimization problem:
INFO - 16:23:23: minimize 0.001*-y_4(x_1)
INFO - 16:23:23: with respect to x_1
INFO - 16:23:23: under the inequality constraints
INFO - 16:23:23: g_1(x_1) <= 0
INFO - 16:23:23: over the design space:
INFO - 16:23:23: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:23: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:23: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:23: | x_1[0] | 0.1 | 0.3992751295198352 | 0.4 | float |
INFO - 16:23:23: | x_1[1] | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:23: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:23: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:23: 2%|▏ | 1/50 [00:00<00:00, 95.45 it/sec, feas=False, obj=-0.734]
INFO - 16:23:23: 4%|▍ | 2/50 [00:00<00:01, 43.04 it/sec, feas=True, obj=-0.725]
INFO - 16:23:23: 6%|▌ | 3/50 [00:00<00:01, 36.71 it/sec, feas=True, obj=-0.725]
INFO - 16:23:23: 8%|▊ | 4/50 [00:00<00:01, 33.80 it/sec, feas=True, obj=-0.728]
INFO - 16:23:23: 10%|█ | 5/50 [00:00<00:01, 31.93 it/sec, feas=True, obj=-0.734]
WARNING - 16:23:23: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 0.0009157477359807847 is still above the tolerance 1e-06.
INFO - 16:23:23: 12%|█▏ | 6/50 [00:00<00:01, 29.54 it/sec, feas=True, obj=-0.734]
INFO - 16:23:23: 14%|█▍ | 7/50 [00:00<00:01, 29.10 it/sec, feas=True, obj=-0.734]
INFO - 16:23:23: 16%|█▌ | 8/50 [00:00<00:01, 28.93 it/sec, feas=True, obj=-0.734]
INFO - 16:23:23: 18%|█▊ | 9/50 [00:00<00:01, 28.76 it/sec, feas=True, obj=-0.734]
INFO - 16:23:23: 20%|██ | 10/50 [00:00<00:01, 28.55 it/sec, feas=True, obj=-0.734]
INFO - 16:23:23: 22%|██▏ | 11/50 [00:00<00:01, 29.62 it/sec, feas=True, obj=-0.734]
INFO - 16:23:23: 24%|██▍ | 12/50 [00:00<00:01, 30.55 it/sec, feas=True, obj=-0.734]
INFO - 16:23:23: Optimization result:
INFO - 16:23:23: Optimizer info:
INFO - 16:23:23: Status: None
INFO - 16:23:23: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:23: Solution:
INFO - 16:23:23: The solution is feasible.
INFO - 16:23:23: Objective: -0.7339139488504138
INFO - 16:23:23: Standardized constraints:
INFO - 16:23:23: g_1 = [-0.07573422 -0.05174376 -0.05052817 -0.05324831 -0.05649902 -0.19260329
INFO - 16:23:23: -0.04739671]
INFO - 16:23:23: Design space:
INFO - 16:23:23: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:23: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:23: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:23: | x_1[0] | 0.1 | 0.1000000000000004 | 0.4 | float |
INFO - 16:23:23: | x_1[1] | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:23: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:23: *** End StructureScenario execution (time: 0:00:00.395386) ***
INFO - 16:23:23: *** Start PropulsionScenario execution ***
INFO - 16:23:23: PropulsionScenario
INFO - 16:23:23: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:23: MDO formulation: MDF
INFO - 16:23:23: Optimization problem:
INFO - 16:23:23: minimize 0.001*-y_4(x_3)
INFO - 16:23:23: with respect to x_3
INFO - 16:23:23: under the inequality constraints
INFO - 16:23:23: g_3(x_3) <= 0
INFO - 16:23:23: over the design space:
INFO - 16:23:23: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:23: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:23: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:23: | x_3 | 0.1 | 0.2871004772038968 | 1 | float |
INFO - 16:23:23: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:23: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:23: 2%|▏ | 1/50 [00:00<00:00, 83.75 it/sec, feas=True, obj=-0.734]
INFO - 16:23:23: Optimization result:
INFO - 16:23:23: Optimizer info:
INFO - 16:23:23: Status: 8
INFO - 16:23:23: Message: Positive directional derivative for linesearch
INFO - 16:23:23: Solution:
INFO - 16:23:23: The solution is feasible.
INFO - 16:23:23: Objective: -0.7339139488504138
INFO - 16:23:23: Standardized constraints:
INFO - 16:23:23: g_3 = [-7.18559647e-01 -2.81440353e-01 2.22044605e-16 -1.27460556e-01]
INFO - 16:23:23: Design space:
INFO - 16:23:23: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:23: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:23: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:23: | x_3 | 0.1 | 0.2871004772038968 | 1 | float |
INFO - 16:23:23: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:23: *** End PropulsionScenario execution (time: 0:00:00.014090) ***
INFO - 16:23:23: *** Start AerodynamicsScenario execution ***
INFO - 16:23:23: AerodynamicsScenario
INFO - 16:23:23: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:23: MDO formulation: MDF
INFO - 16:23:23: Optimization problem:
INFO - 16:23:23: minimize 0.001*-y_4(x_2)
INFO - 16:23:23: with respect to x_2
INFO - 16:23:23: under the inequality constraints
INFO - 16:23:23: g_2(x_2) <= 0
INFO - 16:23:23: over the design space:
INFO - 16:23:23: +------+-------------+-------+-------------+-------+
INFO - 16:23:23: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:23: +------+-------------+-------+-------------+-------+
INFO - 16:23:23: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:23: +------+-------------+-------+-------------+-------+
INFO - 16:23:23: Solving optimization problem with algorithm SLSQP:
WARNING - 16:23:23: Optimization found no feasible point; the least infeasible point is selected.
INFO - 16:23:23: 2%|▏ | 1/50 [00:00<00:00, 104.30 it/sec, feas=False, obj=-0.734]
INFO - 16:23:23: Optimization result:
INFO - 16:23:23: Optimizer info:
INFO - 16:23:23: Status: 8
INFO - 16:23:23: Message: Positive directional derivative for linesearch
INFO - 16:23:23: Solution:
WARNING - 16:23:23: The solution is not feasible.
INFO - 16:23:23: Objective: -0.7339139488504138
INFO - 16:23:23: Standardized constraints:
INFO - 16:23:23: g_2 = 0.010000000000000009
INFO - 16:23:23: Design space:
INFO - 16:23:23: +------+-------------+-------+-------------+-------+
INFO - 16:23:23: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:23: +------+-------------+-------+-------------+-------+
INFO - 16:23:23: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:23: +------+-------------+-------+-------------+-------+
INFO - 16:23:23: *** End AerodynamicsScenario execution (time: 0:00:00.011382) ***
INFO - 16:23:23: *** Start StructureScenario execution ***
INFO - 16:23:23: StructureScenario
INFO - 16:23:23: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:23: MDO formulation: MDF
INFO - 16:23:23: Optimization problem:
INFO - 16:23:23: minimize 0.001*-y_4(x_1)
INFO - 16:23:23: with respect to x_1
INFO - 16:23:23: under the inequality constraints
INFO - 16:23:23: g_1(x_1) <= 0
INFO - 16:23:23: over the design space:
INFO - 16:23:23: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:23: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:23: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:23: | x_1[0] | 0.1 | 0.1000000000000004 | 0.4 | float |
INFO - 16:23:23: | x_1[1] | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:23: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:23: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:23: 2%|▏ | 1/50 [00:00<00:00, 83.04 it/sec, feas=True, obj=-0.734]
INFO - 16:23:23: 4%|▍ | 2/50 [00:00<00:00, 138.81 it/sec, feas=True, obj=-0.734]
INFO - 16:23:23: 6%|▌ | 3/50 [00:00<00:00, 180.45 it/sec, feas=True, obj=-0.734]
INFO - 16:23:23: Optimization result:
INFO - 16:23:23: Optimizer info:
INFO - 16:23:23: Status: None
INFO - 16:23:23: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:23: Solution:
INFO - 16:23:23: The solution is feasible.
INFO - 16:23:23: Objective: -0.7339139488504138
INFO - 16:23:23: Standardized constraints:
INFO - 16:23:23: g_1 = [-0.07573422 -0.05174376 -0.05052817 -0.05324831 -0.05649902 -0.19260329
INFO - 16:23:23: -0.04739671]
INFO - 16:23:23: Design space:
INFO - 16:23:23: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:23: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:23: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:23: | x_1[0] | 0.1 | 0.1000000000000004 | 0.4 | float |
INFO - 16:23:23: | x_1[1] | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:23: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:23: *** End StructureScenario execution (time: 0:00:00.019155) ***
INFO - 16:23:23: 5%|▌ | 5/100 [00:06<02:08, 44.42 it/min, feas=False, obj=-0.734]
INFO - 16:23:23: *** Start PropulsionScenario execution ***
INFO - 16:23:23: PropulsionScenario
INFO - 16:23:23: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:23: MDO formulation: MDF
INFO - 16:23:23: Optimization problem:
INFO - 16:23:23: minimize 0.001*-y_4(x_3)
INFO - 16:23:23: with respect to x_3
INFO - 16:23:23: under the inequality constraints
INFO - 16:23:23: g_3(x_3) <= 0
INFO - 16:23:23: over the design space:
INFO - 16:23:23: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:23: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:23: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:23: | x_3 | 0.1 | 0.2871004772038968 | 1 | float |
INFO - 16:23:23: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:23: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:23: 2%|▏ | 1/50 [00:00<00:01, 38.64 it/sec, feas=True, obj=-0.977]
INFO - 16:23:23: Optimization result:
INFO - 16:23:23: Optimizer info:
INFO - 16:23:23: Status: 8
INFO - 16:23:23: Message: Positive directional derivative for linesearch
INFO - 16:23:23: Solution:
INFO - 16:23:23: The solution is feasible.
INFO - 16:23:23: Objective: -0.9766732148551409
INFO - 16:23:23: Standardized constraints:
INFO - 16:23:23: g_3 = [-8.42489023e-01 -1.57510977e-01 2.22044605e-16 -1.27460556e-01]
INFO - 16:23:23: Design space:
INFO - 16:23:23: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:23: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:23: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:23: | x_3 | 0.1 | 0.2871004772038968 | 1 | float |
INFO - 16:23:23: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:23: *** End PropulsionScenario execution (time: 0:00:00.027781) ***
INFO - 16:23:23: *** Start AerodynamicsScenario execution ***
INFO - 16:23:23: AerodynamicsScenario
INFO - 16:23:23: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:23: MDO formulation: MDF
INFO - 16:23:23: Optimization problem:
INFO - 16:23:23: minimize 0.001*-y_4(x_2)
INFO - 16:23:23: with respect to x_2
INFO - 16:23:23: under the inequality constraints
INFO - 16:23:23: g_2(x_2) <= 0
INFO - 16:23:23: over the design space:
INFO - 16:23:23: +------+-------------+-------+-------------+-------+
INFO - 16:23:23: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:23: +------+-------------+-------+-------------+-------+
INFO - 16:23:23: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:23: +------+-------------+-------+-------------+-------+
INFO - 16:23:23: Solving optimization problem with algorithm SLSQP:
WARNING - 16:23:23: Optimization found no feasible point; the least infeasible point is selected.
INFO - 16:23:23: 2%|▏ | 1/50 [00:00<00:00, 86.13 it/sec, feas=False, obj=-0.977]
INFO - 16:23:23: Optimization result:
INFO - 16:23:23: Optimizer info:
INFO - 16:23:23: Status: 8
INFO - 16:23:23: Message: Positive directional derivative for linesearch
INFO - 16:23:23: Solution:
WARNING - 16:23:23: The solution is not feasible.
INFO - 16:23:23: Objective: -0.9766732148551409
INFO - 16:23:23: Standardized constraints:
INFO - 16:23:23: g_2 = 0.010000000000000009
INFO - 16:23:23: Design space:
INFO - 16:23:23: +------+-------------+-------+-------------+-------+
INFO - 16:23:23: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:23: +------+-------------+-------+-------------+-------+
INFO - 16:23:23: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:23: +------+-------------+-------+-------------+-------+
INFO - 16:23:23: *** End AerodynamicsScenario execution (time: 0:00:00.013158) ***
INFO - 16:23:23: *** Start StructureScenario execution ***
INFO - 16:23:23: StructureScenario
INFO - 16:23:23: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:23: MDO formulation: MDF
INFO - 16:23:23: Optimization problem:
INFO - 16:23:23: minimize 0.001*-y_4(x_1)
INFO - 16:23:23: with respect to x_1
INFO - 16:23:23: under the inequality constraints
INFO - 16:23:23: g_1(x_1) <= 0
INFO - 16:23:23: over the design space:
INFO - 16:23:23: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:23: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:23: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:23: | x_1[0] | 0.1 | 0.1000000000000004 | 0.4 | float |
INFO - 16:23:23: | x_1[1] | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:23: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:23: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:23: 2%|▏ | 1/50 [00:00<00:00, 99.51 it/sec, feas=True, obj=-0.977]
INFO - 16:23:23: 4%|▍ | 2/50 [00:00<00:00, 48.06 it/sec, feas=True, obj=-0.977]
INFO - 16:23:23: 6%|▌ | 3/50 [00:00<00:01, 40.13 it/sec, feas=True, obj=-0.977]
WARNING - 16:23:23: MDAGaussSeidel has reached its maximum number of unsuccessful iterations, but the normalized residual norm 0.0009157477359807847 is still above the tolerance 1e-06.
INFO - 16:23:23: 8%|▊ | 4/50 [00:00<00:01, 33.10 it/sec, feas=True, obj=-0.977]
INFO - 16:23:23: 10%|█ | 5/50 [00:00<00:01, 32.16 it/sec, feas=True, obj=-0.977]
INFO - 16:23:23: 12%|█▏ | 6/50 [00:00<00:01, 31.28 it/sec, feas=True, obj=-0.977]
INFO - 16:23:23: 14%|█▍ | 7/50 [00:00<00:01, 30.36 it/sec, feas=True, obj=-0.977]
INFO - 16:23:23: 16%|█▌ | 8/50 [00:00<00:01, 31.44 it/sec, feas=True, obj=-0.977]
INFO - 16:23:23: 18%|█▊ | 9/50 [00:00<00:01, 32.48 it/sec, feas=True, obj=-0.977]
INFO - 16:23:23: Optimization result:
INFO - 16:23:23: Optimizer info:
INFO - 16:23:23: Status: None
INFO - 16:23:23: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:23: Solution:
INFO - 16:23:23: The solution is feasible.
INFO - 16:23:23: Objective: -0.976907009554311
INFO - 16:23:23: Standardized constraints:
INFO - 16:23:23: g_1 = [-0.02505357 -0.02542063 -0.03358482 -0.04103714 -0.04706944 -0.20645898
INFO - 16:23:23: -0.03354102]
INFO - 16:23:23: Design space:
INFO - 16:23:23: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:23: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:23: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:23: | x_1[0] | 0.1 | 0.3999999999999999 | 0.4 | float |
INFO - 16:23:23: | x_1[1] | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:23: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:23: *** End StructureScenario execution (time: 0:00:00.279648) ***
INFO - 16:23:23: *** Start PropulsionScenario execution ***
INFO - 16:23:23: PropulsionScenario
INFO - 16:23:23: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:23: MDO formulation: MDF
INFO - 16:23:23: Optimization problem:
INFO - 16:23:23: minimize 0.001*-y_4(x_3)
INFO - 16:23:23: with respect to x_3
INFO - 16:23:23: under the inequality constraints
INFO - 16:23:23: g_3(x_3) <= 0
INFO - 16:23:23: over the design space:
INFO - 16:23:23: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:23: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:23: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:23: | x_3 | 0.1 | 0.2871004772038968 | 1 | float |
INFO - 16:23:23: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:23: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:24: 2%|▏ | 1/50 [00:00<00:00, 72.09 it/sec, feas=True, obj=-0.977]
INFO - 16:23:24: Optimization result:
INFO - 16:23:24: Optimizer info:
INFO - 16:23:24: Status: 8
INFO - 16:23:24: Message: Positive directional derivative for linesearch
INFO - 16:23:24: Solution:
INFO - 16:23:24: The solution is feasible.
INFO - 16:23:24: Objective: -0.976907009554311
INFO - 16:23:24: Standardized constraints:
INFO - 16:23:24: g_3 = [-8.42259408e-01 -1.57740592e-01 2.22044605e-16 -1.27460556e-01]
INFO - 16:23:24: Design space:
INFO - 16:23:24: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:24: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:24: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:24: | x_3 | 0.1 | 0.2871004772038968 | 1 | float |
INFO - 16:23:24: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:24: *** End PropulsionScenario execution (time: 0:00:00.015842) ***
INFO - 16:23:24: *** Start AerodynamicsScenario execution ***
INFO - 16:23:24: AerodynamicsScenario
INFO - 16:23:24: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:24: MDO formulation: MDF
INFO - 16:23:24: Optimization problem:
INFO - 16:23:24: minimize 0.001*-y_4(x_2)
INFO - 16:23:24: with respect to x_2
INFO - 16:23:24: under the inequality constraints
INFO - 16:23:24: g_2(x_2) <= 0
INFO - 16:23:24: over the design space:
INFO - 16:23:24: +------+-------------+-------+-------------+-------+
INFO - 16:23:24: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:24: +------+-------------+-------+-------------+-------+
INFO - 16:23:24: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:24: +------+-------------+-------+-------------+-------+
INFO - 16:23:24: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:24: 2%|▏ | 1/50 [00:00<00:00, 109.17 it/sec, feas=False, obj=-0.977]
INFO - 16:23:24: 4%|▍ | 2/50 [00:00<00:00, 172.82 it/sec, feas=False, obj=-0.977]
INFO - 16:23:24: 6%|▌ | 3/50 [00:00<00:00, 213.98 it/sec, feas=False, obj=-0.977]
INFO - 16:23:24: 8%|▊ | 4/50 [00:00<00:00, 242.45 it/sec, feas=False, obj=-0.977]
INFO - 16:23:24: 10%|█ | 5/50 [00:00<00:00, 262.86 it/sec, feas=False, obj=-0.977]
INFO - 16:23:24: 12%|█▏ | 6/50 [00:00<00:00, 279.08 it/sec, feas=False, obj=-0.977]
INFO - 16:23:24: 14%|█▍ | 7/50 [00:00<00:00, 292.03 it/sec, feas=False, obj=-0.977]
INFO - 16:23:24: 16%|█▌ | 8/50 [00:00<00:00, 304.58 it/sec, feas=False, obj=-0.977]
INFO - 16:23:24: 18%|█▊ | 9/50 [00:00<00:00, 318.13 it/sec, feas=False, obj=-0.977]
INFO - 16:23:24: 20%|██ | 10/50 [00:00<00:00, 330.71 it/sec, feas=False, obj=-0.977]
INFO - 16:23:24: 22%|██▏ | 11/50 [00:00<00:00, 332.90 it/sec, feas=False, obj=-0.977]
INFO - 16:23:24: 24%|██▍ | 12/50 [00:00<00:00, 338.88 it/sec, feas=False, obj=-0.977]
INFO - 16:23:24: 26%|██▌ | 13/50 [00:00<00:00, 343.18 it/sec, feas=False, obj=-0.977]
INFO - 16:23:24: 28%|██▊ | 14/50 [00:00<00:00, 346.66 it/sec, feas=False, obj=-0.977]
INFO - 16:23:24: 30%|███ | 15/50 [00:00<00:00, 349.91 it/sec, feas=False, obj=-0.977]
INFO - 16:23:24: 32%|███▏ | 16/50 [00:00<00:00, 352.62 it/sec, feas=False, obj=-0.977]
INFO - 16:23:24: 34%|███▍ | 17/50 [00:00<00:00, 355.18 it/sec, feas=False, obj=-0.977]
INFO - 16:23:24: 36%|███▌ | 18/50 [00:00<00:00, 357.62 it/sec, feas=False, obj=-0.977]
INFO - 16:23:24: 38%|███▊ | 19/50 [00:00<00:00, 359.62 it/sec, feas=False, obj=-0.977]
INFO - 16:23:24: 40%|████ | 20/50 [00:00<00:00, 361.44 it/sec, feas=False, obj=-0.977]
INFO - 16:23:24: 42%|████▏ | 21/50 [00:00<00:00, 364.80 it/sec, feas=False, obj=-0.977]
INFO - 16:23:24: 44%|████▍ | 22/50 [00:00<00:00, 289.95 it/sec, feas=False, obj=-0.977]
INFO - 16:23:24: 46%|████▌ | 23/50 [00:00<00:00, 294.31 it/sec, feas=False, obj=-0.977]
INFO - 16:23:24: 48%|████▊ | 24/50 [00:00<00:00, 294.86 it/sec, feas=False, obj=-0.977]
INFO - 16:23:24: 50%|█████ | 25/50 [00:00<00:00, 298.47 it/sec, feas=False, obj=-0.977]
INFO - 16:23:24: 52%|█████▏ | 26/50 [00:00<00:00, 301.29 it/sec, feas=False, obj=-0.977]
INFO - 16:23:24: 54%|█████▍ | 27/50 [00:00<00:00, 304.11 it/sec, feas=False, obj=-0.977]
INFO - 16:23:24: 56%|█████▌ | 28/50 [00:00<00:00, 306.64 it/sec, feas=False, obj=-0.977]
INFO - 16:23:24: 58%|█████▊ | 29/50 [00:00<00:00, 309.02 it/sec, feas=False, obj=-0.977]
INFO - 16:23:24: 60%|██████ | 30/50 [00:00<00:00, 311.56 it/sec, feas=False, obj=-0.977]
INFO - 16:23:24: 62%|██████▏ | 31/50 [00:00<00:00, 313.99 it/sec, feas=False, obj=-0.977]
INFO - 16:23:24: 64%|██████▍ | 32/50 [00:00<00:00, 316.37 it/sec, feas=False, obj=-0.977]
WARNING - 16:23:24: Optimization found no feasible point; the least infeasible point is selected.
INFO - 16:23:24: 66%|██████▌ | 33/50 [00:00<00:00, 270.25 it/sec, feas=False, obj=-0.977]
INFO - 16:23:24: Optimization result:
INFO - 16:23:24: Optimizer info:
INFO - 16:23:24: Status: 8
INFO - 16:23:24: Message: Positive directional derivative for linesearch
INFO - 16:23:24: Solution:
WARNING - 16:23:24: The solution is not feasible.
INFO - 16:23:24: Objective: -0.976907009554311
INFO - 16:23:24: Standardized constraints:
INFO - 16:23:24: g_2 = 0.010000000000000009
INFO - 16:23:24: Design space:
INFO - 16:23:24: +------+-------------+-------+-------------+-------+
INFO - 16:23:24: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:24: +------+-------------+-------+-------------+-------+
INFO - 16:23:24: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:24: +------+-------------+-------+-------------+-------+
INFO - 16:23:24: *** End AerodynamicsScenario execution (time: 0:00:00.123872) ***
INFO - 16:23:24: *** Start StructureScenario execution ***
INFO - 16:23:24: StructureScenario
INFO - 16:23:24: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:24: MDO formulation: MDF
INFO - 16:23:24: Optimization problem:
INFO - 16:23:24: minimize 0.001*-y_4(x_1)
INFO - 16:23:24: with respect to x_1
INFO - 16:23:24: under the inequality constraints
INFO - 16:23:24: g_1(x_1) <= 0
INFO - 16:23:24: over the design space:
INFO - 16:23:24: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:24: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:24: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:24: | x_1[0] | 0.1 | 0.3999999999999999 | 0.4 | float |
INFO - 16:23:24: | x_1[1] | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:24: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:24: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:24: 2%|▏ | 1/50 [00:00<00:00, 96.12 it/sec, feas=True, obj=-0.977]
INFO - 16:23:24: Optimization result:
INFO - 16:23:24: Optimizer info:
INFO - 16:23:24: Status: 8
INFO - 16:23:24: Message: Positive directional derivative for linesearch
INFO - 16:23:24: Solution:
INFO - 16:23:24: The solution is feasible.
INFO - 16:23:24: Objective: -0.976907009554311
INFO - 16:23:24: Standardized constraints:
INFO - 16:23:24: g_1 = [-0.02505357 -0.02542063 -0.03358482 -0.04103714 -0.04706944 -0.20645898
INFO - 16:23:24: -0.03354102]
INFO - 16:23:24: Design space:
INFO - 16:23:24: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:24: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:24: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:24: | x_1[0] | 0.1 | 0.3999999999999999 | 0.4 | float |
INFO - 16:23:24: | x_1[1] | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:24: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:24: *** End StructureScenario execution (time: 0:00:00.012558) ***
INFO - 16:23:24: 6%|▌ | 6/100 [00:07<01:53, 49.59 it/min, feas=False, obj=-0.977]
INFO - 16:23:24: *** Start PropulsionScenario execution ***
INFO - 16:23:24: PropulsionScenario
INFO - 16:23:24: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:24: MDO formulation: MDF
INFO - 16:23:24: Optimization problem:
INFO - 16:23:24: minimize 0.001*-y_4(x_3)
INFO - 16:23:24: with respect to x_3
INFO - 16:23:24: under the inequality constraints
INFO - 16:23:24: g_3(x_3) <= 0
INFO - 16:23:24: over the design space:
INFO - 16:23:24: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:24: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:24: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:24: | x_3 | 0.1 | 0.2871004772038968 | 1 | float |
INFO - 16:23:24: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:24: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:24: 2%|▏ | 1/50 [00:00<00:01, 36.98 it/sec, feas=True, obj=-1.05]
INFO - 16:23:24: Optimization result:
INFO - 16:23:24: Optimizer info:
INFO - 16:23:24: Status: 8
INFO - 16:23:24: Message: Positive directional derivative for linesearch
INFO - 16:23:24: Solution:
INFO - 16:23:24: The solution is feasible.
INFO - 16:23:24: Objective: -1.050166244533434
INFO - 16:23:24: Standardized constraints:
INFO - 16:23:24: g_3 = [-6.70083434e-01 -3.29916566e-01 2.22044605e-16 -1.27460556e-01]
INFO - 16:23:24: Design space:
INFO - 16:23:24: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:24: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:24: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:24: | x_3 | 0.1 | 0.2871004772038968 | 1 | float |
INFO - 16:23:24: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:24: *** End PropulsionScenario execution (time: 0:00:00.029116) ***
INFO - 16:23:24: *** Start AerodynamicsScenario execution ***
INFO - 16:23:24: AerodynamicsScenario
INFO - 16:23:24: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:24: MDO formulation: MDF
INFO - 16:23:24: Optimization problem:
INFO - 16:23:24: minimize 0.001*-y_4(x_2)
INFO - 16:23:24: with respect to x_2
INFO - 16:23:24: under the inequality constraints
INFO - 16:23:24: g_2(x_2) <= 0
INFO - 16:23:24: over the design space:
INFO - 16:23:24: +------+-------------+-------+-------------+-------+
INFO - 16:23:24: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:24: +------+-------------+-------+-------------+-------+
INFO - 16:23:24: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:24: +------+-------------+-------+-------------+-------+
INFO - 16:23:24: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:24: 2%|▏ | 1/50 [00:00<00:00, 105.37 it/sec, feas=False, obj=-1.05]
INFO - 16:23:24: 4%|▍ | 2/50 [00:00<00:00, 163.97 it/sec, feas=False, obj=-1.05]
INFO - 16:23:24: 6%|▌ | 3/50 [00:00<00:00, 199.92 it/sec, feas=False, obj=-1.05]
INFO - 16:23:24: 8%|▊ | 4/50 [00:00<00:00, 224.04 it/sec, feas=False, obj=-1.05]
INFO - 16:23:24: 10%|█ | 5/50 [00:00<00:00, 242.77 it/sec, feas=False, obj=-1.05]
INFO - 16:23:24: 12%|█▏ | 6/50 [00:00<00:00, 256.89 it/sec, feas=False, obj=-1.05]
INFO - 16:23:24: 14%|█▍ | 7/50 [00:00<00:00, 272.35 it/sec, feas=False, obj=-1.05]
INFO - 16:23:24: 16%|█▌ | 8/50 [00:00<00:00, 288.08 it/sec, feas=False, obj=-1.05]
INFO - 16:23:24: 18%|█▊ | 9/50 [00:00<00:00, 300.49 it/sec, feas=False, obj=-1.05]
INFO - 16:23:24: 20%|██ | 10/50 [00:00<00:00, 302.38 it/sec, feas=False, obj=-1.05]
INFO - 16:23:24: 22%|██▏ | 11/50 [00:00<00:00, 306.73 it/sec, feas=False, obj=-1.05]
INFO - 16:23:24: 24%|██▍ | 12/50 [00:00<00:00, 310.33 it/sec, feas=False, obj=-1.05]
INFO - 16:23:24: 26%|██▌ | 13/50 [00:00<00:00, 308.47 it/sec, feas=False, obj=-1.05]
INFO - 16:23:24: 28%|██▊ | 14/50 [00:00<00:00, 219.36 it/sec, feas=False, obj=-1.05]
INFO - 16:23:24: 30%|███ | 15/50 [00:00<00:00, 224.86 it/sec, feas=False, obj=-1.05]
INFO - 16:23:24: 32%|███▏ | 16/50 [00:00<00:00, 230.15 it/sec, feas=False, obj=-1.05]
INFO - 16:23:24: 34%|███▍ | 17/50 [00:00<00:00, 235.16 it/sec, feas=False, obj=-1.05]
WARNING - 16:23:24: Optimization found no feasible point; the least infeasible point is selected.
INFO - 16:23:24: 36%|███▌ | 18/50 [00:00<00:00, 186.49 it/sec, feas=False, obj=-1.05]
INFO - 16:23:24: Optimization result:
INFO - 16:23:24: Optimizer info:
INFO - 16:23:24: Status: 8
INFO - 16:23:24: Message: Positive directional derivative for linesearch
INFO - 16:23:24: Solution:
WARNING - 16:23:24: The solution is not feasible.
INFO - 16:23:24: Objective: -1.050166244533434
INFO - 16:23:24: Standardized constraints:
INFO - 16:23:24: g_2 = 0.010000000000000009
INFO - 16:23:24: Design space:
INFO - 16:23:24: +------+-------------+-------+-------------+-------+
INFO - 16:23:24: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:24: +------+-------------+-------+-------------+-------+
INFO - 16:23:24: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:24: +------+-------------+-------+-------------+-------+
INFO - 16:23:24: *** End AerodynamicsScenario execution (time: 0:00:00.098232) ***
INFO - 16:23:24: *** Start StructureScenario execution ***
INFO - 16:23:24: StructureScenario
INFO - 16:23:24: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:24: MDO formulation: MDF
INFO - 16:23:24: Optimization problem:
INFO - 16:23:24: minimize 0.001*-y_4(x_1)
INFO - 16:23:24: with respect to x_1
INFO - 16:23:24: under the inequality constraints
INFO - 16:23:24: g_1(x_1) <= 0
INFO - 16:23:24: over the design space:
INFO - 16:23:24: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:24: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:24: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:24: | x_1[0] | 0.1 | 0.3999999999999999 | 0.4 | float |
INFO - 16:23:24: | x_1[1] | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:24: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:24: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:24: 2%|▏ | 1/50 [00:00<00:00, 92.39 it/sec, feas=False, obj=-1.05]
INFO - 16:23:24: 4%|▍ | 2/50 [00:00<00:01, 40.28 it/sec, feas=True, obj=-1.03]
INFO - 16:23:24: 6%|▌ | 3/50 [00:00<00:01, 33.85 it/sec, feas=True, obj=-1.04]
INFO - 16:23:24: 8%|▊ | 4/50 [00:00<00:01, 31.98 it/sec, feas=True, obj=-1.05]
INFO - 16:23:24: 10%|█ | 5/50 [00:00<00:01, 30.75 it/sec, feas=True, obj=-1.05]
WARNING - 16:23:24: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 0.0009157477359807847 is still above the tolerance 1e-06.
INFO - 16:23:24: 12%|█▏ | 6/50 [00:00<00:01, 28.77 it/sec, feas=True, obj=-1.05]
INFO - 16:23:24: 14%|█▍ | 7/50 [00:00<00:01, 28.62 it/sec, feas=True, obj=-1.05]
INFO - 16:23:24: 16%|█▌ | 8/50 [00:00<00:01, 28.14 it/sec, feas=True, obj=-1.05]
INFO - 16:23:24: Optimization result:
INFO - 16:23:24: Optimizer info:
INFO - 16:23:24: Status: None
INFO - 16:23:24: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:24: Solution:
INFO - 16:23:24: The solution is feasible.
INFO - 16:23:24: Objective: -1.0501097518158482
INFO - 16:23:24: Standardized constraints:
INFO - 16:23:24: g_1 = [-2.58485524e-02 -1.74692489e-02 -2.44407670e-02 -3.21952521e-02
INFO - 16:23:24: -3.88530648e-02 -2.40000000e-01 5.55111512e-16]
INFO - 16:23:24: Design space:
INFO - 16:23:24: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:24: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:24: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:24: | x_1[0] | 0.1 | 0.3050815823044163 | 0.4 | float |
INFO - 16:23:24: | x_1[1] | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:24: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:24: *** End StructureScenario execution (time: 0:00:00.287081) ***
INFO - 16:23:24: *** Start PropulsionScenario execution ***
INFO - 16:23:24: PropulsionScenario
INFO - 16:23:24: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:24: MDO formulation: MDF
INFO - 16:23:24: Optimization problem:
INFO - 16:23:24: minimize 0.001*-y_4(x_3)
INFO - 16:23:24: with respect to x_3
INFO - 16:23:24: under the inequality constraints
INFO - 16:23:24: g_3(x_3) <= 0
INFO - 16:23:24: over the design space:
INFO - 16:23:24: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:24: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:24: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:24: | x_3 | 0.1 | 0.2871004772038968 | 1 | float |
INFO - 16:23:24: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:24: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:24: 2%|▏ | 1/50 [00:00<00:00, 106.93 it/sec, feas=True, obj=-1.05]
INFO - 16:23:24: Optimization result:
INFO - 16:23:24: Optimizer info:
INFO - 16:23:24: Status: 8
INFO - 16:23:24: Message: Positive directional derivative for linesearch
INFO - 16:23:24: Solution:
INFO - 16:23:24: The solution is feasible.
INFO - 16:23:24: Objective: -1.0501097518158482
INFO - 16:23:24: Standardized constraints:
INFO - 16:23:24: g_3 = [-6.70237655e-01 -3.29762345e-01 2.22044605e-16 -1.27460556e-01]
INFO - 16:23:24: Design space:
INFO - 16:23:24: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:24: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:24: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:24: | x_3 | 0.1 | 0.2871004772038968 | 1 | float |
INFO - 16:23:24: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:24: *** End PropulsionScenario execution (time: 0:00:00.011274) ***
INFO - 16:23:24: *** Start AerodynamicsScenario execution ***
INFO - 16:23:24: AerodynamicsScenario
INFO - 16:23:24: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:24: MDO formulation: MDF
INFO - 16:23:24: Optimization problem:
INFO - 16:23:24: minimize 0.001*-y_4(x_2)
INFO - 16:23:24: with respect to x_2
INFO - 16:23:24: under the inequality constraints
INFO - 16:23:24: g_2(x_2) <= 0
INFO - 16:23:24: over the design space:
INFO - 16:23:24: +------+-------------+-------+-------------+-------+
INFO - 16:23:24: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:24: +------+-------------+-------+-------------+-------+
INFO - 16:23:24: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:24: +------+-------------+-------+-------------+-------+
INFO - 16:23:24: Solving optimization problem with algorithm SLSQP:
WARNING - 16:23:24: Optimization found no feasible point; the least infeasible point is selected.
INFO - 16:23:24: 2%|▏ | 1/50 [00:00<00:00, 88.37 it/sec, feas=False, obj=-1.05]
INFO - 16:23:24: Optimization result:
INFO - 16:23:24: Optimizer info:
INFO - 16:23:24: Status: 8
INFO - 16:23:24: Message: Positive directional derivative for linesearch
INFO - 16:23:24: Solution:
WARNING - 16:23:24: The solution is not feasible.
INFO - 16:23:24: Objective: -1.0501097518158482
INFO - 16:23:24: Standardized constraints:
INFO - 16:23:24: g_2 = 0.010000000000000009
INFO - 16:23:24: Design space:
INFO - 16:23:24: +------+-------------+-------+-------------+-------+
INFO - 16:23:24: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:24: +------+-------------+-------+-------------+-------+
INFO - 16:23:24: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:24: +------+-------------+-------+-------------+-------+
INFO - 16:23:24: *** End AerodynamicsScenario execution (time: 0:00:00.012905) ***
INFO - 16:23:24: *** Start StructureScenario execution ***
INFO - 16:23:24: StructureScenario
INFO - 16:23:24: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:24: MDO formulation: MDF
INFO - 16:23:24: Optimization problem:
INFO - 16:23:24: minimize 0.001*-y_4(x_1)
INFO - 16:23:24: with respect to x_1
INFO - 16:23:24: under the inequality constraints
INFO - 16:23:24: g_1(x_1) <= 0
INFO - 16:23:24: over the design space:
INFO - 16:23:24: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:24: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:24: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:24: | x_1[0] | 0.1 | 0.3050815823044163 | 0.4 | float |
INFO - 16:23:24: | x_1[1] | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:24: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:24: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:24: 2%|▏ | 1/50 [00:00<00:00, 101.85 it/sec, feas=True, obj=-1.05]
INFO - 16:23:24: 4%|▍ | 2/50 [00:00<00:00, 164.32 it/sec, feas=True, obj=-1.05]
INFO - 16:23:24: 6%|▌ | 3/50 [00:00<00:00, 207.25 it/sec, feas=True, obj=-1.05]
INFO - 16:23:24: Optimization result:
INFO - 16:23:24: Optimizer info:
INFO - 16:23:24: Status: None
INFO - 16:23:24: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:24: Solution:
INFO - 16:23:24: The solution is feasible.
INFO - 16:23:24: Objective: -1.0501097518158482
INFO - 16:23:24: Standardized constraints:
INFO - 16:23:24: g_1 = [-2.58485524e-02 -1.74692489e-02 -2.44407670e-02 -3.21952521e-02
INFO - 16:23:24: -3.88530648e-02 -2.40000000e-01 5.55111512e-16]
INFO - 16:23:24: Design space:
INFO - 16:23:24: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:24: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:24: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:24: | x_1[0] | 0.1 | 0.3050815823044163 | 0.4 | float |
INFO - 16:23:24: | x_1[1] | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:24: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:24: *** End StructureScenario execution (time: 0:00:00.018770) ***
INFO - 16:23:24: 7%|▋ | 7/100 [00:07<01:43, 54.14 it/min, feas=False, obj=-1.05]
INFO - 16:23:24: *** Start PropulsionScenario execution ***
INFO - 16:23:24: PropulsionScenario
INFO - 16:23:24: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:24: MDO formulation: MDF
INFO - 16:23:24: Optimization problem:
INFO - 16:23:24: minimize 0.001*-y_4(x_3)
INFO - 16:23:24: with respect to x_3
INFO - 16:23:24: under the inequality constraints
INFO - 16:23:24: g_3(x_3) <= 0
INFO - 16:23:24: over the design space:
INFO - 16:23:24: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:24: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:24: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:24: | x_3 | 0.1 | 0.2871004772038968 | 1 | float |
INFO - 16:23:24: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:24: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:24: 2%|▏ | 1/50 [00:00<00:01, 35.34 it/sec, feas=False, obj=-1.66]
INFO - 16:23:24: 4%|▍ | 2/50 [00:00<00:01, 34.58 it/sec, feas=True, obj=-1.6]
WARNING - 16:23:24: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 6.724932466608626e-05 is still above the tolerance 1e-06.
INFO - 16:23:24: 6%|▌ | 3/50 [00:00<00:01, 28.75 it/sec, feas=False, obj=-1.66]
INFO - 16:23:24: 8%|▊ | 4/50 [00:00<00:02, 20.17 it/sec, feas=True, obj=-1.6]
WARNING - 16:23:24: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 6.724932466608626e-05 is still above the tolerance 1e-06.
INFO - 16:23:24: 10%|█ | 5/50 [00:00<00:02, 20.42 it/sec, feas=True, obj=-1.6]
INFO - 16:23:24: Optimization result:
INFO - 16:23:24: Optimizer info:
INFO - 16:23:24: Status: 8
INFO - 16:23:24: Message: Positive directional derivative for linesearch
INFO - 16:23:24: Solution:
INFO - 16:23:24: The solution is feasible.
INFO - 16:23:24: Objective: -1.5969285678632634
INFO - 16:23:24: Standardized constraints:
INFO - 16:23:24: g_3 = [-7.56690385e-01 -2.43309615e-01 3.10862447e-15 -1.57579394e-01]
INFO - 16:23:24: Design space:
INFO - 16:23:24: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:24: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:24: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:24: | x_3 | 0.1 | 0.2216870035048433 | 1 | float |
INFO - 16:23:24: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:24: *** End PropulsionScenario execution (time: 0:00:00.247197) ***
INFO - 16:23:24: *** Start AerodynamicsScenario execution ***
INFO - 16:23:24: AerodynamicsScenario
INFO - 16:23:24: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:24: MDO formulation: MDF
INFO - 16:23:24: Optimization problem:
INFO - 16:23:24: minimize 0.001*-y_4(x_2)
INFO - 16:23:24: with respect to x_2
INFO - 16:23:24: under the inequality constraints
INFO - 16:23:24: g_2(x_2) <= 0
INFO - 16:23:24: over the design space:
INFO - 16:23:24: +------+-------------+-------+-------------+-------+
INFO - 16:23:24: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:24: +------+-------------+-------+-------------+-------+
INFO - 16:23:24: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:24: +------+-------------+-------+-------------+-------+
INFO - 16:23:24: Solving optimization problem with algorithm SLSQP:
WARNING - 16:23:24: Optimization found no feasible point; the least infeasible point is selected.
INFO - 16:23:24: 2%|▏ | 1/50 [00:00<00:00, 104.38 it/sec, feas=False, obj=-1.6]
INFO - 16:23:24: Optimization result:
INFO - 16:23:24: Optimizer info:
INFO - 16:23:24: Status: 8
INFO - 16:23:24: Message: Positive directional derivative for linesearch
INFO - 16:23:24: Solution:
WARNING - 16:23:24: The solution is not feasible.
INFO - 16:23:24: Objective: -1.5969285678632634
INFO - 16:23:24: Standardized constraints:
INFO - 16:23:24: g_2 = 0.010000000000000009
INFO - 16:23:24: Design space:
INFO - 16:23:24: +------+-------------+-------+-------------+-------+
INFO - 16:23:24: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:24: +------+-------------+-------+-------------+-------+
INFO - 16:23:24: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:24: +------+-------------+-------+-------------+-------+
INFO - 16:23:24: *** End AerodynamicsScenario execution (time: 0:00:00.011186) ***
INFO - 16:23:24: *** Start StructureScenario execution ***
INFO - 16:23:24: StructureScenario
INFO - 16:23:24: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:24: MDO formulation: MDF
INFO - 16:23:24: Optimization problem:
INFO - 16:23:24: minimize 0.001*-y_4(x_1)
INFO - 16:23:24: with respect to x_1
INFO - 16:23:24: under the inequality constraints
INFO - 16:23:24: g_1(x_1) <= 0
INFO - 16:23:24: over the design space:
INFO - 16:23:24: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:24: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:24: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:24: | x_1[0] | 0.1 | 0.3050815823044163 | 0.4 | float |
INFO - 16:23:24: | x_1[1] | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:24: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:24: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:24: 2%|▏ | 1/50 [00:00<00:00, 97.18 it/sec, feas=False, obj=-1.6]
INFO - 16:23:24: 4%|▍ | 2/50 [00:00<00:01, 40.89 it/sec, feas=True, obj=-1.6]
INFO - 16:23:25: 6%|▌ | 3/50 [00:00<00:01, 34.25 it/sec, feas=True, obj=-1.6]
INFO - 16:23:25: 8%|▊ | 4/50 [00:00<00:01, 31.63 it/sec, feas=True, obj=-1.6]
INFO - 16:23:25: 10%|█ | 5/50 [00:00<00:01, 30.25 it/sec, feas=True, obj=-1.6]
INFO - 16:23:25: Optimization result:
INFO - 16:23:25: Optimizer info:
INFO - 16:23:25: Status: None
INFO - 16:23:25: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:25: Solution:
INFO - 16:23:25: The solution is feasible.
INFO - 16:23:25: Objective: -1.5968133716572748
INFO - 16:23:25: Standardized constraints:
INFO - 16:23:25: g_1 = [-3.08368226e-02 -1.97344151e-02 -2.57420113e-02 -3.30453850e-02
INFO - 16:23:25: -3.94554742e-02 -2.40000000e-01 1.11022302e-16]
INFO - 16:23:25: Design space:
INFO - 16:23:25: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:25: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:25: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:25: | x_1[0] | 0.1 | 0.2701423180096533 | 0.4 | float |
INFO - 16:23:25: | x_1[1] | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:25: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:25: *** End StructureScenario execution (time: 0:00:00.167985) ***
INFO - 16:23:25: *** Start PropulsionScenario execution ***
INFO - 16:23:25: PropulsionScenario
INFO - 16:23:25: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:25: MDO formulation: MDF
INFO - 16:23:25: Optimization problem:
INFO - 16:23:25: minimize 0.001*-y_4(x_3)
INFO - 16:23:25: with respect to x_3
INFO - 16:23:25: under the inequality constraints
INFO - 16:23:25: g_3(x_3) <= 0
INFO - 16:23:25: over the design space:
INFO - 16:23:25: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:25: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:25: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:25: | x_3 | 0.1 | 0.2216870035048433 | 1 | float |
INFO - 16:23:25: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:25: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:25: 2%|▏ | 1/50 [00:00<00:00, 110.00 it/sec, feas=True, obj=-1.6]
INFO - 16:23:25: 4%|▍ | 2/50 [00:00<00:00, 158.21 it/sec, feas=True, obj=-1.6]
INFO - 16:23:25: 6%|▌ | 3/50 [00:00<00:00, 187.63 it/sec, feas=True, obj=-1.6]
INFO - 16:23:25: Optimization result:
INFO - 16:23:25: Optimizer info:
INFO - 16:23:25: Status: None
INFO - 16:23:25: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:25: Solution:
INFO - 16:23:25: The solution is feasible.
INFO - 16:23:25: Objective: -1.5968133716572748
INFO - 16:23:25: Standardized constraints:
INFO - 16:23:25: g_3 = [-7.56738583e-01 -2.43261417e-01 3.10862447e-15 -1.57579394e-01]
INFO - 16:23:25: Design space:
INFO - 16:23:25: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:25: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:25: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:25: | x_3 | 0.1 | 0.2216870035048433 | 1 | float |
INFO - 16:23:25: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:25: *** End PropulsionScenario execution (time: 0:00:00.018299) ***
INFO - 16:23:25: *** Start AerodynamicsScenario execution ***
INFO - 16:23:25: AerodynamicsScenario
INFO - 16:23:25: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:25: MDO formulation: MDF
INFO - 16:23:25: Optimization problem:
INFO - 16:23:25: minimize 0.001*-y_4(x_2)
INFO - 16:23:25: with respect to x_2
INFO - 16:23:25: under the inequality constraints
INFO - 16:23:25: g_2(x_2) <= 0
INFO - 16:23:25: over the design space:
INFO - 16:23:25: +------+-------------+-------+-------------+-------+
INFO - 16:23:25: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:25: +------+-------------+-------+-------------+-------+
INFO - 16:23:25: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:25: +------+-------------+-------+-------------+-------+
INFO - 16:23:25: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:25: 2%|▏ | 1/50 [00:00<00:00, 86.54 it/sec, feas=False, obj=-1.6]
INFO - 16:23:25: 4%|▍ | 2/50 [00:00<00:00, 137.01 it/sec, feas=False, obj=-1.6]
INFO - 16:23:25: 6%|▌ | 3/50 [00:00<00:00, 169.83 it/sec, feas=False, obj=-1.6]
INFO - 16:23:25: 8%|▊ | 4/50 [00:00<00:00, 191.48 it/sec, feas=False, obj=-1.6]
INFO - 16:23:25: 10%|█ | 5/50 [00:00<00:00, 208.01 it/sec, feas=False, obj=-1.6]
INFO - 16:23:25: 12%|█▏ | 6/50 [00:00<00:00, 220.43 it/sec, feas=False, obj=-1.6]
INFO - 16:23:25: 14%|█▍ | 7/50 [00:00<00:00, 231.80 it/sec, feas=False, obj=-1.6]
INFO - 16:23:25: 16%|█▌ | 8/50 [00:00<00:00, 243.68 it/sec, feas=False, obj=-1.6]
INFO - 16:23:25: 18%|█▊ | 9/50 [00:00<00:00, 253.68 it/sec, feas=False, obj=-1.6]
INFO - 16:23:25: 20%|██ | 10/50 [00:00<00:00, 255.89 it/sec, feas=False, obj=-1.6]
INFO - 16:23:25: 22%|██▏ | 11/50 [00:00<00:00, 260.89 it/sec, feas=False, obj=-1.6]
INFO - 16:23:25: 24%|██▍ | 12/50 [00:00<00:00, 264.86 it/sec, feas=False, obj=-1.6]
INFO - 16:23:25: 26%|██▌ | 13/50 [00:00<00:00, 268.30 it/sec, feas=False, obj=-1.6]
INFO - 16:23:25: 28%|██▊ | 14/50 [00:00<00:00, 271.45 it/sec, feas=False, obj=-1.6]
INFO - 16:23:25: 30%|███ | 15/50 [00:00<00:00, 274.23 it/sec, feas=False, obj=-1.6]
INFO - 16:23:25: 32%|███▏ | 16/50 [00:00<00:00, 276.73 it/sec, feas=False, obj=-1.6]
INFO - 16:23:25: 34%|███▍ | 17/50 [00:00<00:00, 278.83 it/sec, feas=False, obj=-1.6]
INFO - 16:23:25: 36%|███▌ | 18/50 [00:00<00:00, 212.69 it/sec, feas=False, obj=-1.6]
INFO - 16:23:25: 38%|███▊ | 19/50 [00:00<00:00, 216.06 it/sec, feas=False, obj=-1.6]
INFO - 16:23:25: 40%|████ | 20/50 [00:00<00:00, 219.37 it/sec, feas=False, obj=-1.6]
INFO - 16:23:25: 42%|████▏ | 21/50 [00:00<00:00, 222.79 it/sec, feas=False, obj=-1.6]
INFO - 16:23:25: 44%|████▍ | 22/50 [00:00<00:00, 225.84 it/sec, feas=False, obj=-1.6]
INFO - 16:23:25: 46%|████▌ | 23/50 [00:00<00:00, 228.72 it/sec, feas=False, obj=-1.6]
INFO - 16:23:25: 48%|████▊ | 24/50 [00:00<00:00, 231.77 it/sec, feas=False, obj=-1.6]
INFO - 16:23:25: 50%|█████ | 25/50 [00:00<00:00, 233.50 it/sec, feas=False, obj=-1.6]
INFO - 16:23:25: 52%|█████▏ | 26/50 [00:00<00:00, 236.40 it/sec, feas=False, obj=-1.6]
INFO - 16:23:25: 54%|█████▍ | 27/50 [00:00<00:00, 238.76 it/sec, feas=False, obj=-1.6]
INFO - 16:23:25: 56%|█████▌ | 28/50 [00:00<00:00, 240.86 it/sec, feas=False, obj=-1.6]
INFO - 16:23:25: 58%|█████▊ | 29/50 [00:00<00:00, 207.98 it/sec, feas=False, obj=-1.6]
INFO - 16:23:25: 60%|██████ | 30/50 [00:00<00:00, 210.32 it/sec, feas=False, obj=-1.6]
INFO - 16:23:25: 62%|██████▏ | 31/50 [00:00<00:00, 212.66 it/sec, feas=False, obj=-1.6]
INFO - 16:23:25: 64%|██████▍ | 32/50 [00:00<00:00, 214.92 it/sec, feas=False, obj=-1.6]
INFO - 16:23:25: 66%|██████▌ | 33/50 [00:00<00:00, 217.05 it/sec, feas=False, obj=-1.6]
INFO - 16:23:25: 68%|██████▊ | 34/50 [00:00<00:00, 219.08 it/sec, feas=False, obj=-1.6]
INFO - 16:23:25: 70%|███████ | 35/50 [00:00<00:00, 221.23 it/sec, feas=False, obj=-1.6]
INFO - 16:23:25: 72%|███████▏ | 36/50 [00:00<00:00, 223.36 it/sec, feas=False, obj=-1.6]
INFO - 16:23:25: 74%|███████▍ | 37/50 [00:00<00:00, 205.03 it/sec, feas=False, obj=-1.6]
INFO - 16:23:25: 76%|███████▌ | 38/50 [00:00<00:00, 206.89 it/sec, feas=False, obj=-1.6]
INFO - 16:23:25: 78%|███████▊ | 39/50 [00:00<00:00, 208.77 it/sec, feas=False, obj=-1.6]
INFO - 16:23:25: 80%|████████ | 40/50 [00:00<00:00, 190.15 it/sec, feas=False, obj=-1.6]
INFO - 16:23:25: 82%|████████▏ | 41/50 [00:00<00:00, 192.07 it/sec, feas=False, obj=-1.6]
INFO - 16:23:25: 84%|████████▍ | 42/50 [00:00<00:00, 193.93 it/sec, feas=False, obj=-1.6]
INFO - 16:23:25: 86%|████████▌ | 43/50 [00:00<00:00, 195.73 it/sec, feas=False, obj=-1.6]
INFO - 16:23:25: 88%|████████▊ | 44/50 [00:00<00:00, 197.48 it/sec, feas=False, obj=-1.6]
INFO - 16:23:25: 90%|█████████ | 45/50 [00:00<00:00, 199.13 it/sec, feas=False, obj=-1.6]
INFO - 16:23:25: 92%|█████████▏| 46/50 [00:00<00:00, 184.63 it/sec, feas=False, obj=-1.6]
INFO - 16:23:25: 94%|█████████▍| 47/50 [00:00<00:00, 186.35 it/sec, feas=False, obj=-1.6]
INFO - 16:23:25: 96%|█████████▌| 48/50 [00:00<00:00, 187.97 it/sec, feas=False, obj=-1.6]
INFO - 16:23:25: 98%|█████████▊| 49/50 [00:00<00:00, 189.57 it/sec, feas=False, obj=-1.6]
INFO - 16:23:25: 100%|██████████| 50/50 [00:00<00:00, 191.13 it/sec, feas=False, obj=-1.6]
WARNING - 16:23:25: Optimization found no feasible point; the least infeasible point is selected.
INFO - 16:23:25: Optimization result:
INFO - 16:23:25: Optimizer info:
INFO - 16:23:25: Status: None
INFO - 16:23:25: Message: Maximum number of iterations reached. GEMSEO stopped the driver.
INFO - 16:23:25: Solution:
WARNING - 16:23:25: The solution is not feasible.
INFO - 16:23:25: Objective: -1.5968133716572748
INFO - 16:23:25: Standardized constraints:
INFO - 16:23:25: g_2 = 0.010000000000000009
INFO - 16:23:25: Design space:
INFO - 16:23:25: +------+-------------+-------+-------------+-------+
INFO - 16:23:25: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:25: +------+-------------+-------+-------------+-------+
INFO - 16:23:25: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:25: +------+-------------+-------+-------------+-------+
INFO - 16:23:25: *** End AerodynamicsScenario execution (time: 0:00:00.264431) ***
INFO - 16:23:25: *** Start StructureScenario execution ***
INFO - 16:23:25: StructureScenario
INFO - 16:23:25: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:25: MDO formulation: MDF
INFO - 16:23:25: Optimization problem:
INFO - 16:23:25: minimize 0.001*-y_4(x_1)
INFO - 16:23:25: with respect to x_1
INFO - 16:23:25: under the inequality constraints
INFO - 16:23:25: g_1(x_1) <= 0
INFO - 16:23:25: over the design space:
INFO - 16:23:25: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:25: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:25: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:25: | x_1[0] | 0.1 | 0.2701423180096533 | 0.4 | float |
INFO - 16:23:25: | x_1[1] | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:25: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:25: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:25: 2%|▏ | 1/50 [00:00<00:00, 73.88 it/sec, feas=True, obj=-1.6]
INFO - 16:23:25: Optimization result:
INFO - 16:23:25: Optimizer info:
INFO - 16:23:25: Status: 8
INFO - 16:23:25: Message: Positive directional derivative for linesearch
INFO - 16:23:25: Solution:
INFO - 16:23:25: The solution is feasible.
INFO - 16:23:25: Objective: -1.5968133716572748
INFO - 16:23:25: Standardized constraints:
INFO - 16:23:25: g_1 = [-3.08368226e-02 -1.97344151e-02 -2.57420113e-02 -3.30453850e-02
INFO - 16:23:25: -3.94554742e-02 -2.40000000e-01 1.11022302e-16]
INFO - 16:23:25: Design space:
INFO - 16:23:25: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:25: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:25: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:25: | x_1[0] | 0.1 | 0.2701423180096533 | 0.4 | float |
INFO - 16:23:25: | x_1[1] | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:25: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:25: *** End StructureScenario execution (time: 0:00:00.015715) ***
INFO - 16:23:25: 8%|▊ | 8/100 [00:08<01:37, 56.33 it/min, feas=False, obj=-1.6]
INFO - 16:23:25: *** Start PropulsionScenario execution ***
INFO - 16:23:25: PropulsionScenario
INFO - 16:23:25: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:25: MDO formulation: MDF
INFO - 16:23:25: Optimization problem:
INFO - 16:23:25: minimize 0.001*-y_4(x_3)
INFO - 16:23:25: with respect to x_3
INFO - 16:23:25: under the inequality constraints
INFO - 16:23:25: g_3(x_3) <= 0
INFO - 16:23:25: over the design space:
INFO - 16:23:25: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:25: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:25: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:25: | x_3 | 0.1 | 0.2216870035048433 | 1 | float |
INFO - 16:23:25: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:25: Solving optimization problem with algorithm SLSQP:
WARNING - 16:23:25: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 0.00026899729866434503 is still above the tolerance 1e-06.
INFO - 16:23:25: 2%|▏ | 1/50 [00:00<00:01, 33.46 it/sec, feas=True, obj=-1.52]
WARNING - 16:23:25: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 0.00026899729866434503 is still above the tolerance 1e-06.
INFO - 16:23:25: 4%|▍ | 2/50 [00:00<00:01, 26.25 it/sec, feas=True, obj=-1.52]
WARNING - 16:23:25: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 0.00020174797399825873 is still above the tolerance 1e-06.
INFO - 16:23:25: 6%|▌ | 3/50 [00:00<00:01, 24.43 it/sec, feas=True, obj=-1.52]
WARNING - 16:23:25: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 0.00020174797399825873 is still above the tolerance 1e-06.
INFO - 16:23:25: 8%|▊ | 4/50 [00:00<00:01, 26.01 it/sec, feas=True, obj=-1.52]
INFO - 16:23:25: Optimization result:
INFO - 16:23:25: Optimizer info:
INFO - 16:23:25: Status: None
INFO - 16:23:25: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:25: Solution:
INFO - 16:23:25: The solution is feasible.
INFO - 16:23:25: Objective: -1.5213983412761007
INFO - 16:23:25: Standardized constraints:
INFO - 16:23:25: g_3 = [-7.77804505e-01 -2.22195495e-01 2.22044605e-16 -1.57764642e-01]
INFO - 16:23:25: Design space:
INFO - 16:23:25: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:25: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:25: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:25: | x_3 | 0.1 | 0.2260985585830691 | 1 | float |
INFO - 16:23:25: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:25: *** End PropulsionScenario execution (time: 0:00:00.156205) ***
INFO - 16:23:25: *** Start AerodynamicsScenario execution ***
INFO - 16:23:25: AerodynamicsScenario
INFO - 16:23:25: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:25: MDO formulation: MDF
INFO - 16:23:25: Optimization problem:
INFO - 16:23:25: minimize 0.001*-y_4(x_2)
INFO - 16:23:25: with respect to x_2
INFO - 16:23:25: under the inequality constraints
INFO - 16:23:25: g_2(x_2) <= 0
INFO - 16:23:25: over the design space:
INFO - 16:23:25: +------+-------------+-------+-------------+-------+
INFO - 16:23:25: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:25: +------+-------------+-------+-------------+-------+
INFO - 16:23:25: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:25: +------+-------------+-------+-------------+-------+
INFO - 16:23:25: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:25: 2%|▏ | 1/50 [00:00<00:00, 72.83 it/sec, feas=False, obj=-1.52]
INFO - 16:23:25: 4%|▍ | 2/50 [00:00<00:00, 116.87 it/sec, feas=False, obj=-1.52]
INFO - 16:23:25: 6%|▌ | 3/50 [00:00<00:00, 146.32 it/sec, feas=False, obj=-1.52]
INFO - 16:23:25: 8%|▊ | 4/50 [00:00<00:00, 166.66 it/sec, feas=False, obj=-1.52]
INFO - 16:23:25: 10%|█ | 5/50 [00:00<00:00, 182.31 it/sec, feas=False, obj=-1.52]
INFO - 16:23:25: 12%|█▏ | 6/50 [00:00<00:00, 193.97 it/sec, feas=False, obj=-1.52]
INFO - 16:23:25: 14%|█▍ | 7/50 [00:00<00:00, 191.56 it/sec, feas=False, obj=-1.52]
INFO - 16:23:25: 16%|█▌ | 8/50 [00:00<00:00, 200.16 it/sec, feas=False, obj=-1.52]
INFO - 16:23:25: 18%|█▊ | 9/50 [00:00<00:00, 207.34 it/sec, feas=False, obj=-1.52]
INFO - 16:23:25: 20%|██ | 10/50 [00:00<00:00, 213.99 it/sec, feas=False, obj=-1.52]
WARNING - 16:23:25: Optimization found no feasible point; the least infeasible point is selected.
INFO - 16:23:25: 22%|██▏ | 11/50 [00:00<00:00, 192.24 it/sec, feas=False, obj=-1.52]
INFO - 16:23:25: Optimization result:
INFO - 16:23:25: Optimizer info:
INFO - 16:23:25: Status: 8
INFO - 16:23:25: Message: Positive directional derivative for linesearch
INFO - 16:23:25: Solution:
WARNING - 16:23:25: The solution is not feasible.
INFO - 16:23:25: Objective: -1.5213983412761007
INFO - 16:23:25: Standardized constraints:
INFO - 16:23:25: g_2 = 0.007145549037898213
INFO - 16:23:25: Design space:
INFO - 16:23:25: +------+-------------+-------+-------------+-------+
INFO - 16:23:25: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:25: +------+-------------+-------+-------------+-------+
INFO - 16:23:25: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:25: +------+-------------+-------+-------------+-------+
INFO - 16:23:25: *** End AerodynamicsScenario execution (time: 0:00:00.059011) ***
INFO - 16:23:25: *** Start StructureScenario execution ***
INFO - 16:23:25: StructureScenario
INFO - 16:23:25: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:25: MDO formulation: MDF
INFO - 16:23:25: Optimization problem:
INFO - 16:23:25: minimize 0.001*-y_4(x_1)
INFO - 16:23:25: with respect to x_1
INFO - 16:23:25: under the inequality constraints
INFO - 16:23:25: g_1(x_1) <= 0
INFO - 16:23:25: over the design space:
INFO - 16:23:25: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:25: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:25: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:25: | x_1[0] | 0.1 | 0.2701423180096533 | 0.4 | float |
INFO - 16:23:25: | x_1[1] | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:25: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:25: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:25: 2%|▏ | 1/50 [00:00<00:00, 76.79 it/sec, feas=False, obj=-1.52]
INFO - 16:23:25: 4%|▍ | 2/50 [00:00<00:01, 46.16 it/sec, feas=True, obj=-1.43]
INFO - 16:23:25: 6%|▌ | 3/50 [00:00<00:01, 37.86 it/sec, feas=True, obj=-1.46]
INFO - 16:23:25: 8%|▊ | 4/50 [00:00<00:01, 33.47 it/sec, feas=True, obj=-1.49]
INFO - 16:23:25: 10%|█ | 5/50 [00:00<00:01, 30.69 it/sec, feas=True, obj=-1.49]
INFO - 16:23:25: 12%|█▏ | 6/50 [00:00<00:01, 29.34 it/sec, feas=True, obj=-1.49]
INFO - 16:23:25: 14%|█▍ | 7/50 [00:00<00:01, 30.44 it/sec, feas=True, obj=-1.49]
INFO - 16:23:25: 16%|█▌ | 8/50 [00:00<00:01, 31.50 it/sec, feas=True, obj=-1.49]
INFO - 16:23:25: Optimization result:
INFO - 16:23:25: Optimizer info:
INFO - 16:23:25: Status: None
INFO - 16:23:25: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:25: Solution:
INFO - 16:23:25: The solution is feasible.
INFO - 16:23:25: Objective: -1.4868788429690418
INFO - 16:23:25: Standardized constraints:
INFO - 16:23:25: g_1 = [-6.04548408e-02 -3.41428436e-02 -3.45469888e-02 -3.91287220e-02
INFO - 16:23:25: -4.39912300e-02 -2.40000001e-01 1.13532961e-09]
INFO - 16:23:25: Design space:
INFO - 16:23:25: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:25: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:25: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:25: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:25: | x_1[1] | 0.75 | 0.7806436800678812 | 1.25 | float |
INFO - 16:23:25: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:25: *** End StructureScenario execution (time: 0:00:00.256853) ***
INFO - 16:23:25: *** Start PropulsionScenario execution ***
INFO - 16:23:25: PropulsionScenario
INFO - 16:23:25: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:25: MDO formulation: MDF
INFO - 16:23:25: Optimization problem:
INFO - 16:23:25: minimize 0.001*-y_4(x_3)
INFO - 16:23:25: with respect to x_3
INFO - 16:23:25: under the inequality constraints
INFO - 16:23:25: g_3(x_3) <= 0
INFO - 16:23:25: over the design space:
INFO - 16:23:25: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:25: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:25: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:25: | x_3 | 0.1 | 0.2260985585830691 | 1 | float |
INFO - 16:23:25: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:25: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:25: 2%|▏ | 1/50 [00:00<00:00, 83.68 it/sec, feas=True, obj=-1.49]
INFO - 16:23:25: Optimization result:
INFO - 16:23:25: Optimizer info:
INFO - 16:23:25: Status: 8
INFO - 16:23:25: Message: Positive directional derivative for linesearch
INFO - 16:23:25: Solution:
INFO - 16:23:25: The solution is feasible.
INFO - 16:23:25: Objective: -1.4868788429690418
INFO - 16:23:25: Standardized constraints:
INFO - 16:23:25: g_3 = [-7.78034653e-01 -2.21965347e-01 2.22044605e-16 -1.57764642e-01]
INFO - 16:23:25: Design space:
INFO - 16:23:25: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:25: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:25: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:25: | x_3 | 0.1 | 0.2260985585830691 | 1 | float |
INFO - 16:23:25: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:25: *** End PropulsionScenario execution (time: 0:00:00.013966) ***
INFO - 16:23:25: *** Start AerodynamicsScenario execution ***
INFO - 16:23:25: AerodynamicsScenario
INFO - 16:23:25: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:25: MDO formulation: MDF
INFO - 16:23:25: Optimization problem:
INFO - 16:23:25: minimize 0.001*-y_4(x_2)
INFO - 16:23:25: with respect to x_2
INFO - 16:23:25: under the inequality constraints
INFO - 16:23:25: g_2(x_2) <= 0
INFO - 16:23:25: over the design space:
INFO - 16:23:25: +------+-------------+-------+-------------+-------+
INFO - 16:23:25: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:25: +------+-------------+-------+-------------+-------+
INFO - 16:23:25: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:25: +------+-------------+-------+-------------+-------+
INFO - 16:23:25: Solving optimization problem with algorithm SLSQP:
WARNING - 16:23:25: Optimization found no feasible point; the least infeasible point is selected.
INFO - 16:23:25: 2%|▏ | 1/50 [00:00<00:00, 107.45 it/sec, feas=False, obj=-1.49]
INFO - 16:23:25: Optimization result:
INFO - 16:23:25: Optimizer info:
INFO - 16:23:25: Status: 8
INFO - 16:23:25: Message: Positive directional derivative for linesearch
INFO - 16:23:25: Solution:
WARNING - 16:23:25: The solution is not feasible.
INFO - 16:23:25: Objective: -1.4868788429690418
INFO - 16:23:25: Standardized constraints:
INFO - 16:23:25: g_2 = 0.007145549037898213
INFO - 16:23:25: Design space:
INFO - 16:23:25: +------+-------------+-------+-------------+-------+
INFO - 16:23:25: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:25: +------+-------------+-------+-------------+-------+
INFO - 16:23:25: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:25: +------+-------------+-------+-------------+-------+
INFO - 16:23:25: *** End AerodynamicsScenario execution (time: 0:00:00.010902) ***
INFO - 16:23:25: *** Start StructureScenario execution ***
INFO - 16:23:25: StructureScenario
INFO - 16:23:25: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:25: MDO formulation: MDF
INFO - 16:23:25: Optimization problem:
INFO - 16:23:25: minimize 0.001*-y_4(x_1)
INFO - 16:23:25: with respect to x_1
INFO - 16:23:25: under the inequality constraints
INFO - 16:23:25: g_1(x_1) <= 0
INFO - 16:23:25: over the design space:
INFO - 16:23:25: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:25: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:25: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:25: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:25: | x_1[1] | 0.75 | 0.7806436800678812 | 1.25 | float |
INFO - 16:23:25: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:25: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:25: 2%|▏ | 1/50 [00:00<00:00, 102.62 it/sec, feas=True, obj=-1.49]
INFO - 16:23:25: Optimization result:
INFO - 16:23:25: Optimizer info:
INFO - 16:23:25: Status: 8
INFO - 16:23:25: Message: Positive directional derivative for linesearch
INFO - 16:23:25: Solution:
INFO - 16:23:25: The solution is feasible.
INFO - 16:23:25: Objective: -1.4868788429690418
INFO - 16:23:25: Standardized constraints:
INFO - 16:23:25: g_1 = [-6.04548408e-02 -3.41428436e-02 -3.45469888e-02 -3.91287220e-02
INFO - 16:23:25: -4.39912300e-02 -2.40000001e-01 1.13532961e-09]
INFO - 16:23:25: Design space:
INFO - 16:23:25: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:25: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:25: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:25: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:25: | x_1[1] | 0.75 | 0.7806436800678812 | 1.25 | float |
INFO - 16:23:25: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:25: *** End StructureScenario execution (time: 0:00:00.011582) ***
INFO - 16:23:25: 9%|▉ | 9/100 [00:09<01:31, 59.54 it/min, feas=False, obj=-1.49]
INFO - 16:23:25: *** Start PropulsionScenario execution ***
INFO - 16:23:25: PropulsionScenario
INFO - 16:23:25: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:25: MDO formulation: MDF
INFO - 16:23:25: Optimization problem:
INFO - 16:23:25: minimize 0.001*-y_4(x_3)
INFO - 16:23:25: with respect to x_3
INFO - 16:23:25: under the inequality constraints
INFO - 16:23:25: g_3(x_3) <= 0
INFO - 16:23:25: over the design space:
INFO - 16:23:25: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:25: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:25: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:25: | x_3 | 0.1 | 0.2260985585830691 | 1 | float |
INFO - 16:23:25: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:25: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:26: 2%|▏ | 1/50 [00:00<00:01, 40.22 it/sec, feas=False, obj=-1.68]
INFO - 16:23:26: 4%|▍ | 2/50 [00:00<00:01, 40.86 it/sec, feas=True, obj=-1.66]
INFO - 16:23:26: 6%|▌ | 3/50 [00:00<00:01, 33.33 it/sec, feas=False, obj=-1.68]
INFO - 16:23:26: 8%|▊ | 4/50 [00:00<00:01, 34.93 it/sec, feas=True, obj=-1.66]
INFO - 16:23:26: 10%|█ | 5/50 [00:00<00:01, 36.00 it/sec, feas=False, obj=-1.68]
INFO - 16:23:26: 12%|█▏ | 6/50 [00:00<00:01, 33.54 it/sec, feas=False, obj=-1.68]
INFO - 16:23:26: 14%|█▍ | 7/50 [00:00<00:01, 34.41 it/sec, feas=True, obj=-1.66]
INFO - 16:23:26: 16%|█▌ | 8/50 [00:00<00:01, 35.33 it/sec, feas=False, obj=-1.68]
INFO - 16:23:26: 18%|█▊ | 9/50 [00:00<00:01, 35.93 it/sec, feas=False, obj=-1.68]
INFO - 16:23:26: 20%|██ | 10/50 [00:00<00:01, 34.42 it/sec, feas=False, obj=-1.68]
INFO - 16:23:26: 22%|██▏ | 11/50 [00:00<00:01, 34.97 it/sec, feas=False, obj=-1.68]
INFO - 16:23:26: 24%|██▍ | 12/50 [00:00<00:01, 35.44 it/sec, feas=False, obj=-1.68]
INFO - 16:23:26: 26%|██▌ | 13/50 [00:00<00:01, 34.39 it/sec, feas=False, obj=-1.68]
INFO - 16:23:26: 28%|██▊ | 14/50 [00:00<00:01, 34.92 it/sec, feas=False, obj=-1.68]
INFO - 16:23:26: 30%|███ | 15/50 [00:00<00:00, 35.32 it/sec, feas=False, obj=-1.68]
INFO - 16:23:26: 32%|███▏ | 16/50 [00:00<00:01, 31.57 it/sec, feas=False, obj=-1.68]
WARNING - 16:23:26: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 6.724932466608626e-05 is still above the tolerance 1e-06.
INFO - 16:23:26: 34%|███▍ | 17/50 [00:00<00:01, 31.65 it/sec, feas=True, obj=-1.66]
INFO - 16:23:26: 36%|███▌ | 18/50 [00:00<00:01, 31.89 it/sec, feas=True, obj=-1.66]
INFO - 16:23:26: 38%|███▊ | 19/50 [00:00<00:00, 32.20 it/sec, feas=True, obj=-1.66]
INFO - 16:23:26: Optimization result:
INFO - 16:23:26: Optimizer info:
INFO - 16:23:26: Status: None
INFO - 16:23:26: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:26: Solution:
INFO - 16:23:26: The solution is feasible.
INFO - 16:23:26: Objective: -1.6551926457432993
INFO - 16:23:26: Standardized constraints:
INFO - 16:23:26: g_3 = [-7.07448563e-01 -2.92551437e-01 7.54951657e-15 -1.60338232e-01]
INFO - 16:23:26: Design space:
INFO - 16:23:26: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:26: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:26: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:26: | x_3 | 0.1 | 0.2138481092692222 | 1 | float |
INFO - 16:23:26: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:26: *** End PropulsionScenario execution (time: 0:00:00.593238) ***
INFO - 16:23:26: *** Start AerodynamicsScenario execution ***
INFO - 16:23:26: AerodynamicsScenario
INFO - 16:23:26: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:26: MDO formulation: MDF
INFO - 16:23:26: Optimization problem:
INFO - 16:23:26: minimize 0.001*-y_4(x_2)
INFO - 16:23:26: with respect to x_2
INFO - 16:23:26: under the inequality constraints
INFO - 16:23:26: g_2(x_2) <= 0
INFO - 16:23:26: over the design space:
INFO - 16:23:26: +------+-------------+-------+-------------+-------+
INFO - 16:23:26: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:26: +------+-------------+-------+-------------+-------+
INFO - 16:23:26: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:26: +------+-------------+-------+-------------+-------+
INFO - 16:23:26: Solving optimization problem with algorithm SLSQP:
WARNING - 16:23:26: Optimization found no feasible point; the least infeasible point is selected.
INFO - 16:23:26: 2%|▏ | 1/50 [00:00<00:00, 74.50 it/sec, feas=False, obj=-1.66]
INFO - 16:23:26: Optimization result:
INFO - 16:23:26: Optimizer info:
INFO - 16:23:26: Status: 8
INFO - 16:23:26: Message: Positive directional derivative for linesearch
INFO - 16:23:26: Solution:
WARNING - 16:23:26: The solution is not feasible.
INFO - 16:23:26: Objective: -1.6551926457432993
INFO - 16:23:26: Standardized constraints:
INFO - 16:23:26: g_2 = 0.010000000000000009
INFO - 16:23:26: Design space:
INFO - 16:23:26: +------+-------------+-------+-------------+-------+
INFO - 16:23:26: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:26: +------+-------------+-------+-------------+-------+
INFO - 16:23:26: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:26: +------+-------------+-------+-------------+-------+
INFO - 16:23:26: *** End AerodynamicsScenario execution (time: 0:00:00.015129) ***
INFO - 16:23:26: *** Start StructureScenario execution ***
INFO - 16:23:26: StructureScenario
INFO - 16:23:26: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:26: MDO formulation: MDF
INFO - 16:23:26: Optimization problem:
INFO - 16:23:26: minimize 0.001*-y_4(x_1)
INFO - 16:23:26: with respect to x_1
INFO - 16:23:26: under the inequality constraints
INFO - 16:23:26: g_1(x_1) <= 0
INFO - 16:23:26: over the design space:
INFO - 16:23:26: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:26: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:26: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:26: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:26: | x_1[1] | 0.75 | 0.7806436800678812 | 1.25 | float |
INFO - 16:23:26: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:26: Solving optimization problem with algorithm SLSQP:
WARNING - 16:23:26: MDAGaussSeidel has reached its maximum number of unsuccessful iterations, but the normalized residual norm 0.0009157477359807847 is still above the tolerance 1e-06.
INFO - 16:23:26: 2%|▏ | 1/50 [00:00<00:00, 53.38 it/sec, feas=True, obj=-1.66]
INFO - 16:23:26: 4%|▍ | 2/50 [00:00<00:01, 30.83 it/sec, feas=True, obj=-1.68]
INFO - 16:23:26: 6%|▌ | 3/50 [00:00<00:01, 27.86 it/sec, feas=True, obj=-1.68]
WARNING - 16:23:26: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 0.0018314954719615695 is still above the tolerance 1e-06.
INFO - 16:23:26: 8%|▊ | 4/50 [00:00<00:01, 25.86 it/sec, feas=True, obj=-1.68]
INFO - 16:23:26: 10%|█ | 5/50 [00:00<00:01, 25.08 it/sec, feas=True, obj=-1.68]
INFO - 16:23:26: 12%|█▏ | 6/50 [00:00<00:01, 24.66 it/sec, feas=True, obj=-1.68]
INFO - 16:23:26: 14%|█▍ | 7/50 [00:00<00:01, 24.52 it/sec, feas=True, obj=-1.68]
INFO - 16:23:26: 16%|█▌ | 8/50 [00:00<00:01, 24.43 it/sec, feas=True, obj=-1.68]
INFO - 16:23:26: 18%|█▊ | 9/50 [00:00<00:01, 24.39 it/sec, feas=True, obj=-1.68]
INFO - 16:23:26: 20%|██ | 10/50 [00:00<00:01, 24.30 it/sec, feas=True, obj=-1.68]
INFO - 16:23:27: 22%|██▏ | 11/50 [00:00<00:01, 25.18 it/sec, feas=True, obj=-1.68]
INFO - 16:23:27: Optimization result:
INFO - 16:23:27: Optimizer info:
INFO - 16:23:27: Status: None
INFO - 16:23:27: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:27: Solution:
INFO - 16:23:27: The solution is feasible.
INFO - 16:23:27: Objective: -1.6834228475014819
INFO - 16:23:27: Standardized constraints:
INFO - 16:23:27: g_1 = [-3.08368226e-02 -1.97344151e-02 -2.57420113e-02 -3.30453850e-02
INFO - 16:23:27: -3.94554742e-02 -2.40000000e-01 5.88418203e-15]
INFO - 16:23:27: Design space:
INFO - 16:23:27: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:27: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:27: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:27: | x_1[0] | 0.1 | 0.2701423180096785 | 0.4 | float |
INFO - 16:23:27: | x_1[1] | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:27: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:27: *** End StructureScenario execution (time: 0:00:00.439419) ***
INFO - 16:23:27: *** Start PropulsionScenario execution ***
INFO - 16:23:27: PropulsionScenario
INFO - 16:23:27: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:27: MDO formulation: MDF
INFO - 16:23:27: Optimization problem:
INFO - 16:23:27: minimize 0.001*-y_4(x_3)
INFO - 16:23:27: with respect to x_3
INFO - 16:23:27: under the inequality constraints
INFO - 16:23:27: g_3(x_3) <= 0
INFO - 16:23:27: over the design space:
INFO - 16:23:27: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:27: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:27: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:27: | x_3 | 0.1 | 0.2138481092692222 | 1 | float |
INFO - 16:23:27: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:27: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:27: 2%|▏ | 1/50 [00:00<00:00, 83.30 it/sec, feas=True, obj=-1.68]
INFO - 16:23:27: Optimization result:
INFO - 16:23:27: Optimizer info:
INFO - 16:23:27: Status: 8
INFO - 16:23:27: Message: Positive directional derivative for linesearch
INFO - 16:23:27: Solution:
INFO - 16:23:27: The solution is feasible.
INFO - 16:23:27: Objective: -1.6834228475014819
INFO - 16:23:27: Standardized constraints:
INFO - 16:23:27: g_3 = [-7.07260344e-01 -2.92739656e-01 7.54951657e-15 -1.60338232e-01]
INFO - 16:23:27: Design space:
INFO - 16:23:27: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:27: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:27: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:27: | x_3 | 0.1 | 0.2138481092692222 | 1 | float |
INFO - 16:23:27: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:27: *** End PropulsionScenario execution (time: 0:00:00.013982) ***
INFO - 16:23:27: *** Start AerodynamicsScenario execution ***
INFO - 16:23:27: AerodynamicsScenario
INFO - 16:23:27: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:27: MDO formulation: MDF
INFO - 16:23:27: Optimization problem:
INFO - 16:23:27: minimize 0.001*-y_4(x_2)
INFO - 16:23:27: with respect to x_2
INFO - 16:23:27: under the inequality constraints
INFO - 16:23:27: g_2(x_2) <= 0
INFO - 16:23:27: over the design space:
INFO - 16:23:27: +------+-------------+-------+-------------+-------+
INFO - 16:23:27: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:27: +------+-------------+-------+-------------+-------+
INFO - 16:23:27: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:27: +------+-------------+-------+-------------+-------+
INFO - 16:23:27: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:27: 2%|▏ | 1/50 [00:00<00:00, 108.76 it/sec, feas=False, obj=-1.68]
INFO - 16:23:27: 4%|▍ | 2/50 [00:00<00:00, 171.12 it/sec, feas=False, obj=-1.68]
INFO - 16:23:27: 6%|▌ | 3/50 [00:00<00:00, 212.26 it/sec, feas=False, obj=-1.68]
INFO - 16:23:27: 8%|▊ | 4/50 [00:00<00:00, 238.19 it/sec, feas=False, obj=-1.68]
INFO - 16:23:27: 10%|█ | 5/50 [00:00<00:00, 258.94 it/sec, feas=False, obj=-1.68]
INFO - 16:23:27: 12%|█▏ | 6/50 [00:00<00:00, 275.51 it/sec, feas=False, obj=-1.68]
INFO - 16:23:27: 14%|█▍ | 7/50 [00:00<00:00, 288.41 it/sec, feas=False, obj=-1.68]
INFO - 16:23:27: 16%|█▌ | 8/50 [00:00<00:00, 299.28 it/sec, feas=False, obj=-1.68]
INFO - 16:23:27: 18%|█▊ | 9/50 [00:00<00:00, 309.21 it/sec, feas=False, obj=-1.68]
INFO - 16:23:27: 20%|██ | 10/50 [00:00<00:00, 318.70 it/sec, feas=False, obj=-1.68]
INFO - 16:23:27: 22%|██▏ | 11/50 [00:00<00:00, 330.23 it/sec, feas=False, obj=-1.68]
INFO - 16:23:27: 24%|██▍ | 12/50 [00:00<00:00, 230.41 it/sec, feas=False, obj=-1.68]
INFO - 16:23:27: 26%|██▌ | 13/50 [00:00<00:00, 238.34 it/sec, feas=False, obj=-1.68]
INFO - 16:23:27: 28%|██▊ | 14/50 [00:00<00:00, 245.18 it/sec, feas=False, obj=-1.68]
INFO - 16:23:27: 30%|███ | 15/50 [00:00<00:00, 251.56 it/sec, feas=False, obj=-1.68]
INFO - 16:23:27: 32%|███▏ | 16/50 [00:00<00:00, 257.46 it/sec, feas=False, obj=-1.68]
INFO - 16:23:27: 34%|███▍ | 17/50 [00:00<00:00, 262.23 it/sec, feas=False, obj=-1.68]
INFO - 16:23:27: 36%|███▌ | 18/50 [00:00<00:00, 267.25 it/sec, feas=False, obj=-1.68]
INFO - 16:23:27: 38%|███▊ | 19/50 [00:00<00:00, 271.45 it/sec, feas=False, obj=-1.68]
INFO - 16:23:27: 40%|████ | 20/50 [00:00<00:00, 275.75 it/sec, feas=False, obj=-1.68]
INFO - 16:23:27: 42%|████▏ | 21/50 [00:00<00:00, 279.76 it/sec, feas=False, obj=-1.68]
INFO - 16:23:27: 44%|████▍ | 22/50 [00:00<00:00, 283.60 it/sec, feas=False, obj=-1.68]
INFO - 16:23:27: 46%|████▌ | 23/50 [00:00<00:00, 239.85 it/sec, feas=False, obj=-1.68]
INFO - 16:23:27: 48%|████▊ | 24/50 [00:00<00:00, 244.84 it/sec, feas=False, obj=-1.68]
INFO - 16:23:27: 50%|█████ | 25/50 [00:00<00:00, 246.26 it/sec, feas=False, obj=-1.68]
INFO - 16:23:27: 52%|█████▏ | 26/50 [00:00<00:00, 250.31 it/sec, feas=False, obj=-1.68]
INFO - 16:23:27: 54%|█████▍ | 27/50 [00:00<00:00, 253.97 it/sec, feas=False, obj=-1.68]
INFO - 16:23:27: 56%|█████▌ | 28/50 [00:00<00:00, 257.10 it/sec, feas=False, obj=-1.68]
INFO - 16:23:27: 58%|█████▊ | 29/50 [00:00<00:00, 260.85 it/sec, feas=False, obj=-1.68]
INFO - 16:23:27: 60%|██████ | 30/50 [00:00<00:00, 262.81 it/sec, feas=False, obj=-1.68]
INFO - 16:23:27: 62%|██████▏ | 31/50 [00:00<00:00, 265.70 it/sec, feas=False, obj=-1.68]
INFO - 16:23:27: 64%|██████▍ | 32/50 [00:00<00:00, 268.44 it/sec, feas=False, obj=-1.68]
INFO - 16:23:27: 66%|██████▌ | 33/50 [00:00<00:00, 271.09 it/sec, feas=False, obj=-1.68]
INFO - 16:23:27: 68%|██████▊ | 34/50 [00:00<00:00, 273.60 it/sec, feas=False, obj=-1.68]
INFO - 16:23:27: 70%|███████ | 35/50 [00:00<00:00, 276.02 it/sec, feas=False, obj=-1.68]
INFO - 16:23:27: 72%|███████▏ | 36/50 [00:00<00:00, 278.23 it/sec, feas=False, obj=-1.68]
INFO - 16:23:27: 74%|███████▍ | 37/50 [00:00<00:00, 280.51 it/sec, feas=False, obj=-1.68]
INFO - 16:23:27: 76%|███████▌ | 38/50 [00:00<00:00, 282.65 it/sec, feas=False, obj=-1.68]
INFO - 16:23:27: 78%|███████▊ | 39/50 [00:00<00:00, 284.77 it/sec, feas=False, obj=-1.68]
INFO - 16:23:27: 80%|████████ | 40/50 [00:00<00:00, 286.83 it/sec, feas=False, obj=-1.68]
INFO - 16:23:27: 82%|████████▏ | 41/50 [00:00<00:00, 258.04 it/sec, feas=False, obj=-1.68]
INFO - 16:23:27: 84%|████████▍ | 42/50 [00:00<00:00, 257.99 it/sec, feas=False, obj=-1.68]
INFO - 16:23:27: 86%|████████▌ | 43/50 [00:00<00:00, 260.11 it/sec, feas=False, obj=-1.68]
INFO - 16:23:27: 88%|████████▊ | 44/50 [00:00<00:00, 255.36 it/sec, feas=False, obj=-1.68]
INFO - 16:23:27: 90%|█████████ | 45/50 [00:00<00:00, 257.27 it/sec, feas=False, obj=-1.68]
INFO - 16:23:27: 92%|█████████▏| 46/50 [00:00<00:00, 259.21 it/sec, feas=False, obj=-1.68]
INFO - 16:23:27: 94%|█████████▍| 47/50 [00:00<00:00, 261.19 it/sec, feas=False, obj=-1.68]
INFO - 16:23:27: 96%|█████████▌| 48/50 [00:00<00:00, 263.09 it/sec, feas=False, obj=-1.68]
INFO - 16:23:27: 98%|█████████▊| 49/50 [00:00<00:00, 264.94 it/sec, feas=False, obj=-1.68]
INFO - 16:23:27: 100%|██████████| 50/50 [00:00<00:00, 266.62 it/sec, feas=False, obj=-1.68]
WARNING - 16:23:27: Optimization found no feasible point; the least infeasible point is selected.
INFO - 16:23:27: Optimization result:
INFO - 16:23:27: Optimizer info:
INFO - 16:23:27: Status: None
INFO - 16:23:27: Message: Maximum number of iterations reached. GEMSEO stopped the driver.
INFO - 16:23:27: Solution:
WARNING - 16:23:27: The solution is not feasible.
INFO - 16:23:27: Objective: -1.6834228475014819
INFO - 16:23:27: Standardized constraints:
INFO - 16:23:27: g_2 = 0.010000000000000009
INFO - 16:23:27: Design space:
INFO - 16:23:27: +------+-------------+-------+-------------+-------+
INFO - 16:23:27: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:27: +------+-------------+-------+-------------+-------+
INFO - 16:23:27: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:27: +------+-------------+-------+-------------+-------+
INFO - 16:23:27: *** End AerodynamicsScenario execution (time: 0:00:00.190218) ***
INFO - 16:23:27: *** Start StructureScenario execution ***
INFO - 16:23:27: StructureScenario
INFO - 16:23:27: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:27: MDO formulation: MDF
INFO - 16:23:27: Optimization problem:
INFO - 16:23:27: minimize 0.001*-y_4(x_1)
INFO - 16:23:27: with respect to x_1
INFO - 16:23:27: under the inequality constraints
INFO - 16:23:27: g_1(x_1) <= 0
INFO - 16:23:27: over the design space:
INFO - 16:23:27: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:27: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:27: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:27: | x_1[0] | 0.1 | 0.2701423180096785 | 0.4 | float |
INFO - 16:23:27: | x_1[1] | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:27: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:27: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:27: 2%|▏ | 1/50 [00:00<00:00, 80.48 it/sec, feas=True, obj=-1.68]
INFO - 16:23:27: Optimization result:
INFO - 16:23:27: Optimizer info:
INFO - 16:23:27: Status: 8
INFO - 16:23:27: Message: Positive directional derivative for linesearch
INFO - 16:23:27: Solution:
INFO - 16:23:27: The solution is feasible.
INFO - 16:23:27: Objective: -1.6834228475014819
INFO - 16:23:27: Standardized constraints:
INFO - 16:23:27: g_1 = [-3.08368226e-02 -1.97344151e-02 -2.57420113e-02 -3.30453850e-02
INFO - 16:23:27: -3.94554742e-02 -2.40000000e-01 5.88418203e-15]
INFO - 16:23:27: Design space:
INFO - 16:23:27: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:27: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:27: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:27: | x_1[0] | 0.1 | 0.2701423180096786 | 0.4 | float |
INFO - 16:23:27: | x_1[1] | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:27: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:27: *** End StructureScenario execution (time: 0:00:00.014826) ***
WARNING - 16:23:27: MDAJacobi has reached its maximum number of iterations, but the normalized residual norm 6.752480683125322e-06 is still above the tolerance 1e-06.
INFO - 16:23:27: 10%|█ | 10/100 [00:10<01:33, 57.82 it/min, feas=False, obj=-1.68]
INFO - 16:23:27: *** Start PropulsionScenario execution ***
INFO - 16:23:27: PropulsionScenario
INFO - 16:23:27: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:27: MDO formulation: MDF
INFO - 16:23:27: Optimization problem:
INFO - 16:23:27: minimize 0.001*-y_4(x_3)
INFO - 16:23:27: with respect to x_3
INFO - 16:23:27: under the inequality constraints
INFO - 16:23:27: g_3(x_3) <= 0
INFO - 16:23:27: over the design space:
INFO - 16:23:27: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:27: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:27: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:27: | x_3 | 0.1 | 0.2138481092692222 | 1 | float |
INFO - 16:23:27: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:27: Solving optimization problem with algorithm SLSQP:
WARNING - 16:23:27: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 0.0021519783893147603 is still above the tolerance 1e-06.
INFO - 16:23:27: 2%|▏ | 1/50 [00:00<00:01, 33.00 it/sec, feas=True, obj=-1.27]
WARNING - 16:23:27: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 0.0022192277139808465 is still above the tolerance 1e-06.
INFO - 16:23:27: 4%|▍ | 2/50 [00:00<00:01, 25.77 it/sec, feas=True, obj=-1.3]
WARNING - 16:23:27: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 0.002185603051647803 is still above the tolerance 1e-06.
INFO - 16:23:27: 6%|▌ | 3/50 [00:00<00:01, 24.07 it/sec, feas=True, obj=-1.3]
WARNING - 16:23:27: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 0.0021519783893147603 is still above the tolerance 1e-06.
INFO - 16:23:27: 8%|▊ | 4/50 [00:00<00:01, 25.70 it/sec, feas=True, obj=-1.3]
INFO - 16:23:27: Optimization result:
INFO - 16:23:27: Optimizer info:
INFO - 16:23:27: Status: None
INFO - 16:23:27: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:27: Solution:
INFO - 16:23:27: The solution is feasible.
INFO - 16:23:27: Objective: -1.3016863762010553
INFO - 16:23:27: Standardized constraints:
INFO - 16:23:27: g_3 = [-8.47756711e-01 -1.52243289e-01 3.33066907e-15 -1.44484273e-01]
INFO - 16:23:27: Design space:
INFO - 16:23:27: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:27: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:27: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:27: | x_3 | 0.1 | 0.2470833052880812 | 1 | float |
INFO - 16:23:27: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:27: *** End PropulsionScenario execution (time: 0:00:00.158325) ***
INFO - 16:23:27: *** Start AerodynamicsScenario execution ***
INFO - 16:23:27: AerodynamicsScenario
INFO - 16:23:27: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:27: MDO formulation: MDF
INFO - 16:23:27: Optimization problem:
INFO - 16:23:27: minimize 0.001*-y_4(x_2)
INFO - 16:23:27: with respect to x_2
INFO - 16:23:27: under the inequality constraints
INFO - 16:23:27: g_2(x_2) <= 0
INFO - 16:23:27: over the design space:
INFO - 16:23:27: +------+-------------+-------+-------------+-------+
INFO - 16:23:27: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:27: +------+-------------+-------+-------------+-------+
INFO - 16:23:27: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:27: +------+-------------+-------+-------------+-------+
INFO - 16:23:27: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:27: 2%|▏ | 1/50 [00:00<00:00, 70.74 it/sec, feas=True, obj=-1.3]
INFO - 16:23:27: Optimization result:
INFO - 16:23:27: Optimizer info:
INFO - 16:23:27: Status: 8
INFO - 16:23:27: Message: Positive directional derivative for linesearch
INFO - 16:23:27: Solution:
INFO - 16:23:27: The solution is feasible.
INFO - 16:23:27: Objective: -1.3016863762010549
INFO - 16:23:27: Standardized constraints:
INFO - 16:23:27: g_2 = -0.025124012073195257
INFO - 16:23:27: Design space:
INFO - 16:23:27: +------+-------------+-------+-------------+-------+
INFO - 16:23:27: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:27: +------+-------------+-------+-------------+-------+
INFO - 16:23:27: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:27: +------+-------------+-------+-------------+-------+
INFO - 16:23:27: *** End AerodynamicsScenario execution (time: 0:00:00.015864) ***
INFO - 16:23:27: *** Start StructureScenario execution ***
INFO - 16:23:27: StructureScenario
INFO - 16:23:27: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:27: MDO formulation: MDF
INFO - 16:23:27: Optimization problem:
INFO - 16:23:27: minimize 0.001*-y_4(x_1)
INFO - 16:23:27: with respect to x_1
INFO - 16:23:27: under the inequality constraints
INFO - 16:23:27: g_1(x_1) <= 0
INFO - 16:23:27: over the design space:
INFO - 16:23:27: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:27: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:27: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:27: | x_1[0] | 0.1 | 0.2701423180096786 | 0.4 | float |
INFO - 16:23:27: | x_1[1] | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:27: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:27: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:27: 2%|▏ | 1/50 [00:00<00:00, 81.87 it/sec, feas=False, obj=-1.3]
WARNING - 16:23:27: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 104644.85641517532 is still above the tolerance 1e-06.
INFO - 16:23:27: 4%|▍ | 2/50 [00:00<00:01, 33.39 it/sec, feas=True, obj=-1.1]
WARNING - 16:23:27: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 70.04013442918753 is still above the tolerance 1e-06.
INFO - 16:23:27: 6%|▌ | 3/50 [00:00<00:01, 27.76 it/sec, feas=True, obj=-1.14]
WARNING - 16:23:27: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 11.373600790819273 is still above the tolerance 1e-06.
INFO - 16:23:27: 8%|▊ | 4/50 [00:00<00:01, 25.26 it/sec, feas=True, obj=-1.15]
WARNING - 16:23:27: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 10.203273731032082 is still above the tolerance 1e-06.
INFO - 16:23:27: 10%|█ | 5/50 [00:00<00:01, 24.17 it/sec, feas=True, obj=-1.15]
WARNING - 16:23:27: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 7.545770325961933 is still above the tolerance 1e-06.
INFO - 16:23:27: 12%|█▏ | 6/50 [00:00<00:01, 23.43 it/sec, feas=True, obj=-1.15]
WARNING - 16:23:27: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 2.0439516135354707 is still above the tolerance 1e-06.
INFO - 16:23:27: 14%|█▍ | 7/50 [00:00<00:01, 23.00 it/sec, feas=True, obj=-1.15]
WARNING - 16:23:27: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 1.8937686445313882 is still above the tolerance 1e-06.
INFO - 16:23:27: 16%|█▌ | 8/50 [00:00<00:01, 22.32 it/sec, feas=True, obj=-1.15]
WARNING - 16:23:27: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 1.8937686220445615 is still above the tolerance 1e-06.
INFO - 16:23:27: 18%|█▊ | 9/50 [00:00<00:01, 22.14 it/sec, feas=True, obj=-1.15]
WARNING - 16:23:27: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 1.8901057464847377 is still above the tolerance 1e-06.
INFO - 16:23:27: 20%|██ | 10/50 [00:00<00:01, 21.95 it/sec, feas=True, obj=-1.15]
WARNING - 16:23:27: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 1.893768732748937 is still above the tolerance 1e-06.
INFO - 16:23:27: 22%|██▏ | 11/50 [00:00<00:01, 21.85 it/sec, feas=True, obj=-1.15]
INFO - 16:23:27: Optimization result:
INFO - 16:23:27: Optimizer info:
INFO - 16:23:27: Status: None
INFO - 16:23:27: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:27: Solution:
INFO - 16:23:27: The solution is feasible.
INFO - 16:23:27: Objective: -1.1517798924997527
INFO - 16:23:27: Standardized constraints:
INFO - 16:23:27: g_1 = [ 3.94280164e-11 -1.58056140e-02 -2.90313158e-02 -3.86700631e-02
INFO - 16:23:27: -4.58056140e-02 -1.64098390e-01 -7.59016097e-02]
INFO - 16:23:27: Design space:
INFO - 16:23:27: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:27: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:27: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:27: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:27: | x_1[1] | 0.75 | 0.9931810172443312 | 1.25 | float |
INFO - 16:23:27: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:27: *** End StructureScenario execution (time: 0:00:00.506425) ***
WARNING - 16:23:27: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 1.8937686220445615 is still above the tolerance 1e-06.
INFO - 16:23:27: *** Start PropulsionScenario execution ***
INFO - 16:23:27: PropulsionScenario
INFO - 16:23:27: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:27: MDO formulation: MDF
INFO - 16:23:27: Optimization problem:
INFO - 16:23:27: minimize 0.001*-y_4(x_3)
INFO - 16:23:27: with respect to x_3
INFO - 16:23:27: under the inequality constraints
INFO - 16:23:27: g_3(x_3) <= 0
INFO - 16:23:27: over the design space:
INFO - 16:23:27: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:27: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:27: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:27: | x_3 | 0.1 | 0.2470833052880812 | 1 | float |
INFO - 16:23:27: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:27: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:28: 2%|▏ | 1/50 [00:00<00:00, 62.21 it/sec, feas=True, obj=-1.15]
INFO - 16:23:28: 4%|▍ | 2/50 [00:00<00:00, 49.44 it/sec, feas=True, obj=-1.15]
INFO - 16:23:28: 6%|▌ | 3/50 [00:00<00:00, 62.77 it/sec, feas=True, obj=-1.15]
INFO - 16:23:28: Optimization result:
INFO - 16:23:28: Optimizer info:
INFO - 16:23:28: Status: None
INFO - 16:23:28: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:28: Solution:
INFO - 16:23:28: The solution is feasible.
INFO - 16:23:28: Objective: -1.1517798924997469
INFO - 16:23:28: Standardized constraints:
INFO - 16:23:28: g_3 = [-8.47150633e-01 -1.52849367e-01 3.33066907e-15 -1.44484273e-01]
INFO - 16:23:28: Design space:
INFO - 16:23:28: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:28: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:28: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:28: | x_3 | 0.1 | 0.2470833052880812 | 1 | float |
INFO - 16:23:28: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:28: *** End PropulsionScenario execution (time: 0:00:00.050371) ***
INFO - 16:23:28: *** Start AerodynamicsScenario execution ***
INFO - 16:23:28: AerodynamicsScenario
INFO - 16:23:28: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:28: MDO formulation: MDF
INFO - 16:23:28: Optimization problem:
INFO - 16:23:28: minimize 0.001*-y_4(x_2)
INFO - 16:23:28: with respect to x_2
INFO - 16:23:28: under the inequality constraints
INFO - 16:23:28: g_2(x_2) <= 0
INFO - 16:23:28: over the design space:
INFO - 16:23:28: +------+-------------+-------+-------------+-------+
INFO - 16:23:28: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:28: +------+-------------+-------+-------------+-------+
INFO - 16:23:28: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:28: +------+-------------+-------+-------------+-------+
INFO - 16:23:28: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:28: 2%|▏ | 1/50 [00:00<00:00, 78.61 it/sec, feas=True, obj=-1.15]
INFO - 16:23:28: Optimization result:
INFO - 16:23:28: Optimizer info:
INFO - 16:23:28: Status: 8
INFO - 16:23:28: Message: Positive directional derivative for linesearch
INFO - 16:23:28: Solution:
INFO - 16:23:28: The solution is feasible.
INFO - 16:23:28: Objective: -1.1517798924997469
INFO - 16:23:28: Standardized constraints:
INFO - 16:23:28: g_2 = -0.025124012073195257
INFO - 16:23:28: Design space:
INFO - 16:23:28: +------+-------------+-------+-------------+-------+
INFO - 16:23:28: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:28: +------+-------------+-------+-------------+-------+
INFO - 16:23:28: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:28: +------+-------------+-------+-------------+-------+
INFO - 16:23:28: *** End AerodynamicsScenario execution (time: 0:00:00.014469) ***
INFO - 16:23:28: *** Start StructureScenario execution ***
INFO - 16:23:28: StructureScenario
INFO - 16:23:28: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:28: MDO formulation: MDF
INFO - 16:23:28: Optimization problem:
INFO - 16:23:28: minimize 0.001*-y_4(x_1)
INFO - 16:23:28: with respect to x_1
INFO - 16:23:28: under the inequality constraints
INFO - 16:23:28: g_1(x_1) <= 0
INFO - 16:23:28: over the design space:
INFO - 16:23:28: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:28: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:28: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:28: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:28: | x_1[1] | 0.75 | 0.9931810172443312 | 1.25 | float |
INFO - 16:23:28: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:28: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:28: 2%|▏ | 1/50 [00:00<00:00, 102.14 it/sec, feas=True, obj=-1.15]
INFO - 16:23:28: Optimization result:
INFO - 16:23:28: Optimizer info:
INFO - 16:23:28: Status: 8
INFO - 16:23:28: Message: Positive directional derivative for linesearch
INFO - 16:23:28: Solution:
INFO - 16:23:28: The solution is feasible.
INFO - 16:23:28: Objective: -1.1517798924997469
INFO - 16:23:28: Standardized constraints:
INFO - 16:23:28: g_1 = [ 3.94280164e-11 -1.58056140e-02 -2.90313158e-02 -3.86700631e-02
INFO - 16:23:28: -4.58056140e-02 -1.64098390e-01 -7.59016097e-02]
INFO - 16:23:28: Design space:
INFO - 16:23:28: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:28: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:28: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:28: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:28: | x_1[1] | 0.75 | 0.9931810172443312 | 1.25 | float |
INFO - 16:23:28: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:28: *** End StructureScenario execution (time: 0:00:00.011930) ***
INFO - 16:23:28: 11%|█ | 11/100 [00:11<01:30, 59.00 it/min, feas=True, obj=-1.15]
INFO - 16:23:28: *** Start PropulsionScenario execution ***
INFO - 16:23:28: PropulsionScenario
INFO - 16:23:28: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:28: MDO formulation: MDF
INFO - 16:23:28: Optimization problem:
INFO - 16:23:28: minimize 0.001*-y_4(x_3)
INFO - 16:23:28: with respect to x_3
INFO - 16:23:28: under the inequality constraints
INFO - 16:23:28: g_3(x_3) <= 0
INFO - 16:23:28: over the design space:
INFO - 16:23:28: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:28: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:28: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:28: | x_3 | 0.1 | 0.2470833052880812 | 1 | float |
INFO - 16:23:28: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:28: Solving optimization problem with algorithm SLSQP:
WARNING - 16:23:28: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 0.22434418687537944 is still above the tolerance 1e-06.
INFO - 16:23:28: 2%|▏ | 1/50 [00:00<00:01, 33.07 it/sec, feas=False, obj=-1.43]
WARNING - 16:23:28: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 0.20174861715646833 is still above the tolerance 1e-06.
INFO - 16:23:28: 4%|▍ | 2/50 [00:00<00:01, 32.61 it/sec, feas=True, obj=-1.4]
WARNING - 16:23:28: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 0.21506380175990175 is still above the tolerance 1e-06.
WARNING - 16:23:28: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 0.20174861715646833 is still above the tolerance 1e-06.
INFO - 16:23:28: 6%|▌ | 3/50 [00:00<00:02, 18.92 it/sec, feas=False, obj=-1.43]
INFO - 16:23:28: Optimization result:
INFO - 16:23:28: Optimizer info:
INFO - 16:23:28: Status: 8
INFO - 16:23:28: Message: Positive directional derivative for linesearch
INFO - 16:23:28: Solution:
INFO - 16:23:28: The solution is feasible.
INFO - 16:23:28: Objective: -1.4006370207770071
INFO - 16:23:28: Standardized constraints:
INFO - 16:23:28: g_3 = [-0.82112785 -0.17887215 0. -0.16627031]
INFO - 16:23:28: Design space:
INFO - 16:23:28: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:28: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:28: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:28: | x_3 | 0.1 | 0.1991404289646734 | 1 | float |
INFO - 16:23:28: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:28: *** End PropulsionScenario execution (time: 0:00:00.160591) ***
INFO - 16:23:28: *** Start AerodynamicsScenario execution ***
INFO - 16:23:28: AerodynamicsScenario
INFO - 16:23:28: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:28: MDO formulation: MDF
INFO - 16:23:28: Optimization problem:
INFO - 16:23:28: minimize 0.001*-y_4(x_2)
INFO - 16:23:28: with respect to x_2
INFO - 16:23:28: under the inequality constraints
INFO - 16:23:28: g_2(x_2) <= 0
INFO - 16:23:28: over the design space:
INFO - 16:23:28: +------+-------------+-------+-------------+-------+
INFO - 16:23:28: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:28: +------+-------------+-------+-------------+-------+
INFO - 16:23:28: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:28: +------+-------------+-------+-------------+-------+
INFO - 16:23:28: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:28: 2%|▏ | 1/50 [00:00<00:00, 76.30 it/sec, feas=True, obj=-1.4]
INFO - 16:23:28: Optimization result:
INFO - 16:23:28: Optimizer info:
INFO - 16:23:28: Status: 8
INFO - 16:23:28: Message: Positive directional derivative for linesearch
INFO - 16:23:28: Solution:
INFO - 16:23:28: The solution is feasible.
INFO - 16:23:28: Objective: -1.4006370207770165
INFO - 16:23:28: Standardized constraints:
INFO - 16:23:28: g_2 = -0.03718449261165868
INFO - 16:23:28: Design space:
INFO - 16:23:28: +------+-------------+-------+-------------+-------+
INFO - 16:23:28: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:28: +------+-------------+-------+-------------+-------+
INFO - 16:23:28: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:28: +------+-------------+-------+-------------+-------+
INFO - 16:23:28: *** End AerodynamicsScenario execution (time: 0:00:00.014838) ***
INFO - 16:23:28: *** Start StructureScenario execution ***
INFO - 16:23:28: StructureScenario
INFO - 16:23:28: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:28: MDO formulation: MDF
INFO - 16:23:28: Optimization problem:
INFO - 16:23:28: minimize 0.001*-y_4(x_1)
INFO - 16:23:28: with respect to x_1
INFO - 16:23:28: under the inequality constraints
INFO - 16:23:28: g_1(x_1) <= 0
INFO - 16:23:28: over the design space:
INFO - 16:23:28: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:28: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:28: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:28: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:28: | x_1[1] | 0.75 | 0.9931810172443312 | 1.25 | float |
INFO - 16:23:28: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:28: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:28: 2%|▏ | 1/50 [00:00<00:00, 73.20 it/sec, feas=False, obj=-1.4]
WARNING - 16:23:28: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 2505.0174851563265 is still above the tolerance 1e-06.
INFO - 16:23:28: 4%|▍ | 2/50 [00:00<00:01, 32.44 it/sec, feas=True, obj=-1.36]
WARNING - 16:23:28: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 1372.0663186202796 is still above the tolerance 1e-06.
INFO - 16:23:28: 6%|▌ | 3/50 [00:00<00:01, 27.41 it/sec, feas=True, obj=-1.37]
WARNING - 16:23:28: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 1363.1707101976592 is still above the tolerance 1e-06.
INFO - 16:23:28: 8%|▊ | 4/50 [00:00<00:01, 25.38 it/sec, feas=True, obj=-1.37]
WARNING - 16:23:28: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 1363.1652162679575 is still above the tolerance 1e-06.
INFO - 16:23:28: 10%|█ | 5/50 [00:00<00:01, 24.31 it/sec, feas=True, obj=-1.37]
WARNING - 16:23:28: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 1363.170710891848 is still above the tolerance 1e-06.
INFO - 16:23:28: 12%|█▏ | 6/50 [00:00<00:01, 25.35 it/sec, feas=True, obj=-1.37]
WARNING - 16:23:28: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 1363.1652149758172 is still above the tolerance 1e-06.
INFO - 16:23:28: 14%|█▍ | 7/50 [00:00<00:01, 26.16 it/sec, feas=True, obj=-1.37]
INFO - 16:23:28: Optimization result:
INFO - 16:23:28: Optimizer info:
INFO - 16:23:28: Status: None
INFO - 16:23:28: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:28: Solution:
INFO - 16:23:28: The solution is feasible.
INFO - 16:23:28: Objective: -1.3665589931000266
INFO - 16:23:28: Standardized constraints:
INFO - 16:23:28: g_1 = [ 3.69926312e-13 -2.07665850e-02 -3.46124082e-02 -4.40279118e-02
INFO - 16:23:28: -5.07665850e-02 -1.26482078e-01 -1.13517922e-01]
INFO - 16:23:28: Design space:
INFO - 16:23:28: +--------+-------------+-------------------+-------------+-------+
INFO - 16:23:28: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:28: +--------+-------------+-------------------+-------------+-------+
INFO - 16:23:28: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:28: | x_1[1] | 0.75 | 1.083249246018729 | 1.25 | float |
INFO - 16:23:28: +--------+-------------+-------------------+-------------+-------+
INFO - 16:23:28: *** End StructureScenario execution (time: 0:00:00.270276) ***
WARNING - 16:23:28: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 1363.170710891848 is still above the tolerance 1e-06.
INFO - 16:23:28: *** Start PropulsionScenario execution ***
INFO - 16:23:28: PropulsionScenario
INFO - 16:23:28: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:28: MDO formulation: MDF
INFO - 16:23:28: Optimization problem:
INFO - 16:23:28: minimize 0.001*-y_4(x_3)
INFO - 16:23:28: with respect to x_3
INFO - 16:23:28: under the inequality constraints
INFO - 16:23:28: g_3(x_3) <= 0
INFO - 16:23:28: over the design space:
INFO - 16:23:28: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:28: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:28: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:28: | x_3 | 0.1 | 0.1991404289646734 | 1 | float |
INFO - 16:23:28: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:28: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:28: 2%|▏ | 1/50 [00:00<00:01, 41.27 it/sec, feas=True, obj=-1.37]
INFO - 16:23:28: 4%|▍ | 2/50 [00:00<00:00, 49.50 it/sec, feas=True, obj=-1.37]
INFO - 16:23:28: 6%|▌ | 3/50 [00:00<00:00, 51.16 it/sec, feas=True, obj=-1.37]
INFO - 16:23:28: Optimization result:
INFO - 16:23:28: Optimizer info:
INFO - 16:23:28: Status: None
INFO - 16:23:28: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:28: Solution:
INFO - 16:23:28: The solution is feasible.
INFO - 16:23:28: Objective: -1.3665589930955264
INFO - 16:23:28: Standardized constraints:
INFO - 16:23:28: g_3 = [-0.81858532 -0.18141468 0. -0.16627031]
INFO - 16:23:28: Design space:
INFO - 16:23:28: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:28: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:28: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:28: | x_3 | 0.1 | 0.1991404289646734 | 1 | float |
INFO - 16:23:28: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:28: *** End PropulsionScenario execution (time: 0:00:00.061295) ***
INFO - 16:23:28: *** Start AerodynamicsScenario execution ***
INFO - 16:23:28: AerodynamicsScenario
INFO - 16:23:28: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:28: MDO formulation: MDF
INFO - 16:23:28: Optimization problem:
INFO - 16:23:28: minimize 0.001*-y_4(x_2)
INFO - 16:23:28: with respect to x_2
INFO - 16:23:28: under the inequality constraints
INFO - 16:23:28: g_2(x_2) <= 0
INFO - 16:23:28: over the design space:
INFO - 16:23:28: +------+-------------+-------+-------------+-------+
INFO - 16:23:28: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:28: +------+-------------+-------+-------------+-------+
INFO - 16:23:28: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:28: +------+-------------+-------+-------------+-------+
INFO - 16:23:28: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:28: 2%|▏ | 1/50 [00:00<00:00, 81.57 it/sec, feas=True, obj=-1.37]
INFO - 16:23:28: Optimization result:
INFO - 16:23:28: Optimizer info:
INFO - 16:23:28: Status: 8
INFO - 16:23:28: Message: Positive directional derivative for linesearch
INFO - 16:23:28: Solution:
INFO - 16:23:28: The solution is feasible.
INFO - 16:23:28: Objective: -1.3665589930955264
INFO - 16:23:28: Standardized constraints:
INFO - 16:23:28: g_2 = -0.03718449261165868
INFO - 16:23:28: Design space:
INFO - 16:23:28: +------+-------------+-------+-------------+-------+
INFO - 16:23:28: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:28: +------+-------------+-------+-------------+-------+
INFO - 16:23:28: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:28: +------+-------------+-------+-------------+-------+
INFO - 16:23:28: *** End AerodynamicsScenario execution (time: 0:00:00.014047) ***
INFO - 16:23:28: *** Start StructureScenario execution ***
INFO - 16:23:28: StructureScenario
INFO - 16:23:28: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:28: MDO formulation: MDF
INFO - 16:23:28: Optimization problem:
INFO - 16:23:28: minimize 0.001*-y_4(x_1)
INFO - 16:23:28: with respect to x_1
INFO - 16:23:28: under the inequality constraints
INFO - 16:23:28: g_1(x_1) <= 0
INFO - 16:23:28: over the design space:
INFO - 16:23:28: +--------+-------------+-------------------+-------------+-------+
INFO - 16:23:28: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:28: +--------+-------------+-------------------+-------------+-------+
INFO - 16:23:28: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:28: | x_1[1] | 0.75 | 1.083249246018729 | 1.25 | float |
INFO - 16:23:28: +--------+-------------+-------------------+-------------+-------+
INFO - 16:23:28: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:28: 2%|▏ | 1/50 [00:00<00:00, 100.35 it/sec, feas=True, obj=-1.37]
INFO - 16:23:28: 4%|▍ | 2/50 [00:00<00:00, 52.44 it/sec, feas=True, obj=-1.37]
INFO - 16:23:28: 6%|▌ | 3/50 [00:00<00:00, 60.57 it/sec, feas=True, obj=-1.37]
INFO - 16:23:28: Optimization result:
INFO - 16:23:28: Optimizer info:
INFO - 16:23:28: Status: None
INFO - 16:23:28: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:28: Solution:
INFO - 16:23:28: The solution is feasible.
INFO - 16:23:28: Objective: -1.3665589930955264
INFO - 16:23:28: Standardized constraints:
INFO - 16:23:28: g_1 = [ 3.69926312e-13 -2.07665850e-02 -3.46124082e-02 -4.40279118e-02
INFO - 16:23:28: -5.07665850e-02 -1.26482078e-01 -1.13517922e-01]
INFO - 16:23:28: Design space:
INFO - 16:23:28: +--------+-------------+-------------------+-------------+-------+
INFO - 16:23:28: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:28: +--------+-------------+-------------------+-------------+-------+
INFO - 16:23:28: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:28: | x_1[1] | 0.75 | 1.083249246018729 | 1.25 | float |
INFO - 16:23:28: +--------+-------------+-------------------+-------------+-------+
INFO - 16:23:28: *** End StructureScenario execution (time: 0:00:00.052102) ***
INFO - 16:23:28: 12%|█▏ | 12/100 [00:11<01:26, 1.02 it/sec, feas=True, obj=-1.37]
INFO - 16:23:28: *** Start PropulsionScenario execution ***
INFO - 16:23:28: PropulsionScenario
INFO - 16:23:28: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:28: MDO formulation: MDF
INFO - 16:23:28: Optimization problem:
INFO - 16:23:28: minimize 0.001*-y_4(x_3)
INFO - 16:23:28: with respect to x_3
INFO - 16:23:28: under the inequality constraints
INFO - 16:23:28: g_3(x_3) <= 0
INFO - 16:23:28: over the design space:
INFO - 16:23:28: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:28: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:28: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:28: | x_3 | 0.1 | 0.1991404289646734 | 1 | float |
INFO - 16:23:28: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:28: Solving optimization problem with algorithm SLSQP:
WARNING - 16:23:28: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 5.771234315013232 is still above the tolerance 1e-06.
INFO - 16:23:28: 2%|▏ | 1/50 [00:00<00:01, 33.11 it/sec, feas=False, obj=-1.67]
WARNING - 16:23:28: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 11.595172809002072 is still above the tolerance 1e-06.
INFO - 16:23:28: 4%|▍ | 2/50 [00:00<00:01, 33.03 it/sec, feas=True, obj=-1.65]
WARNING - 16:23:28: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 6.742639820304175 is still above the tolerance 1e-06.
INFO - 16:23:28: 6%|▌ | 3/50 [00:00<00:01, 32.38 it/sec, feas=False, obj=-1.67]
WARNING - 16:23:28: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 5.787912256793797 is still above the tolerance 1e-06.
INFO - 16:23:28: 8%|▊ | 4/50 [00:00<00:01, 28.60 it/sec, feas=False, obj=-1.67]
WARNING - 16:23:28: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 6.787966735678046 is still above the tolerance 1e-06.
INFO - 16:23:28: 10%|█ | 5/50 [00:00<00:01, 29.31 it/sec, feas=False, obj=-1.67]
WARNING - 16:23:28: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 5.8067422377669695 is still above the tolerance 1e-06.
INFO - 16:23:28: 12%|█▏ | 6/50 [00:00<00:01, 27.59 it/sec, feas=False, obj=-1.67]
WARNING - 16:23:28: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 11.595038247905833 is still above the tolerance 1e-06.
INFO - 16:23:28: 14%|█▍ | 7/50 [00:00<00:01, 28.17 it/sec, feas=True, obj=-1.65]
WARNING - 16:23:28: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 6.838673441800704 is still above the tolerance 1e-06.
INFO - 16:23:28: 16%|█▌ | 8/50 [00:00<00:01, 28.65 it/sec, feas=False, obj=-1.67]
WARNING - 16:23:29: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 5.823016651678465 is still above the tolerance 1e-06.
INFO - 16:23:29: 18%|█▊ | 9/50 [00:00<00:01, 27.59 it/sec, feas=False, obj=-1.67]
WARNING - 16:23:29: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 6.882789773680643 is still above the tolerance 1e-06.
INFO - 16:23:29: 20%|██ | 10/50 [00:00<00:01, 28.04 it/sec, feas=False, obj=-1.67]
WARNING - 16:23:29: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 5.839291142662289 is still above the tolerance 1e-06.
INFO - 16:23:29: 22%|██▏ | 11/50 [00:00<00:01, 27.27 it/sec, feas=False, obj=-1.67]
WARNING - 16:23:29: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 11.595172744482486 is still above the tolerance 1e-06.
INFO - 16:23:29: 24%|██▍ | 12/50 [00:00<00:01, 27.66 it/sec, feas=True, obj=-1.65]
WARNING - 16:23:29: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 6.927040570122076 is still above the tolerance 1e-06.
INFO - 16:23:29: 26%|██▌ | 13/50 [00:00<00:01, 28.01 it/sec, feas=False, obj=-1.67]
WARNING - 16:23:29: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 5.855296624823411 is still above the tolerance 1e-06.
INFO - 16:23:29: 28%|██▊ | 14/50 [00:00<00:01, 27.40 it/sec, feas=False, obj=-1.67]
WARNING - 16:23:29: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 6.970618630892496 is still above the tolerance 1e-06.
INFO - 16:23:29: 30%|███ | 15/50 [00:00<00:01, 27.70 it/sec, feas=False, obj=-1.67]
WARNING - 16:23:29: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 5.87116750641698 is still above the tolerance 1e-06.
INFO - 16:23:29: 32%|███▏ | 16/50 [00:00<00:01, 27.20 it/sec, feas=False, obj=-1.67]
WARNING - 16:23:29: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 7.013793617501316 is still above the tolerance 1e-06.
INFO - 16:23:29: 34%|███▍ | 17/50 [00:00<00:01, 27.44 it/sec, feas=False, obj=-1.67]
WARNING - 16:23:29: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 5.886904005855073 is still above the tolerance 1e-06.
INFO - 16:23:29: 36%|███▌ | 18/50 [00:00<00:01, 26.98 it/sec, feas=False, obj=-1.67]
WARNING - 16:23:29: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 11.595038247905833 is still above the tolerance 1e-06.
INFO - 16:23:29: 38%|███▊ | 19/50 [00:00<00:01, 27.22 it/sec, feas=True, obj=-1.65]
WARNING - 16:23:29: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 7.05683391548447 is still above the tolerance 1e-06.
INFO - 16:23:29: 40%|████ | 20/50 [00:00<00:01, 27.43 it/sec, feas=False, obj=-1.67]
WARNING - 16:23:29: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 6.634635869304429 is still above the tolerance 1e-06.
INFO - 16:23:29: 42%|████▏ | 21/50 [00:00<00:01, 27.63 it/sec, feas=False, obj=-1.67]
WARNING - 16:23:29: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 5.888518014951039 is still above the tolerance 1e-06.
INFO - 16:23:29: 44%|████▍ | 22/50 [00:00<00:01, 27.21 it/sec, feas=False, obj=-1.67]
WARNING - 16:23:29: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 11.595172615479878 is still above the tolerance 1e-06.
INFO - 16:23:29: 46%|████▌ | 23/50 [00:00<00:00, 27.41 it/sec, feas=True, obj=-1.65]
WARNING - 16:23:29: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 7.061003378127396 is still above the tolerance 1e-06.
INFO - 16:23:29: 48%|████▊ | 24/50 [00:00<00:00, 27.58 it/sec, feas=False, obj=-1.67]
WARNING - 16:23:29: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 6.6392088296908485 is still above the tolerance 1e-06.
INFO - 16:23:29: 50%|█████ | 25/50 [00:00<00:00, 27.70 it/sec, feas=False, obj=-1.67]
WARNING - 16:23:29: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 5.890266535039761 is still above the tolerance 1e-06.
INFO - 16:23:29: 52%|█████▏ | 26/50 [00:00<00:00, 27.38 it/sec, feas=False, obj=-1.67]
WARNING - 16:23:29: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 7.065307516515108 is still above the tolerance 1e-06.
INFO - 16:23:29: 54%|█████▍ | 27/50 [00:00<00:00, 27.55 it/sec, feas=False, obj=-1.67]
WARNING - 16:23:29: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 6.643916168722729 is still above the tolerance 1e-06.
INFO - 16:23:29: 56%|█████▌ | 28/50 [00:01<00:00, 27.72 it/sec, feas=False, obj=-1.67]
WARNING - 16:23:29: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 5.891746037536034 is still above the tolerance 1e-06.
INFO - 16:23:29: 58%|█████▊ | 29/50 [00:01<00:00, 27.43 it/sec, feas=False, obj=-1.67]
WARNING - 16:23:29: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 7.069476992606872 is still above the tolerance 1e-06.
INFO - 16:23:29: 60%|██████ | 30/50 [00:01<00:00, 27.55 it/sec, feas=False, obj=-1.67]
WARNING - 16:23:29: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 6.648489299844366 is still above the tolerance 1e-06.
INFO - 16:23:29: 62%|██████▏ | 31/50 [00:01<00:00, 27.70 it/sec, feas=False, obj=-1.67]
WARNING - 16:23:29: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 5.893091059561856 is still above the tolerance 1e-06.
INFO - 16:23:29: 64%|██████▍ | 32/50 [00:01<00:00, 27.46 it/sec, feas=False, obj=-1.67]
WARNING - 16:23:29: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 7.07391552208674 is still above the tolerance 1e-06.
INFO - 16:23:29: 66%|██████▌ | 33/50 [00:01<00:00, 27.59 it/sec, feas=False, obj=-1.67]
WARNING - 16:23:29: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 6.653196802888018 is still above the tolerance 1e-06.
INFO - 16:23:29: 68%|██████▊ | 34/50 [00:01<00:00, 27.72 it/sec, feas=False, obj=-1.67]
WARNING - 16:23:29: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 5.894705077404469 is still above the tolerance 1e-06.
INFO - 16:23:29: 70%|███████ | 35/50 [00:01<00:00, 27.49 it/sec, feas=False, obj=-1.67]
WARNING - 16:23:30: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 7.0779504349724816 is still above the tolerance 1e-06.
INFO - 16:23:30: 72%|███████▏ | 36/50 [00:01<00:00, 27.62 it/sec, feas=False, obj=-1.67]
WARNING - 16:23:30: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 6.657500796383389 is still above the tolerance 1e-06.
INFO - 16:23:30: 74%|███████▍ | 37/50 [00:01<00:00, 27.75 it/sec, feas=False, obj=-1.67]
WARNING - 16:23:30: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 6.5371228942698005 is still above the tolerance 1e-06.
INFO - 16:23:30: 76%|███████▌ | 38/50 [00:01<00:00, 27.87 it/sec, feas=False, obj=-1.67]
WARNING - 16:23:30: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 5.894839541007177 is still above the tolerance 1e-06.
INFO - 16:23:30: 78%|███████▊ | 39/50 [00:01<00:00, 27.66 it/sec, feas=False, obj=-1.67]
WARNING - 16:23:30: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 7.0784885946045595 is still above the tolerance 1e-06.
INFO - 16:23:30: 80%|████████ | 40/50 [00:01<00:00, 27.77 it/sec, feas=False, obj=-1.67]
WARNING - 16:23:30: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 6.65844232709479 is still above the tolerance 1e-06.
INFO - 16:23:30: 82%|████████▏ | 41/50 [00:01<00:00, 27.88 it/sec, feas=False, obj=-1.67]
WARNING - 16:23:30: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 6.54868985746545 is still above the tolerance 1e-06.
INFO - 16:23:30: 84%|████████▍ | 42/50 [00:01<00:00, 27.99 it/sec, feas=False, obj=-1.67]
WARNING - 16:23:30: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 5.89497411189 is still above the tolerance 1e-06.
INFO - 16:23:30: 86%|████████▌ | 43/50 [00:01<00:00, 27.80 it/sec, feas=False, obj=-1.67]
WARNING - 16:23:30: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 7.07889191308067 is still above the tolerance 1e-06.
INFO - 16:23:30: 88%|████████▊ | 44/50 [00:01<00:00, 27.90 it/sec, feas=False, obj=-1.67]
WARNING - 16:23:30: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 6.658845817789649 is still above the tolerance 1e-06.
INFO - 16:23:30: 90%|█████████ | 45/50 [00:01<00:00, 27.99 it/sec, feas=False, obj=-1.67]
WARNING - 16:23:30: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 6.556894490852851 is still above the tolerance 1e-06.
INFO - 16:23:30: 92%|█████████▏| 46/50 [00:01<00:00, 28.09 it/sec, feas=False, obj=-1.67]
WARNING - 16:23:30: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 5.895243026000216 is still above the tolerance 1e-06.
INFO - 16:23:30: 94%|█████████▍| 47/50 [00:01<00:00, 27.91 it/sec, feas=False, obj=-1.67]
WARNING - 16:23:30: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 7.079564457044336 is still above the tolerance 1e-06.
INFO - 16:23:30: 96%|█████████▌| 48/50 [00:01<00:00, 28.01 it/sec, feas=False, obj=-1.67]
WARNING - 16:23:30: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 6.6593838712656686 is still above the tolerance 1e-06.
INFO - 16:23:30: 98%|█████████▊| 49/50 [00:01<00:00, 28.10 it/sec, feas=False, obj=-1.67]
WARNING - 16:23:30: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 6.565367829245478 is still above the tolerance 1e-06.
INFO - 16:23:30: 100%|██████████| 50/50 [00:01<00:00, 28.19 it/sec, feas=False, obj=-1.67]
INFO - 16:23:30: Optimization result:
INFO - 16:23:30: Optimizer info:
INFO - 16:23:30: Status: None
INFO - 16:23:30: Message: Maximum number of iterations reached. GEMSEO stopped the driver.
INFO - 16:23:30: Solution:
INFO - 16:23:30: The solution is feasible.
INFO - 16:23:30: Objective: -1.64925383975747
INFO - 16:23:30: Standardized constraints:
INFO - 16:23:30: g_3 = [-7.08111998e-01 -2.91888002e-01 -3.33066907e-16 -1.56011977e-01]
INFO - 16:23:30: Design space:
INFO - 16:23:30: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:30: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:30: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:30: | x_3 | 0.1 | 0.1890996185187401 | 1 | float |
INFO - 16:23:30: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:30: *** End PropulsionScenario execution (time: 0:00:01.776627) ***
WARNING - 16:23:30: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 11.595172615479878 is still above the tolerance 1e-06.
INFO - 16:23:30: *** Start AerodynamicsScenario execution ***
INFO - 16:23:30: AerodynamicsScenario
INFO - 16:23:30: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:30: MDO formulation: MDF
INFO - 16:23:30: Optimization problem:
INFO - 16:23:30: minimize 0.001*-y_4(x_2)
INFO - 16:23:30: with respect to x_2
INFO - 16:23:30: under the inequality constraints
INFO - 16:23:30: g_2(x_2) <= 0
INFO - 16:23:30: over the design space:
INFO - 16:23:30: +------+-------------+-------+-------------+-------+
INFO - 16:23:30: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:30: +------+-------------+-------+-------------+-------+
INFO - 16:23:30: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:30: +------+-------------+-------+-------------+-------+
INFO - 16:23:30: Solving optimization problem with algorithm SLSQP:
WARNING - 16:23:30: Optimization found no feasible point; the least infeasible point is selected.
INFO - 16:23:30: 2%|▏ | 1/50 [00:00<00:00, 70.05 it/sec, feas=False, obj=-1.65]
INFO - 16:23:30: Optimization result:
INFO - 16:23:30: Optimizer info:
INFO - 16:23:30: Status: 8
INFO - 16:23:30: Message: Positive directional derivative for linesearch
INFO - 16:23:30: Solution:
WARNING - 16:23:30: The solution is not feasible.
INFO - 16:23:30: Objective: -1.6492538397567442
INFO - 16:23:30: Standardized constraints:
INFO - 16:23:30: g_2 = 0.0059637061841320005
INFO - 16:23:30: Design space:
INFO - 16:23:30: +------+-------------+-------+-------------+-------+
INFO - 16:23:30: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:30: +------+-------------+-------+-------------+-------+
INFO - 16:23:30: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:30: +------+-------------+-------+-------------+-------+
INFO - 16:23:30: *** End AerodynamicsScenario execution (time: 0:00:00.015895) ***
INFO - 16:23:30: *** Start StructureScenario execution ***
INFO - 16:23:30: StructureScenario
INFO - 16:23:30: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:30: MDO formulation: MDF
INFO - 16:23:30: Optimization problem:
INFO - 16:23:30: minimize 0.001*-y_4(x_1)
INFO - 16:23:30: with respect to x_1
INFO - 16:23:30: under the inequality constraints
INFO - 16:23:30: g_1(x_1) <= 0
INFO - 16:23:30: over the design space:
INFO - 16:23:30: +--------+-------------+-------------------+-------------+-------+
INFO - 16:23:30: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:30: +--------+-------------+-------------------+-------------+-------+
INFO - 16:23:30: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:30: | x_1[1] | 0.75 | 1.083249246018729 | 1.25 | float |
INFO - 16:23:30: +--------+-------------+-------------------+-------------+-------+
INFO - 16:23:30: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:30: 2%|▏ | 1/50 [00:00<00:00, 58.55 it/sec, feas=True, obj=-1.65]
WARNING - 16:23:30: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 0.056778494335281794 is still above the tolerance 1e-06.
INFO - 16:23:30: 4%|▍ | 2/50 [00:00<00:01, 31.43 it/sec, feas=True, obj=-1.71]
INFO - 16:23:30: 6%|▌ | 3/50 [00:00<00:01, 28.04 it/sec, feas=True, obj=-1.87]
INFO - 16:23:30: 8%|▊ | 4/50 [00:00<00:01, 26.68 it/sec, feas=True, obj=-1.89]
INFO - 16:23:30: 10%|█ | 5/50 [00:00<00:01, 25.77 it/sec, feas=True, obj=-1.89]
INFO - 16:23:30: 12%|█▏ | 6/50 [00:00<00:01, 25.30 it/sec, feas=True, obj=-1.89]
INFO - 16:23:30: 14%|█▍ | 7/50 [00:00<00:01, 26.35 it/sec, feas=True, obj=-1.89]
INFO - 16:23:30: 16%|█▌ | 8/50 [00:00<00:01, 27.36 it/sec, feas=True, obj=-1.89]
INFO - 16:23:30: Optimization result:
INFO - 16:23:30: Optimizer info:
INFO - 16:23:30: Status: None
INFO - 16:23:30: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:30: Solution:
INFO - 16:23:30: The solution is feasible.
INFO - 16:23:30: Objective: -1.8911282795169813
INFO - 16:23:30: Standardized constraints:
INFO - 16:23:30: g_1 = [-5.04995730e-02 -2.87334114e-02 -3.09501946e-02 -3.64722210e-02
INFO - 16:23:30: -4.19002205e-02 -2.40000000e-01 3.55718233e-10]
INFO - 16:23:30: Design space:
INFO - 16:23:30: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:30: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:30: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:30: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:30: | x_1[1] | 0.75 | 0.7806436825458758 | 1.25 | float |
INFO - 16:23:30: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:30: *** End StructureScenario execution (time: 0:00:00.294990) ***
INFO - 16:23:30: *** Start PropulsionScenario execution ***
INFO - 16:23:30: PropulsionScenario
INFO - 16:23:30: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:30: MDO formulation: MDF
INFO - 16:23:30: Optimization problem:
INFO - 16:23:30: minimize 0.001*-y_4(x_3)
INFO - 16:23:30: with respect to x_3
INFO - 16:23:30: under the inequality constraints
INFO - 16:23:30: g_3(x_3) <= 0
INFO - 16:23:30: over the design space:
INFO - 16:23:30: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:30: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:30: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:30: | x_3 | 0.1 | 0.1890996185187401 | 1 | float |
INFO - 16:23:30: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:30: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:30: 2%|▏ | 1/50 [00:00<00:00, 87.24 it/sec, feas=True, obj=-1.89]
INFO - 16:23:30: 4%|▍ | 2/50 [00:00<00:00, 62.24 it/sec, feas=True, obj=-1.89]
INFO - 16:23:30: Optimization result:
INFO - 16:23:30: Optimizer info:
INFO - 16:23:30: Status: 8
INFO - 16:23:30: Message: Positive directional derivative for linesearch
INFO - 16:23:30: Solution:
INFO - 16:23:30: The solution is feasible.
INFO - 16:23:30: Objective: -1.8911282795169826
INFO - 16:23:30: Standardized constraints:
INFO - 16:23:30: g_3 = [-7.13679402e-01 -2.86320598e-01 1.55431223e-15 -1.56011977e-01]
INFO - 16:23:30: Design space:
INFO - 16:23:30: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:30: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:30: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:30: | x_3 | 0.1 | 0.1890996185187405 | 1 | float |
INFO - 16:23:30: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:30: *** End PropulsionScenario execution (time: 0:00:00.034248) ***
INFO - 16:23:30: *** Start AerodynamicsScenario execution ***
INFO - 16:23:30: AerodynamicsScenario
INFO - 16:23:30: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:30: MDO formulation: MDF
INFO - 16:23:30: Optimization problem:
INFO - 16:23:30: minimize 0.001*-y_4(x_2)
INFO - 16:23:30: with respect to x_2
INFO - 16:23:30: under the inequality constraints
INFO - 16:23:30: g_2(x_2) <= 0
INFO - 16:23:30: over the design space:
INFO - 16:23:30: +------+-------------+-------+-------------+-------+
INFO - 16:23:30: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:30: +------+-------------+-------+-------------+-------+
INFO - 16:23:30: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:30: +------+-------------+-------+-------------+-------+
INFO - 16:23:30: Solving optimization problem with algorithm SLSQP:
WARNING - 16:23:30: Optimization found no feasible point; the least infeasible point is selected.
INFO - 16:23:30: 2%|▏ | 1/50 [00:00<00:00, 103.72 it/sec, feas=False, obj=-1.89]
INFO - 16:23:30: Optimization result:
INFO - 16:23:30: Optimizer info:
INFO - 16:23:30: Status: 8
INFO - 16:23:30: Message: Positive directional derivative for linesearch
INFO - 16:23:30: Solution:
WARNING - 16:23:30: The solution is not feasible.
INFO - 16:23:30: Objective: -1.8911282795169826
INFO - 16:23:30: Standardized constraints:
INFO - 16:23:30: g_2 = 0.0059637061841320005
INFO - 16:23:30: Design space:
INFO - 16:23:30: +------+-------------+-------+-------------+-------+
INFO - 16:23:30: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:30: +------+-------------+-------+-------------+-------+
INFO - 16:23:30: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:30: +------+-------------+-------+-------------+-------+
INFO - 16:23:30: *** End AerodynamicsScenario execution (time: 0:00:00.011404) ***
INFO - 16:23:30: *** Start StructureScenario execution ***
INFO - 16:23:30: StructureScenario
INFO - 16:23:30: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:30: MDO formulation: MDF
INFO - 16:23:30: Optimization problem:
INFO - 16:23:30: minimize 0.001*-y_4(x_1)
INFO - 16:23:30: with respect to x_1
INFO - 16:23:30: under the inequality constraints
INFO - 16:23:30: g_1(x_1) <= 0
INFO - 16:23:30: over the design space:
INFO - 16:23:30: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:30: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:30: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:30: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:30: | x_1[1] | 0.75 | 0.7806436825458758 | 1.25 | float |
INFO - 16:23:30: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:30: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:30: 2%|▏ | 1/50 [00:00<00:00, 99.60 it/sec, feas=True, obj=-1.89]
INFO - 16:23:30: 4%|▍ | 2/50 [00:00<00:00, 91.85 it/sec, feas=True, obj=-1.89]
INFO - 16:23:30: 6%|▌ | 3/50 [00:00<00:00, 93.10 it/sec, feas=True, obj=-1.89]
INFO - 16:23:30: Optimization result:
INFO - 16:23:30: Optimizer info:
INFO - 16:23:30: Status: None
INFO - 16:23:30: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:30: Solution:
INFO - 16:23:30: The solution is feasible.
INFO - 16:23:30: Objective: -1.8911282795169826
INFO - 16:23:30: Standardized constraints:
INFO - 16:23:30: g_1 = [-5.04995730e-02 -2.87334114e-02 -3.09501946e-02 -3.64722210e-02
INFO - 16:23:30: -4.19002205e-02 -2.40000000e-01 3.55718233e-10]
INFO - 16:23:30: Design space:
INFO - 16:23:30: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:30: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:30: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:30: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:30: | x_1[1] | 0.75 | 0.7806436825458758 | 1.25 | float |
INFO - 16:23:30: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:30: *** End StructureScenario execution (time: 0:00:00.034775) ***
INFO - 16:23:30: 13%|█▎ | 13/100 [00:14<01:33, 55.56 it/min, feas=False, obj=-1.89]
INFO - 16:23:30: *** Start PropulsionScenario execution ***
INFO - 16:23:30: PropulsionScenario
INFO - 16:23:30: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:30: MDO formulation: MDF
INFO - 16:23:30: Optimization problem:
INFO - 16:23:30: minimize 0.001*-y_4(x_3)
INFO - 16:23:30: with respect to x_3
INFO - 16:23:30: under the inequality constraints
INFO - 16:23:30: g_3(x_3) <= 0
INFO - 16:23:30: over the design space:
INFO - 16:23:30: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:30: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:30: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:30: | x_3 | 0.1 | 0.1890996185187405 | 1 | float |
INFO - 16:23:30: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:30: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:30: 2%|▏ | 1/50 [00:00<00:01, 37.25 it/sec, feas=True, obj=-1.59]
INFO - 16:23:31: 4%|▍ | 2/50 [00:00<00:01, 28.59 it/sec, feas=True, obj=-1.6]
INFO - 16:23:31: 6%|▌ | 3/50 [00:00<00:01, 30.84 it/sec, feas=True, obj=-1.6]
INFO - 16:23:31: 8%|▊ | 4/50 [00:00<00:01, 31.96 it/sec, feas=True, obj=-1.6]
INFO - 16:23:31: Optimization result:
INFO - 16:23:31: Optimizer info:
INFO - 16:23:31: Status: None
INFO - 16:23:31: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:31: Solution:
INFO - 16:23:31: The solution is feasible.
INFO - 16:23:31: Objective: -1.5980464379926134
INFO - 16:23:31: Standardized constraints:
INFO - 16:23:31: g_3 = [-7.90764832e-01 -2.09235168e-01 2.22044605e-15 -1.67966643e-01]
INFO - 16:23:31: Design space:
INFO - 16:23:31: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:31: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:31: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:31: | x_3 | 0.1 | 0.1945020315992327 | 1 | float |
INFO - 16:23:31: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:31: *** End PropulsionScenario execution (time: 0:00:00.127620) ***
INFO - 16:23:31: *** Start AerodynamicsScenario execution ***
INFO - 16:23:31: AerodynamicsScenario
INFO - 16:23:31: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:31: MDO formulation: MDF
INFO - 16:23:31: Optimization problem:
INFO - 16:23:31: minimize 0.001*-y_4(x_2)
INFO - 16:23:31: with respect to x_2
INFO - 16:23:31: under the inequality constraints
INFO - 16:23:31: g_2(x_2) <= 0
INFO - 16:23:31: over the design space:
INFO - 16:23:31: +------+-------------+-------+-------------+-------+
INFO - 16:23:31: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:31: +------+-------------+-------+-------------+-------+
INFO - 16:23:31: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:31: +------+-------------+-------+-------------+-------+
INFO - 16:23:31: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:31: 2%|▏ | 1/50 [00:00<00:00, 84.18 it/sec, feas=True, obj=-1.6]
INFO - 16:23:31: Optimization result:
INFO - 16:23:31: Optimizer info:
INFO - 16:23:31: Status: 8
INFO - 16:23:31: Message: Positive directional derivative for linesearch
INFO - 16:23:31: Solution:
INFO - 16:23:31: The solution is feasible.
INFO - 16:23:31: Objective: -1.5980464379926134
INFO - 16:23:31: Standardized constraints:
INFO - 16:23:31: g_2 = -0.029336068423954087
INFO - 16:23:31: Design space:
INFO - 16:23:31: +------+-------------+-------+-------------+-------+
INFO - 16:23:31: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:31: +------+-------------+-------+-------------+-------+
INFO - 16:23:31: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:31: +------+-------------+-------+-------------+-------+
INFO - 16:23:31: *** End AerodynamicsScenario execution (time: 0:00:00.013621) ***
INFO - 16:23:31: *** Start StructureScenario execution ***
INFO - 16:23:31: StructureScenario
INFO - 16:23:31: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:31: MDO formulation: MDF
INFO - 16:23:31: Optimization problem:
INFO - 16:23:31: minimize 0.001*-y_4(x_1)
INFO - 16:23:31: with respect to x_1
INFO - 16:23:31: under the inequality constraints
INFO - 16:23:31: g_1(x_1) <= 0
INFO - 16:23:31: over the design space:
INFO - 16:23:31: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:31: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:31: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:31: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:31: | x_1[1] | 0.75 | 0.7806436825458758 | 1.25 | float |
INFO - 16:23:31: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:31: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:31: 2%|▏ | 1/50 [00:00<00:00, 97.48 it/sec, feas=False, obj=-1.6]
WARNING - 16:23:31: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 83742.11219639464 is still above the tolerance 1e-06.
INFO - 16:23:31: 4%|▍ | 2/50 [00:00<00:01, 34.12 it/sec, feas=True, obj=-1.38]
WARNING - 16:23:31: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 163.1649046157224 is still above the tolerance 1e-06.
INFO - 16:23:31: 6%|▌ | 3/50 [00:00<00:01, 28.33 it/sec, feas=True, obj=-1.42]
WARNING - 16:23:31: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 48.98353495697865 is still above the tolerance 1e-06.
INFO - 16:23:31: 8%|▊ | 4/50 [00:00<00:01, 26.12 it/sec, feas=True, obj=-1.43]
WARNING - 16:23:31: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 47.921263920006105 is still above the tolerance 1e-06.
INFO - 16:23:31: 10%|█ | 5/50 [00:00<00:01, 24.99 it/sec, feas=True, obj=-1.43]
WARNING - 16:23:31: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 47.91943318636026 is still above the tolerance 1e-06.
INFO - 16:23:31: 12%|█▏ | 6/50 [00:00<00:01, 24.26 it/sec, feas=True, obj=-1.43]
WARNING - 16:23:31: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 47.92126423260303 is still above the tolerance 1e-06.
INFO - 16:23:31: 14%|█▍ | 7/50 [00:00<00:01, 23.78 it/sec, feas=True, obj=-1.43]
WARNING - 16:23:31: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 47.91943274420979 is still above the tolerance 1e-06.
INFO - 16:23:31: 16%|█▌ | 8/50 [00:00<00:01, 23.28 it/sec, feas=True, obj=-1.43]
INFO - 16:23:31: Optimization result:
INFO - 16:23:31: Optimizer info:
INFO - 16:23:31: Status: 8
INFO - 16:23:31: Message: Positive directional derivative for linesearch
INFO - 16:23:31: Solution:
INFO - 16:23:31: The solution is feasible.
INFO - 16:23:31: Objective: -1.4307726327026875
INFO - 16:23:31: Standardized constraints:
INFO - 16:23:31: g_1 = [ 2.17603713e-14 -1.76574100e-02 -3.11145863e-02 -4.06700028e-02
INFO - 16:23:31: -4.76574100e-02 -1.51034915e-01 -8.89650853e-02]
INFO - 16:23:31: Design space:
INFO - 16:23:31: +--------+-------------+-------------------+-------------+-------+
INFO - 16:23:31: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:31: +--------+-------------+-------------------+-------------+-------+
INFO - 16:23:31: | x_1[0] | 0.1 | 0.100000000000001 | 0.4 | float |
INFO - 16:23:31: | x_1[1] | 0.75 | 1.025352074928868 | 1.25 | float |
INFO - 16:23:31: +--------+-------------+-------------------+-------------+-------+
INFO - 16:23:31: *** End StructureScenario execution (time: 0:00:00.345944) ***
INFO - 16:23:31: *** Start PropulsionScenario execution ***
INFO - 16:23:31: PropulsionScenario
INFO - 16:23:31: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:31: MDO formulation: MDF
INFO - 16:23:31: Optimization problem:
INFO - 16:23:31: minimize 0.001*-y_4(x_3)
INFO - 16:23:31: with respect to x_3
INFO - 16:23:31: under the inequality constraints
INFO - 16:23:31: g_3(x_3) <= 0
INFO - 16:23:31: over the design space:
INFO - 16:23:31: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:31: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:31: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:31: | x_3 | 0.1 | 0.1945020315992327 | 1 | float |
INFO - 16:23:31: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:31: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:31: 2%|▏ | 1/50 [00:00<00:00, 52.54 it/sec, feas=True, obj=-1.43]
INFO - 16:23:31: 4%|▍ | 2/50 [00:00<00:00, 68.00 it/sec, feas=True, obj=-1.43]
INFO - 16:23:31: 6%|▌ | 3/50 [00:00<00:00, 70.58 it/sec, feas=True, obj=-1.43]
INFO - 16:23:31: Optimization result:
INFO - 16:23:31: Optimizer info:
INFO - 16:23:31: Status: 8
INFO - 16:23:31: Message: Positive directional derivative for linesearch
INFO - 16:23:31: Solution:
INFO - 16:23:31: The solution is feasible.
INFO - 16:23:31: Objective: -1.4307726327025028
INFO - 16:23:31: Standardized constraints:
INFO - 16:23:31: g_3 = [-7.88210951e-01 -2.11789049e-01 2.22044605e-15 -1.67966643e-01]
INFO - 16:23:31: Design space:
INFO - 16:23:31: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:31: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:31: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:31: | x_3 | 0.1 | 0.1945020315992327 | 1 | float |
INFO - 16:23:31: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:31: *** End PropulsionScenario execution (time: 0:00:00.044670) ***
INFO - 16:23:31: *** Start AerodynamicsScenario execution ***
INFO - 16:23:31: AerodynamicsScenario
INFO - 16:23:31: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:31: MDO formulation: MDF
INFO - 16:23:31: Optimization problem:
INFO - 16:23:31: minimize 0.001*-y_4(x_2)
INFO - 16:23:31: with respect to x_2
INFO - 16:23:31: under the inequality constraints
INFO - 16:23:31: g_2(x_2) <= 0
INFO - 16:23:31: over the design space:
INFO - 16:23:31: +------+-------------+-------+-------------+-------+
INFO - 16:23:31: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:31: +------+-------------+-------+-------------+-------+
INFO - 16:23:31: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:31: +------+-------------+-------+-------------+-------+
INFO - 16:23:31: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:31: 2%|▏ | 1/50 [00:00<00:00, 84.08 it/sec, feas=True, obj=-1.43]
INFO - 16:23:31: Optimization result:
INFO - 16:23:31: Optimizer info:
INFO - 16:23:31: Status: 8
INFO - 16:23:31: Message: Positive directional derivative for linesearch
INFO - 16:23:31: Solution:
INFO - 16:23:31: The solution is feasible.
INFO - 16:23:31: Objective: -1.4307726327025028
INFO - 16:23:31: Standardized constraints:
INFO - 16:23:31: g_2 = -0.029336068423954087
INFO - 16:23:31: Design space:
INFO - 16:23:31: +------+-------------+-------+-------------+-------+
INFO - 16:23:31: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:31: +------+-------------+-------+-------------+-------+
INFO - 16:23:31: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:31: +------+-------------+-------+-------------+-------+
INFO - 16:23:31: *** End AerodynamicsScenario execution (time: 0:00:00.013631) ***
INFO - 16:23:31: *** Start StructureScenario execution ***
INFO - 16:23:31: StructureScenario
INFO - 16:23:31: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:31: MDO formulation: MDF
INFO - 16:23:31: Optimization problem:
INFO - 16:23:31: minimize 0.001*-y_4(x_1)
INFO - 16:23:31: with respect to x_1
INFO - 16:23:31: under the inequality constraints
INFO - 16:23:31: g_1(x_1) <= 0
INFO - 16:23:31: over the design space:
INFO - 16:23:31: +--------+-------------+-------------------+-------------+-------+
INFO - 16:23:31: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:31: +--------+-------------+-------------------+-------------+-------+
INFO - 16:23:31: | x_1[0] | 0.1 | 0.100000000000001 | 0.4 | float |
INFO - 16:23:31: | x_1[1] | 0.75 | 1.025352074928868 | 1.25 | float |
INFO - 16:23:31: +--------+-------------+-------------------+-------------+-------+
INFO - 16:23:31: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:31: 2%|▏ | 1/50 [00:00<00:00, 96.56 it/sec, feas=True, obj=-1.43]
INFO - 16:23:31: 4%|▍ | 2/50 [00:00<00:00, 107.55 it/sec, feas=True, obj=-1.43]
INFO - 16:23:31: 6%|▌ | 3/50 [00:00<00:00, 71.54 it/sec, feas=True, obj=-1.43]
INFO - 16:23:31: Optimization result:
INFO - 16:23:31: Optimizer info:
INFO - 16:23:31: Status: None
INFO - 16:23:31: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:31: Solution:
INFO - 16:23:31: The solution is feasible.
INFO - 16:23:31: Objective: -1.4307726327025028
INFO - 16:23:31: Standardized constraints:
INFO - 16:23:31: g_1 = [ 2.17603713e-14 -1.76574100e-02 -3.11145863e-02 -4.06700028e-02
INFO - 16:23:31: -4.76574100e-02 -1.51034915e-01 -8.89650853e-02]
INFO - 16:23:31: Design space:
INFO - 16:23:31: +--------+-------------+-------------------+-------------+-------+
INFO - 16:23:31: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:31: +--------+-------------+-------------------+-------------+-------+
INFO - 16:23:31: | x_1[0] | 0.1 | 0.100000000000001 | 0.4 | float |
INFO - 16:23:31: | x_1[1] | 0.75 | 1.025352074928868 | 1.25 | float |
INFO - 16:23:31: +--------+-------------+-------------------+-------------+-------+
INFO - 16:23:31: *** End StructureScenario execution (time: 0:00:00.044579) ***
INFO - 16:23:31: 14%|█▍ | 14/100 [00:14<01:30, 57.27 it/min, feas=True, obj=-1.43]
INFO - 16:23:31: *** Start PropulsionScenario execution ***
INFO - 16:23:31: PropulsionScenario
INFO - 16:23:31: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:31: MDO formulation: MDF
INFO - 16:23:31: Optimization problem:
INFO - 16:23:31: minimize 0.001*-y_4(x_3)
INFO - 16:23:31: with respect to x_3
INFO - 16:23:31: under the inequality constraints
INFO - 16:23:31: g_3(x_3) <= 0
INFO - 16:23:31: over the design space:
INFO - 16:23:31: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:31: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:31: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:31: | x_3 | 0.1 | 0.1945020315992327 | 1 | float |
INFO - 16:23:31: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:31: Solving optimization problem with algorithm SLSQP:
WARNING - 16:23:31: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 0.5244185412098862 is still above the tolerance 1e-06.
INFO - 16:23:31: 2%|▏ | 1/50 [00:00<00:01, 32.77 it/sec, feas=False, obj=-1.64]
WARNING - 16:23:31: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 0.6961770766641683 is still above the tolerance 1e-06.
INFO - 16:23:31: 4%|▍ | 2/50 [00:00<00:01, 31.41 it/sec, feas=True, obj=-1.63]
WARNING - 16:23:31: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 0.5412312228649894 is still above the tolerance 1e-06.
INFO - 16:23:31: 6%|▌ | 3/50 [00:00<00:01, 26.83 it/sec, feas=False, obj=-1.64]
WARNING - 16:23:31: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 0.6963115729825144 is still above the tolerance 1e-06.
INFO - 16:23:31: 8%|▊ | 4/50 [00:00<00:01, 25.03 it/sec, feas=True, obj=-1.63]
WARNING - 16:23:31: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 0.6963115729825148 is still above the tolerance 1e-06.
INFO - 16:23:31: 10%|█ | 5/50 [00:00<00:01, 26.07 it/sec, feas=True, obj=-1.63]
WARNING - 16:23:31: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 0.6964460693017623 is still above the tolerance 1e-06.
INFO - 16:23:31: 12%|█▏ | 6/50 [00:00<00:01, 26.65 it/sec, feas=True, obj=-1.63]
INFO - 16:23:31: Optimization result:
INFO - 16:23:31: Optimizer info:
INFO - 16:23:31: Status: None
INFO - 16:23:31: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:31: Solution:
INFO - 16:23:31: The solution is feasible.
INFO - 16:23:31: Objective: -1.6322370774103923
INFO - 16:23:31: Standardized constraints:
INFO - 16:23:31: g_3 = [-7.22331895e-01 -2.77668105e-01 1.04360964e-14 -1.55194346e-01]
INFO - 16:23:31: Design space:
INFO - 16:23:31: +------+-------------+-------------------+-------------+-------+
INFO - 16:23:31: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:31: +------+-------------+-------------------+-------------+-------+
INFO - 16:23:31: | x_3 | 0.1 | 0.190188145273491 | 1 | float |
INFO - 16:23:31: +------+-------------+-------------------+-------------+-------+
INFO - 16:23:31: *** End PropulsionScenario execution (time: 0:00:00.227938) ***
INFO - 16:23:31: *** Start AerodynamicsScenario execution ***
INFO - 16:23:31: AerodynamicsScenario
INFO - 16:23:31: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:31: MDO formulation: MDF
INFO - 16:23:31: Optimization problem:
INFO - 16:23:31: minimize 0.001*-y_4(x_2)
INFO - 16:23:31: with respect to x_2
INFO - 16:23:31: under the inequality constraints
INFO - 16:23:31: g_2(x_2) <= 0
INFO - 16:23:31: over the design space:
INFO - 16:23:31: +------+-------------+-------+-------------+-------+
INFO - 16:23:31: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:31: +------+-------------+-------+-------------+-------+
INFO - 16:23:31: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:31: +------+-------------+-------+-------------+-------+
INFO - 16:23:31: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:31: 2%|▏ | 1/50 [00:00<00:00, 65.00 it/sec, feas=True, obj=-1.63]
INFO - 16:23:31: Optimization result:
INFO - 16:23:31: Optimizer info:
INFO - 16:23:31: Status: 8
INFO - 16:23:31: Message: Positive directional derivative for linesearch
INFO - 16:23:31: Solution:
INFO - 16:23:31: The solution is feasible.
INFO - 16:23:31: Objective: -1.6322370774103463
INFO - 16:23:31: Standardized constraints:
INFO - 16:23:31: g_2 = -0.005118161063181859
INFO - 16:23:31: Design space:
INFO - 16:23:31: +------+-------------+-------+-------------+-------+
INFO - 16:23:31: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:31: +------+-------------+-------+-------------+-------+
INFO - 16:23:31: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:31: +------+-------------+-------+-------------+-------+
INFO - 16:23:31: *** End AerodynamicsScenario execution (time: 0:00:00.017325) ***
INFO - 16:23:31: *** Start StructureScenario execution ***
INFO - 16:23:31: StructureScenario
INFO - 16:23:31: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:31: MDO formulation: MDF
INFO - 16:23:31: Optimization problem:
INFO - 16:23:31: minimize 0.001*-y_4(x_1)
INFO - 16:23:31: with respect to x_1
INFO - 16:23:31: under the inequality constraints
INFO - 16:23:31: g_1(x_1) <= 0
INFO - 16:23:31: over the design space:
INFO - 16:23:31: +--------+-------------+-------------------+-------------+-------+
INFO - 16:23:31: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:31: +--------+-------------+-------------------+-------------+-------+
INFO - 16:23:31: | x_1[0] | 0.1 | 0.100000000000001 | 0.4 | float |
INFO - 16:23:31: | x_1[1] | 0.75 | 1.025352074928868 | 1.25 | float |
INFO - 16:23:31: +--------+-------------+-------------------+-------------+-------+
INFO - 16:23:31: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:31: 2%|▏ | 1/50 [00:00<00:00, 65.19 it/sec, feas=True, obj=-1.63]
INFO - 16:23:31: 4%|▍ | 2/50 [00:00<00:01, 33.15 it/sec, feas=True, obj=-1.72]
INFO - 16:23:31: 6%|▌ | 3/50 [00:00<00:01, 29.04 it/sec, feas=True, obj=-1.78]
INFO - 16:23:31: 8%|▊ | 4/50 [00:00<00:01, 27.32 it/sec, feas=True, obj=-1.78]
INFO - 16:23:32: 10%|█ | 5/50 [00:00<00:01, 26.38 it/sec, feas=True, obj=-1.78]
WARNING - 16:23:32: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 0.0009157477359807847 is still above the tolerance 1e-06.
INFO - 16:23:32: 12%|█▏ | 6/50 [00:00<00:01, 25.24 it/sec, feas=True, obj=-1.78]
INFO - 16:23:32: Optimization result:
INFO - 16:23:32: Optimizer info:
INFO - 16:23:32: Status: 8
INFO - 16:23:32: Message: Positive directional derivative for linesearch
INFO - 16:23:32: Solution:
INFO - 16:23:32: The solution is feasible.
INFO - 16:23:32: Objective: -1.7839847444068309
INFO - 16:23:32: Standardized constraints:
INFO - 16:23:32: g_1 = [ 3.13815640e-12 -4.69095511e-03 -1.65273245e-02 -2.66662315e-02
INFO - 16:23:32: -3.46909551e-02 -2.25164458e-01 -1.48355421e-02]
INFO - 16:23:32: Design space:
INFO - 16:23:32: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:32: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:32: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:32: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:32: | x_1[1] | 0.75 | 0.8264638086844417 | 1.25 | float |
INFO - 16:23:32: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:32: *** End StructureScenario execution (time: 0:00:00.240180) ***
INFO - 16:23:32: *** Start PropulsionScenario execution ***
INFO - 16:23:32: PropulsionScenario
INFO - 16:23:32: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:32: MDO formulation: MDF
INFO - 16:23:32: Optimization problem:
INFO - 16:23:32: minimize 0.001*-y_4(x_3)
INFO - 16:23:32: with respect to x_3
INFO - 16:23:32: under the inequality constraints
INFO - 16:23:32: g_3(x_3) <= 0
INFO - 16:23:32: over the design space:
INFO - 16:23:32: +------+-------------+-------------------+-------------+-------+
INFO - 16:23:32: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:32: +------+-------------+-------------------+-------------+-------+
INFO - 16:23:32: | x_3 | 0.1 | 0.190188145273491 | 1 | float |
INFO - 16:23:32: +------+-------------+-------------------+-------------+-------+
INFO - 16:23:32: Solving optimization problem with algorithm SLSQP:
WARNING - 16:23:32: MDAGaussSeidel has reached its maximum number of unsuccessful iterations, but the normalized residual norm 6.724932466608626e-05 is still above the tolerance 1e-06.
INFO - 16:23:32: 2%|▏ | 1/50 [00:00<00:01, 45.23 it/sec, feas=True, obj=-1.78]
INFO - 16:23:32: Optimization result:
INFO - 16:23:32: Optimizer info:
INFO - 16:23:32: Status: 8
INFO - 16:23:32: Message: Positive directional derivative for linesearch
INFO - 16:23:32: Solution:
INFO - 16:23:32: The solution is feasible.
INFO - 16:23:32: Objective: -1.7839847444068309
INFO - 16:23:32: Standardized constraints:
INFO - 16:23:32: g_3 = [-7.25606009e-01 -2.74393991e-01 1.04360964e-14 -1.55194346e-01]
INFO - 16:23:32: Design space:
INFO - 16:23:32: +------+-------------+-------------------+-------------+-------+
INFO - 16:23:32: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:32: +------+-------------+-------------------+-------------+-------+
INFO - 16:23:32: | x_3 | 0.1 | 0.190188145273491 | 1 | float |
INFO - 16:23:32: +------+-------------+-------------------+-------------+-------+
INFO - 16:23:32: *** End PropulsionScenario execution (time: 0:00:00.024271) ***
INFO - 16:23:32: *** Start AerodynamicsScenario execution ***
INFO - 16:23:32: AerodynamicsScenario
INFO - 16:23:32: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:32: MDO formulation: MDF
INFO - 16:23:32: Optimization problem:
INFO - 16:23:32: minimize 0.001*-y_4(x_2)
INFO - 16:23:32: with respect to x_2
INFO - 16:23:32: under the inequality constraints
INFO - 16:23:32: g_2(x_2) <= 0
INFO - 16:23:32: over the design space:
INFO - 16:23:32: +------+-------------+-------+-------------+-------+
INFO - 16:23:32: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:32: +------+-------------+-------+-------------+-------+
INFO - 16:23:32: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:32: +------+-------------+-------+-------------+-------+
INFO - 16:23:32: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:32: 2%|▏ | 1/50 [00:00<00:00, 81.71 it/sec, feas=True, obj=-1.78]
INFO - 16:23:32: Optimization result:
INFO - 16:23:32: Optimizer info:
INFO - 16:23:32: Status: 8
INFO - 16:23:32: Message: Positive directional derivative for linesearch
INFO - 16:23:32: Solution:
INFO - 16:23:32: The solution is feasible.
INFO - 16:23:32: Objective: -1.7839847444068309
INFO - 16:23:32: Standardized constraints:
INFO - 16:23:32: g_2 = -0.005118161063181859
INFO - 16:23:32: Design space:
INFO - 16:23:32: +------+-------------+-------+-------------+-------+
INFO - 16:23:32: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:32: +------+-------------+-------+-------------+-------+
INFO - 16:23:32: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:32: +------+-------------+-------+-------------+-------+
INFO - 16:23:32: *** End AerodynamicsScenario execution (time: 0:00:00.013921) ***
INFO - 16:23:32: *** Start StructureScenario execution ***
INFO - 16:23:32: StructureScenario
INFO - 16:23:32: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:32: MDO formulation: MDF
INFO - 16:23:32: Optimization problem:
INFO - 16:23:32: minimize 0.001*-y_4(x_1)
INFO - 16:23:32: with respect to x_1
INFO - 16:23:32: under the inequality constraints
INFO - 16:23:32: g_1(x_1) <= 0
INFO - 16:23:32: over the design space:
INFO - 16:23:32: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:32: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:32: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:32: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:32: | x_1[1] | 0.75 | 0.8264638086844417 | 1.25 | float |
INFO - 16:23:32: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:32: Solving optimization problem with algorithm SLSQP:
WARNING - 16:23:32: MDAGaussSeidel has reached its maximum number of unsuccessful iterations, but the normalized residual norm 0.0009157477359807847 is still above the tolerance 1e-06.
INFO - 16:23:32: 2%|▏ | 1/50 [00:00<00:00, 51.66 it/sec, feas=True, obj=-1.78]
INFO - 16:23:32: Optimization result:
INFO - 16:23:32: Optimizer info:
INFO - 16:23:32: Status: 8
INFO - 16:23:32: Message: Positive directional derivative for linesearch
INFO - 16:23:32: Solution:
INFO - 16:23:32: The solution is feasible.
INFO - 16:23:32: Objective: -1.7839847444068313
INFO - 16:23:32: Standardized constraints:
INFO - 16:23:32: g_1 = [ 3.13815640e-12 -4.69095511e-03 -1.65273245e-02 -2.66662315e-02
INFO - 16:23:32: -3.46909551e-02 -2.25164458e-01 -1.48355421e-02]
INFO - 16:23:32: Design space:
INFO - 16:23:32: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:32: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:32: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:32: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:32: | x_1[1] | 0.75 | 0.8264638086844417 | 1.25 | float |
INFO - 16:23:32: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:32: *** End StructureScenario execution (time: 0:00:00.021484) ***
INFO - 16:23:32: 15%|█▌ | 15/100 [00:15<01:26, 59.00 it/min, feas=True, obj=-1.78]
INFO - 16:23:32: *** Start PropulsionScenario execution ***
INFO - 16:23:32: PropulsionScenario
INFO - 16:23:32: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:32: MDO formulation: MDF
INFO - 16:23:32: Optimization problem:
INFO - 16:23:32: minimize 0.001*-y_4(x_3)
INFO - 16:23:32: with respect to x_3
INFO - 16:23:32: under the inequality constraints
INFO - 16:23:32: g_3(x_3) <= 0
INFO - 16:23:32: over the design space:
INFO - 16:23:32: +------+-------------+-------------------+-------------+-------+
INFO - 16:23:32: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:32: +------+-------------+-------------------+-------------+-------+
INFO - 16:23:32: | x_3 | 0.1 | 0.190188145273491 | 1 | float |
INFO - 16:23:32: +------+-------------+-------------------+-------------+-------+
INFO - 16:23:32: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:32: 2%|▏ | 1/50 [00:00<00:01, 44.36 it/sec, feas=False, obj=-2.02]
INFO - 16:23:32: 4%|▍ | 2/50 [00:00<00:01, 46.23 it/sec, feas=True, obj=-2]
INFO - 16:23:32: 6%|▌ | 3/50 [00:00<00:01, 38.35 it/sec, feas=False, obj=-2.02]
INFO - 16:23:32: 8%|▊ | 4/50 [00:00<00:01, 33.68 it/sec, feas=True, obj=-2]
INFO - 16:23:32: 10%|█ | 5/50 [00:00<00:01, 32.09 it/sec, feas=True, obj=-2]
INFO - 16:23:32: 12%|█▏ | 6/50 [00:00<00:01, 34.04 it/sec, feas=True, obj=-2]
INFO - 16:23:32: Optimization result:
INFO - 16:23:32: Optimizer info:
INFO - 16:23:32: Status: None
INFO - 16:23:32: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:32: Solution:
INFO - 16:23:32: The solution is feasible.
INFO - 16:23:32: Objective: -1.9978124577039875
INFO - 16:23:32: Standardized constraints:
INFO - 16:23:32: g_3 = [-7.59779301e-01 -2.40220699e-01 2.88657986e-15 -1.65669802e-01]
INFO - 16:23:32: Design space:
INFO - 16:23:32: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:32: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:32: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:32: | x_3 | 0.1 | 0.1766383461160826 | 1 | float |
INFO - 16:23:32: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:32: *** End PropulsionScenario execution (time: 0:00:00.179088) ***
INFO - 16:23:32: *** Start AerodynamicsScenario execution ***
INFO - 16:23:32: AerodynamicsScenario
INFO - 16:23:32: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:32: MDO formulation: MDF
INFO - 16:23:32: Optimization problem:
INFO - 16:23:32: minimize 0.001*-y_4(x_2)
INFO - 16:23:32: with respect to x_2
INFO - 16:23:32: under the inequality constraints
INFO - 16:23:32: g_2(x_2) <= 0
INFO - 16:23:32: over the design space:
INFO - 16:23:32: +------+-------------+-------+-------------+-------+
INFO - 16:23:32: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:32: +------+-------------+-------+-------------+-------+
INFO - 16:23:32: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:32: +------+-------------+-------+-------------+-------+
INFO - 16:23:32: Solving optimization problem with algorithm SLSQP:
WARNING - 16:23:32: Optimization found no feasible point; the least infeasible point is selected.
INFO - 16:23:32: 2%|▏ | 1/50 [00:00<00:00, 64.33 it/sec, feas=False, obj=-2]
INFO - 16:23:32: Optimization result:
INFO - 16:23:32: Optimizer info:
INFO - 16:23:32: Status: 8
INFO - 16:23:32: Message: Positive directional derivative for linesearch
INFO - 16:23:32: Solution:
WARNING - 16:23:32: The solution is not feasible.
INFO - 16:23:32: Objective: -1.9978124577039875
INFO - 16:23:32: Standardized constraints:
INFO - 16:23:32: g_2 = 0.010000000000000009
INFO - 16:23:32: Design space:
INFO - 16:23:32: +------+-------------+-------+-------------+-------+
INFO - 16:23:32: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:32: +------+-------------+-------+-------------+-------+
INFO - 16:23:32: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:32: +------+-------------+-------+-------------+-------+
INFO - 16:23:32: *** End AerodynamicsScenario execution (time: 0:00:00.017082) ***
INFO - 16:23:32: *** Start StructureScenario execution ***
INFO - 16:23:32: StructureScenario
INFO - 16:23:32: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:32: MDO formulation: MDF
INFO - 16:23:32: Optimization problem:
INFO - 16:23:32: minimize 0.001*-y_4(x_1)
INFO - 16:23:32: with respect to x_1
INFO - 16:23:32: under the inequality constraints
INFO - 16:23:32: g_1(x_1) <= 0
INFO - 16:23:32: over the design space:
INFO - 16:23:32: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:32: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:32: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:32: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:32: | x_1[1] | 0.75 | 0.8264638086844417 | 1.25 | float |
INFO - 16:23:32: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:32: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:32: 2%|▏ | 1/50 [00:00<00:00, 97.48 it/sec, feas=True, obj=-2]
INFO - 16:23:32: 4%|▍ | 2/50 [00:00<00:01, 36.18 it/sec, feas=True, obj=-2.08]
WARNING - 16:23:32: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 0.0009157477359807847 is still above the tolerance 1e-06.
INFO - 16:23:32: 6%|▌ | 3/50 [00:00<00:01, 29.24 it/sec, feas=True, obj=-2.08]
WARNING - 16:23:32: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 0.0009157477359807847 is still above the tolerance 1e-06.
INFO - 16:23:32: 8%|▊ | 4/50 [00:00<00:01, 26.65 it/sec, feas=True, obj=-2.08]
WARNING - 16:23:32: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 0.0009157477359807847 is still above the tolerance 1e-06.
INFO - 16:23:32: 10%|█ | 5/50 [00:00<00:01, 25.29 it/sec, feas=True, obj=-2.08]
INFO - 16:23:32: 12%|█▏ | 6/50 [00:00<00:01, 26.51 it/sec, feas=True, obj=-2.08]
INFO - 16:23:32: Optimization result:
INFO - 16:23:32: Optimizer info:
INFO - 16:23:32: Status: None
INFO - 16:23:32: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:32: Solution:
INFO - 16:23:32: The solution is feasible.
INFO - 16:23:32: Objective: -2.0828738878823994
INFO - 16:23:32: Standardized constraints:
INFO - 16:23:32: g_1 = [-6.69869398e-02 -3.73369732e-02 -3.65073599e-02 -4.04881103e-02
INFO - 16:23:32: -4.50079933e-02 -2.40000000e-01 1.13207221e-11]
INFO - 16:23:32: Design space:
INFO - 16:23:32: +--------+-------------+-------------------+-------------+-------+
INFO - 16:23:32: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:32: +--------+-------------+-------------------+-------------+-------+
INFO - 16:23:32: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:32: | x_1[1] | 0.75 | 0.758860986177669 | 1.25 | float |
INFO - 16:23:32: +--------+-------------+-------------------+-------------+-------+
INFO - 16:23:32: *** End StructureScenario execution (time: 0:00:00.228750) ***
INFO - 16:23:32: *** Start PropulsionScenario execution ***
INFO - 16:23:32: PropulsionScenario
INFO - 16:23:32: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:32: MDO formulation: MDF
INFO - 16:23:32: Optimization problem:
INFO - 16:23:32: minimize 0.001*-y_4(x_3)
INFO - 16:23:32: with respect to x_3
INFO - 16:23:32: under the inequality constraints
INFO - 16:23:32: g_3(x_3) <= 0
INFO - 16:23:32: over the design space:
INFO - 16:23:32: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:32: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:32: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:32: | x_3 | 0.1 | 0.1766383461160826 | 1 | float |
INFO - 16:23:32: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:32: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:32: 2%|▏ | 1/50 [00:00<00:00, 90.18 it/sec, feas=True, obj=-2.08]
WARNING - 16:23:32: MDAGaussSeidel has reached its maximum number of unsuccessful iterations, but the normalized residual norm 6.724932466608626e-05 is still above the tolerance 1e-06.
INFO - 16:23:32: 4%|▍ | 2/50 [00:00<00:00, 76.34 it/sec, feas=True, obj=-2.08]
INFO - 16:23:32: 6%|▌ | 3/50 [00:00<00:00, 99.24 it/sec, feas=True, obj=-2.08]
INFO - 16:23:32: Optimization result:
INFO - 16:23:32: Optimizer info:
INFO - 16:23:32: Status: None
INFO - 16:23:32: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:32: Solution:
INFO - 16:23:32: The solution is feasible.
INFO - 16:23:32: Objective: -2.0828738878823994
INFO - 16:23:32: Standardized constraints:
INFO - 16:23:32: g_3 = [-7.60046158e-01 -2.39953842e-01 2.88657986e-15 -1.65669802e-01]
INFO - 16:23:32: Design space:
INFO - 16:23:32: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:32: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:32: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:32: | x_3 | 0.1 | 0.1766383461160826 | 1 | float |
INFO - 16:23:32: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:32: *** End PropulsionScenario execution (time: 0:00:00.032574) ***
INFO - 16:23:32: *** Start AerodynamicsScenario execution ***
INFO - 16:23:32: AerodynamicsScenario
INFO - 16:23:32: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:32: MDO formulation: MDF
INFO - 16:23:32: Optimization problem:
INFO - 16:23:32: minimize 0.001*-y_4(x_2)
INFO - 16:23:32: with respect to x_2
INFO - 16:23:32: under the inequality constraints
INFO - 16:23:32: g_2(x_2) <= 0
INFO - 16:23:32: over the design space:
INFO - 16:23:32: +------+-------------+-------+-------------+-------+
INFO - 16:23:32: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:32: +------+-------------+-------+-------------+-------+
INFO - 16:23:32: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:32: +------+-------------+-------+-------------+-------+
INFO - 16:23:32: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:32: 2%|▏ | 1/50 [00:00<00:00, 79.97 it/sec, feas=False, obj=-2.08]
INFO - 16:23:32: 4%|▍ | 2/50 [00:00<00:00, 128.99 it/sec, feas=False, obj=-2.08]
INFO - 16:23:32: 6%|▌ | 3/50 [00:00<00:00, 160.75 it/sec, feas=False, obj=-2.08]
INFO - 16:23:32: 8%|▊ | 4/50 [00:00<00:00, 182.69 it/sec, feas=False, obj=-2.08]
INFO - 16:23:32: 10%|█ | 5/50 [00:00<00:00, 199.37 it/sec, feas=False, obj=-2.08]
INFO - 16:23:32: 12%|█▏ | 6/50 [00:00<00:00, 211.84 it/sec, feas=False, obj=-2.08]
INFO - 16:23:32: 14%|█▍ | 7/50 [00:00<00:00, 222.05 it/sec, feas=False, obj=-2.08]
INFO - 16:23:32: 16%|█▌ | 8/50 [00:00<00:00, 230.07 it/sec, feas=False, obj=-2.08]
INFO - 16:23:32: 18%|█▊ | 9/50 [00:00<00:00, 237.44 it/sec, feas=False, obj=-2.08]
INFO - 16:23:32: 20%|██ | 10/50 [00:00<00:00, 244.60 it/sec, feas=False, obj=-2.08]
INFO - 16:23:32: 22%|██▏ | 11/50 [00:00<00:00, 250.72 it/sec, feas=False, obj=-2.08]
INFO - 16:23:32: 24%|██▍ | 12/50 [00:00<00:00, 174.29 it/sec, feas=False, obj=-2.08]
INFO - 16:23:32: 26%|██▌ | 13/50 [00:00<00:00, 180.63 it/sec, feas=False, obj=-2.08]
INFO - 16:23:32: 28%|██▊ | 14/50 [00:00<00:00, 186.23 it/sec, feas=False, obj=-2.08]
INFO - 16:23:32: 30%|███ | 15/50 [00:00<00:00, 191.44 it/sec, feas=False, obj=-2.08]
INFO - 16:23:32: 32%|███▏ | 16/50 [00:00<00:00, 196.07 it/sec, feas=False, obj=-2.08]
INFO - 16:23:32: 34%|███▍ | 17/50 [00:00<00:00, 200.48 it/sec, feas=False, obj=-2.08]
INFO - 16:23:32: 36%|███▌ | 18/50 [00:00<00:00, 204.39 it/sec, feas=False, obj=-2.08]
INFO - 16:23:32: 38%|███▊ | 19/50 [00:00<00:00, 168.80 it/sec, feas=False, obj=-2.08]
INFO - 16:23:32: 40%|████ | 20/50 [00:00<00:00, 172.69 it/sec, feas=False, obj=-2.08]
INFO - 16:23:32: 42%|████▏ | 21/50 [00:00<00:00, 176.42 it/sec, feas=False, obj=-2.08]
INFO - 16:23:32: 44%|████▍ | 22/50 [00:00<00:00, 179.99 it/sec, feas=False, obj=-2.08]
INFO - 16:23:32: 46%|████▌ | 23/50 [00:00<00:00, 183.40 it/sec, feas=False, obj=-2.08]
INFO - 16:23:32: 48%|████▊ | 24/50 [00:00<00:00, 186.60 it/sec, feas=False, obj=-2.08]
INFO - 16:23:32: 50%|█████ | 25/50 [00:00<00:00, 189.67 it/sec, feas=False, obj=-2.08]
INFO - 16:23:32: 52%|█████▏ | 26/50 [00:00<00:00, 192.59 it/sec, feas=False, obj=-2.08]
INFO - 16:23:32: 54%|█████▍ | 27/50 [00:00<00:00, 195.38 it/sec, feas=False, obj=-2.08]
INFO - 16:23:32: 56%|█████▌ | 28/50 [00:00<00:00, 198.04 it/sec, feas=False, obj=-2.08]
INFO - 16:23:32: 58%|█████▊ | 29/50 [00:00<00:00, 173.19 it/sec, feas=False, obj=-2.08]
INFO - 16:23:32: 60%|██████ | 30/50 [00:00<00:00, 175.86 it/sec, feas=False, obj=-2.08]
WARNING - 16:23:32: Optimization found no feasible point; the least infeasible point is selected.
INFO - 16:23:32: 62%|██████▏ | 31/50 [00:00<00:00, 169.49 it/sec, feas=False, obj=-2.08]
INFO - 16:23:32: Optimization result:
INFO - 16:23:32: Optimizer info:
INFO - 16:23:32: Status: 8
INFO - 16:23:32: Message: Positive directional derivative for linesearch
INFO - 16:23:32: Solution:
WARNING - 16:23:32: The solution is not feasible.
INFO - 16:23:32: Objective: -2.0828738878823994
INFO - 16:23:32: Standardized constraints:
INFO - 16:23:32: g_2 = 0.010000000000000009
INFO - 16:23:32: Design space:
INFO - 16:23:32: +------+-------------+-------+-------------+-------+
INFO - 16:23:32: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:32: +------+-------------+-------+-------------+-------+
INFO - 16:23:32: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:32: +------+-------------+-------+-------------+-------+
INFO - 16:23:32: *** End AerodynamicsScenario execution (time: 0:00:00.184627) ***
INFO - 16:23:32: *** Start StructureScenario execution ***
INFO - 16:23:32: StructureScenario
INFO - 16:23:32: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:32: MDO formulation: MDF
INFO - 16:23:32: Optimization problem:
INFO - 16:23:32: minimize 0.001*-y_4(x_1)
INFO - 16:23:32: with respect to x_1
INFO - 16:23:32: under the inequality constraints
INFO - 16:23:32: g_1(x_1) <= 0
INFO - 16:23:32: over the design space:
INFO - 16:23:32: +--------+-------------+-------------------+-------------+-------+
INFO - 16:23:32: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:32: +--------+-------------+-------------------+-------------+-------+
INFO - 16:23:32: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:32: | x_1[1] | 0.75 | 0.758860986177669 | 1.25 | float |
INFO - 16:23:32: +--------+-------------+-------------------+-------------+-------+
INFO - 16:23:32: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:32: 2%|▏ | 1/50 [00:00<00:00, 82.54 it/sec, feas=True, obj=-2.08]
INFO - 16:23:32: 4%|▍ | 2/50 [00:00<00:00, 88.37 it/sec, feas=True, obj=-2.08]
INFO - 16:23:32: 6%|▌ | 3/50 [00:00<00:00, 93.98 it/sec, feas=True, obj=-2.08]
INFO - 16:23:32: Optimization result:
INFO - 16:23:32: Optimizer info:
INFO - 16:23:32: Status: None
INFO - 16:23:32: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:32: Solution:
INFO - 16:23:32: The solution is feasible.
INFO - 16:23:32: Objective: -2.0828738878823994
INFO - 16:23:32: Standardized constraints:
INFO - 16:23:32: g_1 = [-6.69869398e-02 -3.73369732e-02 -3.65073599e-02 -4.04881103e-02
INFO - 16:23:32: -4.50079933e-02 -2.40000000e-01 1.13207221e-11]
INFO - 16:23:32: Design space:
INFO - 16:23:32: +--------+-------------+-------------------+-------------+-------+
INFO - 16:23:32: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:32: +--------+-------------+-------------------+-------------+-------+
INFO - 16:23:32: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:32: | x_1[1] | 0.75 | 0.758860986177669 | 1.25 | float |
INFO - 16:23:32: +--------+-------------+-------------------+-------------+-------+
INFO - 16:23:32: *** End StructureScenario execution (time: 0:00:00.034447) ***
INFO - 16:23:32: 16%|█▌ | 16/100 [00:15<01:23, 1.00 it/sec, feas=False, obj=-2.08]
INFO - 16:23:32: *** Start PropulsionScenario execution ***
INFO - 16:23:32: PropulsionScenario
INFO - 16:23:32: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:32: MDO formulation: MDF
INFO - 16:23:32: Optimization problem:
INFO - 16:23:32: minimize 0.001*-y_4(x_3)
INFO - 16:23:32: with respect to x_3
INFO - 16:23:32: under the inequality constraints
INFO - 16:23:32: g_3(x_3) <= 0
INFO - 16:23:32: over the design space:
INFO - 16:23:32: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:32: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:32: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:32: | x_3 | 0.1 | 0.1766383461160826 | 1 | float |
INFO - 16:23:32: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:32: Solving optimization problem with algorithm SLSQP:
WARNING - 16:23:32: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 6.724932466608626e-05 is still above the tolerance 1e-06.
INFO - 16:23:32: 2%|▏ | 1/50 [00:00<00:01, 33.31 it/sec, feas=True, obj=-1.78]
WARNING - 16:23:32: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 0.00020209792738312525 is still above the tolerance 1e-06.
INFO - 16:23:32: 4%|▍ | 2/50 [00:00<00:01, 25.81 it/sec, feas=True, obj=-1.82]
WARNING - 16:23:32: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 0.00013449864933217252 is still above the tolerance 1e-06.
INFO - 16:23:33: 6%|▌ | 3/50 [00:00<00:01, 24.07 it/sec, feas=True, obj=-1.82]
WARNING - 16:23:33: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 0.00020174797399825873 is still above the tolerance 1e-06.
INFO - 16:23:33: 8%|▊ | 4/50 [00:00<00:01, 23.25 it/sec, feas=True, obj=-1.82]
INFO - 16:23:33: Optimization result:
INFO - 16:23:33: Optimizer info:
INFO - 16:23:33: Status: None
INFO - 16:23:33: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:33: Solution:
INFO - 16:23:33: The solution is feasible.
INFO - 16:23:33: Objective: -1.8235453671182642
INFO - 16:23:33: Standardized constraints:
INFO - 16:23:33: g_3 = [-7.25018659e-01 -2.74981341e-01 4.44089210e-16 -1.55720362e-01]
INFO - 16:23:33: Design space:
INFO - 16:23:33: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:33: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:33: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:33: | x_3 | 0.1 | 0.1899274199511195 | 1 | float |
INFO - 16:23:33: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:33: *** End PropulsionScenario execution (time: 0:00:00.174722) ***
INFO - 16:23:33: *** Start AerodynamicsScenario execution ***
INFO - 16:23:33: AerodynamicsScenario
INFO - 16:23:33: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:33: MDO formulation: MDF
INFO - 16:23:33: Optimization problem:
INFO - 16:23:33: minimize 0.001*-y_4(x_2)
INFO - 16:23:33: with respect to x_2
INFO - 16:23:33: under the inequality constraints
INFO - 16:23:33: g_2(x_2) <= 0
INFO - 16:23:33: over the design space:
INFO - 16:23:33: +------+-------------+-------+-------------+-------+
INFO - 16:23:33: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:33: +------+-------------+-------+-------------+-------+
INFO - 16:23:33: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:33: +------+-------------+-------+-------------+-------+
INFO - 16:23:33: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:33: 2%|▏ | 1/50 [00:00<00:00, 87.07 it/sec, feas=True, obj=-1.82]
INFO - 16:23:33: Optimization result:
INFO - 16:23:33: Optimizer info:
INFO - 16:23:33: Status: 8
INFO - 16:23:33: Message: Positive directional derivative for linesearch
INFO - 16:23:33: Solution:
INFO - 16:23:33: The solution is feasible.
INFO - 16:23:33: Objective: -1.8235453671182646
INFO - 16:23:33: Standardized constraints:
INFO - 16:23:33: g_2 = -0.0035728811892454804
INFO - 16:23:33: Design space:
INFO - 16:23:33: +------+-------------+-------+-------------+-------+
INFO - 16:23:33: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:33: +------+-------------+-------+-------------+-------+
INFO - 16:23:33: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:33: +------+-------------+-------+-------------+-------+
INFO - 16:23:33: *** End AerodynamicsScenario execution (time: 0:00:00.013226) ***
INFO - 16:23:33: *** Start StructureScenario execution ***
INFO - 16:23:33: StructureScenario
INFO - 16:23:33: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:33: MDO formulation: MDF
INFO - 16:23:33: Optimization problem:
INFO - 16:23:33: minimize 0.001*-y_4(x_1)
INFO - 16:23:33: with respect to x_1
INFO - 16:23:33: under the inequality constraints
INFO - 16:23:33: g_1(x_1) <= 0
INFO - 16:23:33: over the design space:
INFO - 16:23:33: +--------+-------------+-------------------+-------------+-------+
INFO - 16:23:33: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:33: +--------+-------------+-------------------+-------------+-------+
INFO - 16:23:33: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:33: | x_1[1] | 0.75 | 0.758860986177669 | 1.25 | float |
INFO - 16:23:33: +--------+-------------+-------------------+-------------+-------+
INFO - 16:23:33: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:33: 2%|▏ | 1/50 [00:00<00:00, 97.05 it/sec, feas=False, obj=-1.82]
INFO - 16:23:33: 4%|▍ | 2/50 [00:00<00:01, 40.26 it/sec, feas=True, obj=-1.75]
INFO - 16:23:33: 6%|▌ | 3/50 [00:00<00:01, 33.13 it/sec, feas=True, obj=-1.76]
INFO - 16:23:33: 8%|▊ | 4/50 [00:00<00:01, 30.36 it/sec, feas=True, obj=-1.76]
INFO - 16:23:33: 10%|█ | 5/50 [00:00<00:01, 29.12 it/sec, feas=True, obj=-1.76]
INFO - 16:23:33: 12%|█▏ | 6/50 [00:00<00:01, 28.37 it/sec, feas=True, obj=-1.76]
INFO - 16:23:33: Optimization result:
INFO - 16:23:33: Optimizer info:
INFO - 16:23:33: Status: None
INFO - 16:23:33: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:33: Solution:
INFO - 16:23:33: The solution is feasible.
INFO - 16:23:33: Objective: -1.7562465412695143
INFO - 16:23:33: Standardized constraints:
INFO - 16:23:33: g_1 = [ 9.74775816e-14 -3.62382928e-03 -1.53268079e-02 -2.55137356e-02
INFO - 16:23:33: -3.36238293e-02 -2.29828719e-01 -1.01712814e-02]
INFO - 16:23:33: Design space:
INFO - 16:23:33: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:33: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:33: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:33: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:33: | x_1[1] | 0.75 | 0.8123346543629744 | 1.25 | float |
INFO - 16:23:33: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:33: *** End StructureScenario execution (time: 0:00:00.214305) ***
INFO - 16:23:33: *** Start PropulsionScenario execution ***
INFO - 16:23:33: PropulsionScenario
INFO - 16:23:33: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:33: MDO formulation: MDF
INFO - 16:23:33: Optimization problem:
INFO - 16:23:33: minimize 0.001*-y_4(x_3)
INFO - 16:23:33: with respect to x_3
INFO - 16:23:33: under the inequality constraints
INFO - 16:23:33: g_3(x_3) <= 0
INFO - 16:23:33: over the design space:
INFO - 16:23:33: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:33: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:33: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:33: | x_3 | 0.1 | 0.1899274199511195 | 1 | float |
INFO - 16:23:33: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:33: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:33: 2%|▏ | 1/50 [00:00<00:00, 88.10 it/sec, feas=True, obj=-1.76]
INFO - 16:23:33: Optimization result:
INFO - 16:23:33: Optimizer info:
INFO - 16:23:33: Status: 8
INFO - 16:23:33: Message: Positive directional derivative for linesearch
INFO - 16:23:33: Solution:
INFO - 16:23:33: The solution is feasible.
INFO - 16:23:33: Objective: -1.7562465412695143
INFO - 16:23:33: Standardized constraints:
INFO - 16:23:33: g_3 = [-7.24801092e-01 -2.75198908e-01 4.44089210e-16 -1.55720362e-01]
INFO - 16:23:33: Design space:
INFO - 16:23:33: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:33: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:33: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:33: | x_3 | 0.1 | 0.1899274199511195 | 1 | float |
INFO - 16:23:33: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:33: *** End PropulsionScenario execution (time: 0:00:00.013356) ***
INFO - 16:23:33: *** Start AerodynamicsScenario execution ***
INFO - 16:23:33: AerodynamicsScenario
INFO - 16:23:33: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:33: MDO formulation: MDF
INFO - 16:23:33: Optimization problem:
INFO - 16:23:33: minimize 0.001*-y_4(x_2)
INFO - 16:23:33: with respect to x_2
INFO - 16:23:33: under the inequality constraints
INFO - 16:23:33: g_2(x_2) <= 0
INFO - 16:23:33: over the design space:
INFO - 16:23:33: +------+-------------+-------+-------------+-------+
INFO - 16:23:33: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:33: +------+-------------+-------+-------------+-------+
INFO - 16:23:33: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:33: +------+-------------+-------+-------------+-------+
INFO - 16:23:33: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:33: 2%|▏ | 1/50 [00:00<00:00, 108.45 it/sec, feas=True, obj=-1.76]
INFO - 16:23:33: Optimization result:
INFO - 16:23:33: Optimizer info:
INFO - 16:23:33: Status: 8
INFO - 16:23:33: Message: Positive directional derivative for linesearch
INFO - 16:23:33: Solution:
INFO - 16:23:33: The solution is feasible.
INFO - 16:23:33: Objective: -1.7562465412695143
INFO - 16:23:33: Standardized constraints:
INFO - 16:23:33: g_2 = -0.0035728811892454804
INFO - 16:23:33: Design space:
INFO - 16:23:33: +------+-------------+-------+-------------+-------+
INFO - 16:23:33: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:33: +------+-------------+-------+-------------+-------+
INFO - 16:23:33: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:33: +------+-------------+-------+-------------+-------+
INFO - 16:23:33: *** End AerodynamicsScenario execution (time: 0:00:00.010755) ***
INFO - 16:23:33: *** Start StructureScenario execution ***
INFO - 16:23:33: StructureScenario
INFO - 16:23:33: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:33: MDO formulation: MDF
INFO - 16:23:33: Optimization problem:
INFO - 16:23:33: minimize 0.001*-y_4(x_1)
INFO - 16:23:33: with respect to x_1
INFO - 16:23:33: under the inequality constraints
INFO - 16:23:33: g_1(x_1) <= 0
INFO - 16:23:33: over the design space:
INFO - 16:23:33: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:33: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:33: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:33: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:33: | x_1[1] | 0.75 | 0.8123346543629744 | 1.25 | float |
INFO - 16:23:33: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:33: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:33: 2%|▏ | 1/50 [00:00<00:00, 102.50 it/sec, feas=True, obj=-1.76]
INFO - 16:23:33: 4%|▍ | 2/50 [00:00<00:00, 60.08 it/sec, feas=True, obj=-1.76]
INFO - 16:23:33: 6%|▌ | 3/50 [00:00<00:00, 75.37 it/sec, feas=True, obj=-1.76]
INFO - 16:23:33: Optimization result:
INFO - 16:23:33: Optimizer info:
INFO - 16:23:33: Status: None
INFO - 16:23:33: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:33: Solution:
INFO - 16:23:33: The solution is feasible.
INFO - 16:23:33: Objective: -1.7562465412695143
INFO - 16:23:33: Standardized constraints:
INFO - 16:23:33: g_1 = [ 9.74775816e-14 -3.62382928e-03 -1.53268079e-02 -2.55137356e-02
INFO - 16:23:33: -3.36238293e-02 -2.29828719e-01 -1.01712814e-02]
INFO - 16:23:33: Design space:
INFO - 16:23:33: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:33: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:33: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:33: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:33: | x_1[1] | 0.75 | 0.8123346543629744 | 1.25 | float |
INFO - 16:23:33: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:33: *** End StructureScenario execution (time: 0:00:00.042291) ***
INFO - 16:23:33: 17%|█▋ | 17/100 [00:16<01:20, 1.03 it/sec, feas=True, obj=-1.76]
INFO - 16:23:33: *** Start PropulsionScenario execution ***
INFO - 16:23:33: PropulsionScenario
INFO - 16:23:33: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:33: MDO formulation: MDF
INFO - 16:23:33: Optimization problem:
INFO - 16:23:33: minimize 0.001*-y_4(x_3)
INFO - 16:23:33: with respect to x_3
INFO - 16:23:33: under the inequality constraints
INFO - 16:23:33: g_3(x_3) <= 0
INFO - 16:23:33: over the design space:
INFO - 16:23:33: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:33: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:33: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:33: | x_3 | 0.1 | 0.1899274199511195 | 1 | float |
INFO - 16:23:33: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:33: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:33: 2%|▏ | 1/50 [00:00<00:01, 41.78 it/sec, feas=False, obj=-2.06]
INFO - 16:23:33: 4%|▍ | 2/50 [00:00<00:01, 43.83 it/sec, feas=True, obj=-2.03]
INFO - 16:23:33: 6%|▌ | 3/50 [00:00<00:01, 35.95 it/sec, feas=False, obj=-2.06]
INFO - 16:23:33: 8%|▊ | 4/50 [00:00<00:01, 32.96 it/sec, feas=True, obj=-2.03]
INFO - 16:23:33: 10%|█ | 5/50 [00:00<00:01, 34.81 it/sec, feas=True, obj=-2.03]
INFO - 16:23:33: 12%|█▏ | 6/50 [00:00<00:01, 36.22 it/sec, feas=True, obj=-2.03]
INFO - 16:23:33: Optimization result:
INFO - 16:23:33: Optimizer info:
INFO - 16:23:33: Status: None
INFO - 16:23:33: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:33: Solution:
INFO - 16:23:33: The solution is feasible.
INFO - 16:23:33: Objective: -2.0319358723538214
INFO - 16:23:33: Standardized constraints:
INFO - 16:23:33: g_3 = [-7.60781149e-01 -2.39218851e-01 -4.44089210e-16 -1.69700308e-01]
INFO - 16:23:33: Design space:
INFO - 16:23:33: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:33: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:33: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:33: | x_3 | 0.1 | 0.1716759097349043 | 1 | float |
INFO - 16:23:33: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:33: *** End PropulsionScenario execution (time: 0:00:00.168036) ***
INFO - 16:23:33: *** Start AerodynamicsScenario execution ***
INFO - 16:23:33: AerodynamicsScenario
INFO - 16:23:33: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:33: MDO formulation: MDF
INFO - 16:23:33: Optimization problem:
INFO - 16:23:33: minimize 0.001*-y_4(x_2)
INFO - 16:23:33: with respect to x_2
INFO - 16:23:33: under the inequality constraints
INFO - 16:23:33: g_2(x_2) <= 0
INFO - 16:23:33: over the design space:
INFO - 16:23:33: +------+-------------+-------+-------------+-------+
INFO - 16:23:33: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:33: +------+-------------+-------+-------------+-------+
INFO - 16:23:33: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:33: +------+-------------+-------+-------------+-------+
INFO - 16:23:33: Solving optimization problem with algorithm SLSQP:
WARNING - 16:23:33: Optimization found no feasible point; the least infeasible point is selected.
INFO - 16:23:33: 2%|▏ | 1/50 [00:00<00:00, 75.38 it/sec, feas=False, obj=-2.03]
INFO - 16:23:33: Optimization result:
INFO - 16:23:33: Optimizer info:
INFO - 16:23:33: Status: 8
INFO - 16:23:33: Message: Positive directional derivative for linesearch
INFO - 16:23:33: Solution:
WARNING - 16:23:33: The solution is not feasible.
INFO - 16:23:33: Objective: -2.0319358723538214
INFO - 16:23:33: Standardized constraints:
INFO - 16:23:33: g_2 = 0.006512928860621825
INFO - 16:23:33: Design space:
INFO - 16:23:33: +------+-------------+-------+-------------+-------+
INFO - 16:23:33: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:33: +------+-------------+-------+-------------+-------+
INFO - 16:23:33: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:33: +------+-------------+-------+-------------+-------+
INFO - 16:23:33: *** End AerodynamicsScenario execution (time: 0:00:00.014995) ***
INFO - 16:23:33: *** Start StructureScenario execution ***
INFO - 16:23:33: StructureScenario
INFO - 16:23:33: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:33: MDO formulation: MDF
INFO - 16:23:33: Optimization problem:
INFO - 16:23:33: minimize 0.001*-y_4(x_1)
INFO - 16:23:33: with respect to x_1
INFO - 16:23:33: under the inequality constraints
INFO - 16:23:33: g_1(x_1) <= 0
INFO - 16:23:33: over the design space:
INFO - 16:23:33: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:33: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:33: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:33: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:33: | x_1[1] | 0.75 | 0.8123346543629744 | 1.25 | float |
INFO - 16:23:33: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:33: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:33: 2%|▏ | 1/50 [00:00<00:00, 96.08 it/sec, feas=True, obj=-2.03]
INFO - 16:23:33: 4%|▍ | 2/50 [00:00<00:01, 37.75 it/sec, feas=True, obj=-2.07]
INFO - 16:23:33: 6%|▌ | 3/50 [00:00<00:01, 31.45 it/sec, feas=True, obj=-2.08]
INFO - 16:23:33: 8%|▊ | 4/50 [00:00<00:01, 28.98 it/sec, feas=True, obj=-2.08]
INFO - 16:23:33: 10%|█ | 5/50 [00:00<00:01, 27.68 it/sec, feas=True, obj=-2.08]
INFO - 16:23:33: Optimization result:
INFO - 16:23:33: Optimizer info:
INFO - 16:23:33: Status: 8
INFO - 16:23:33: Message: Positive directional derivative for linesearch
INFO - 16:23:33: Solution:
INFO - 16:23:33: The solution is feasible.
INFO - 16:23:33: Objective: -2.0753700033182243
INFO - 16:23:33: Standardized constraints:
INFO - 16:23:33: g_1 = [-0.0551151 -0.03124244 -0.03261897 -0.03770501 -0.04287074 -0.24
INFO - 16:23:33: 0. ]
INFO - 16:23:33: Design space:
INFO - 16:23:33: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:33: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:33: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:33: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:33: | x_1[1] | 0.75 | 0.7806436836765263 | 1.25 | float |
INFO - 16:23:33: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:33: *** End StructureScenario execution (time: 0:00:00.182799) ***
INFO - 16:23:33: *** Start PropulsionScenario execution ***
INFO - 16:23:33: PropulsionScenario
INFO - 16:23:33: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:33: MDO formulation: MDF
INFO - 16:23:33: Optimization problem:
INFO - 16:23:33: minimize 0.001*-y_4(x_3)
INFO - 16:23:33: with respect to x_3
INFO - 16:23:33: under the inequality constraints
INFO - 16:23:33: g_3(x_3) <= 0
INFO - 16:23:33: over the design space:
INFO - 16:23:33: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:33: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:33: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:33: | x_3 | 0.1 | 0.1716759097349043 | 1 | float |
INFO - 16:23:33: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:33: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:33: 2%|▏ | 1/50 [00:00<00:00, 88.86 it/sec, feas=True, obj=-2.08]
INFO - 16:23:33: Optimization result:
INFO - 16:23:33: Optimizer info:
INFO - 16:23:33: Status: 8
INFO - 16:23:33: Message: Positive directional derivative for linesearch
INFO - 16:23:33: Solution:
INFO - 16:23:33: The solution is feasible.
INFO - 16:23:33: Objective: -2.0753700033182243
INFO - 16:23:33: Standardized constraints:
INFO - 16:23:33: g_3 = [-7.60908105e-01 -2.39091895e-01 -4.44089210e-16 -1.69700308e-01]
INFO - 16:23:33: Design space:
INFO - 16:23:33: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:33: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:33: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:33: | x_3 | 0.1 | 0.1716759097349043 | 1 | float |
INFO - 16:23:33: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:33: *** End PropulsionScenario execution (time: 0:00:00.013148) ***
INFO - 16:23:33: *** Start AerodynamicsScenario execution ***
INFO - 16:23:33: AerodynamicsScenario
INFO - 16:23:33: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:33: MDO formulation: MDF
INFO - 16:23:33: Optimization problem:
INFO - 16:23:33: minimize 0.001*-y_4(x_2)
INFO - 16:23:33: with respect to x_2
INFO - 16:23:33: under the inequality constraints
INFO - 16:23:33: g_2(x_2) <= 0
INFO - 16:23:33: over the design space:
INFO - 16:23:33: +------+-------------+-------+-------------+-------+
INFO - 16:23:33: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:33: +------+-------------+-------+-------------+-------+
INFO - 16:23:33: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:33: +------+-------------+-------+-------------+-------+
INFO - 16:23:33: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:33: 2%|▏ | 1/50 [00:00<00:00, 109.16 it/sec, feas=False, obj=-2.08]
INFO - 16:23:33: 4%|▍ | 2/50 [00:00<00:00, 173.08 it/sec, feas=False, obj=-2.08]
INFO - 16:23:33: 6%|▌ | 3/50 [00:00<00:00, 213.61 it/sec, feas=False, obj=-2.08]
INFO - 16:23:33: 8%|▊ | 4/50 [00:00<00:00, 240.84 it/sec, feas=False, obj=-2.08]
INFO - 16:23:33: 10%|█ | 5/50 [00:00<00:00, 261.20 it/sec, feas=False, obj=-2.08]
INFO - 16:23:33: 12%|█▏ | 6/50 [00:00<00:00, 276.69 it/sec, feas=False, obj=-2.08]
INFO - 16:23:33: 14%|█▍ | 7/50 [00:00<00:00, 288.98 it/sec, feas=False, obj=-2.08]
INFO - 16:23:33: 16%|█▌ | 8/50 [00:00<00:00, 299.09 it/sec, feas=False, obj=-2.08]
INFO - 16:23:33: 18%|█▊ | 9/50 [00:00<00:00, 308.55 it/sec, feas=False, obj=-2.08]
INFO - 16:23:33: 20%|██ | 10/50 [00:00<00:00, 316.52 it/sec, feas=False, obj=-2.08]
INFO - 16:23:33: 22%|██▏ | 11/50 [00:00<00:00, 217.56 it/sec, feas=False, obj=-2.08]
INFO - 16:23:33: 24%|██▍ | 12/50 [00:00<00:00, 225.50 it/sec, feas=False, obj=-2.08]
INFO - 16:23:33: 26%|██▌ | 13/50 [00:00<00:00, 233.01 it/sec, feas=False, obj=-2.08]
INFO - 16:23:33: 28%|██▊ | 14/50 [00:00<00:00, 239.97 it/sec, feas=False, obj=-2.08]
INFO - 16:23:33: 30%|███ | 15/50 [00:00<00:00, 246.33 it/sec, feas=False, obj=-2.08]
INFO - 16:23:33: 32%|███▏ | 16/50 [00:00<00:00, 251.55 it/sec, feas=False, obj=-2.08]
INFO - 16:23:33: 34%|███▍ | 17/50 [00:00<00:00, 257.01 it/sec, feas=False, obj=-2.08]
INFO - 16:23:33: 36%|███▌ | 18/50 [00:00<00:00, 202.97 it/sec, feas=False, obj=-2.08]
INFO - 16:23:33: 38%|███▊ | 19/50 [00:00<00:00, 203.23 it/sec, feas=False, obj=-2.08]
INFO - 16:23:33: 40%|████ | 20/50 [00:00<00:00, 208.70 it/sec, feas=False, obj=-2.08]
INFO - 16:23:33: 42%|████▏ | 21/50 [00:00<00:00, 213.48 it/sec, feas=False, obj=-2.08]
INFO - 16:23:33: 44%|████▍ | 22/50 [00:00<00:00, 218.02 it/sec, feas=False, obj=-2.08]
INFO - 16:23:33: 46%|████▌ | 23/50 [00:00<00:00, 222.37 it/sec, feas=False, obj=-2.08]
INFO - 16:23:33: 48%|████▊ | 24/50 [00:00<00:00, 226.53 it/sec, feas=False, obj=-2.08]
INFO - 16:23:33: 50%|█████ | 25/50 [00:00<00:00, 230.22 it/sec, feas=False, obj=-2.08]
INFO - 16:23:33: 52%|█████▏ | 26/50 [00:00<00:00, 234.04 it/sec, feas=False, obj=-2.08]
INFO - 16:23:33: 54%|█████▍ | 27/50 [00:00<00:00, 237.60 it/sec, feas=False, obj=-2.08]
INFO - 16:23:33: 56%|█████▌ | 28/50 [00:00<00:00, 241.03 it/sec, feas=False, obj=-2.08]
INFO - 16:23:33: 58%|█████▊ | 29/50 [00:00<00:00, 244.22 it/sec, feas=False, obj=-2.08]
WARNING - 16:23:33: Optimization found no feasible point; the least infeasible point is selected.
INFO - 16:23:33: 60%|██████ | 30/50 [00:00<00:00, 215.39 it/sec, feas=False, obj=-2.08]
INFO - 16:23:33: Optimization result:
INFO - 16:23:33: Optimizer info:
INFO - 16:23:33: Status: 8
INFO - 16:23:33: Message: Positive directional derivative for linesearch
INFO - 16:23:33: Solution:
WARNING - 16:23:33: The solution is not feasible.
INFO - 16:23:33: Objective: -2.0753700033182243
INFO - 16:23:33: Standardized constraints:
INFO - 16:23:33: g_2 = 0.006512928860621825
INFO - 16:23:33: Design space:
INFO - 16:23:33: +------+-------------+-------+-------------+-------+
INFO - 16:23:33: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:33: +------+-------------+-------+-------------+-------+
INFO - 16:23:33: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:33: +------+-------------+-------+-------------+-------+
INFO - 16:23:33: *** End AerodynamicsScenario execution (time: 0:00:00.141087) ***
INFO - 16:23:33: *** Start StructureScenario execution ***
INFO - 16:23:33: StructureScenario
INFO - 16:23:33: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:33: MDO formulation: MDF
INFO - 16:23:33: Optimization problem:
INFO - 16:23:33: minimize 0.001*-y_4(x_1)
INFO - 16:23:33: with respect to x_1
INFO - 16:23:33: under the inequality constraints
INFO - 16:23:33: g_1(x_1) <= 0
INFO - 16:23:33: over the design space:
INFO - 16:23:33: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:33: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:33: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:33: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:33: | x_1[1] | 0.75 | 0.7806436836765263 | 1.25 | float |
INFO - 16:23:33: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:33: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:33: 2%|▏ | 1/50 [00:00<00:00, 75.84 it/sec, feas=True, obj=-2.08]
INFO - 16:23:33: Optimization result:
INFO - 16:23:33: Optimizer info:
INFO - 16:23:33: Status: 8
INFO - 16:23:33: Message: Positive directional derivative for linesearch
INFO - 16:23:33: Solution:
INFO - 16:23:33: The solution is feasible.
INFO - 16:23:33: Objective: -2.0753700033182243
INFO - 16:23:33: Standardized constraints:
INFO - 16:23:33: g_1 = [-0.0551151 -0.03124244 -0.03261897 -0.03770501 -0.04287074 -0.24
INFO - 16:23:33: 0. ]
INFO - 16:23:33: Design space:
INFO - 16:23:33: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:33: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:33: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:33: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:33: | x_1[1] | 0.75 | 0.7806436836765263 | 1.25 | float |
INFO - 16:23:33: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:33: *** End StructureScenario execution (time: 0:00:00.015329) ***
INFO - 16:23:33: 18%|█▊ | 18/100 [00:17<01:17, 1.05 it/sec, feas=False, obj=-2.08]
INFO - 16:23:33: *** Start PropulsionScenario execution ***
INFO - 16:23:33: PropulsionScenario
INFO - 16:23:33: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:33: MDO formulation: MDF
INFO - 16:23:33: Optimization problem:
INFO - 16:23:33: minimize 0.001*-y_4(x_3)
INFO - 16:23:33: with respect to x_3
INFO - 16:23:33: under the inequality constraints
INFO - 16:23:33: g_3(x_3) <= 0
INFO - 16:23:33: over the design space:
INFO - 16:23:33: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:33: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:33: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:33: | x_3 | 0.1 | 0.1716759097349043 | 1 | float |
INFO - 16:23:33: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:33: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:34: 2%|▏ | 1/50 [00:00<00:01, 34.75 it/sec, feas=True, obj=-1.7]
INFO - 16:23:34: 4%|▍ | 2/50 [00:00<00:01, 27.06 it/sec, feas=True, obj=-1.77]
WARNING - 16:23:34: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 6.724932466608626e-05 is still above the tolerance 1e-06.
INFO - 16:23:34: 6%|▌ | 3/50 [00:00<00:01, 24.77 it/sec, feas=True, obj=-1.77]
INFO - 16:23:34: Optimization result:
INFO - 16:23:34: Optimizer info:
INFO - 16:23:34: Status: 8
INFO - 16:23:34: Message: Positive directional derivative for linesearch
INFO - 16:23:34: Solution:
INFO - 16:23:34: The solution is feasible.
INFO - 16:23:34: Objective: -1.7719444451107387
INFO - 16:23:34: Standardized constraints:
INFO - 16:23:34: g_3 = [-7.12243630e-01 -2.87756370e-01 3.08642001e-14 -1.54820592e-01]
INFO - 16:23:34: Design space:
INFO - 16:23:34: +------+-------------+-------------------+-------------+-------+
INFO - 16:23:34: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:34: +------+-------------+-------------------+-------------+-------+
INFO - 16:23:34: | x_3 | 0.1 | 0.193481053267354 | 1 | float |
INFO - 16:23:34: +------+-------------+-------------------+-------------+-------+
INFO - 16:23:34: *** End PropulsionScenario execution (time: 0:00:00.123238) ***
INFO - 16:23:34: *** Start AerodynamicsScenario execution ***
INFO - 16:23:34: AerodynamicsScenario
INFO - 16:23:34: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:34: MDO formulation: MDF
INFO - 16:23:34: Optimization problem:
INFO - 16:23:34: minimize 0.001*-y_4(x_2)
INFO - 16:23:34: with respect to x_2
INFO - 16:23:34: under the inequality constraints
INFO - 16:23:34: g_2(x_2) <= 0
INFO - 16:23:34: over the design space:
INFO - 16:23:34: +------+-------------+-------+-------------+-------+
INFO - 16:23:34: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:34: +------+-------------+-------+-------------+-------+
INFO - 16:23:34: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:34: +------+-------------+-------+-------------+-------+
INFO - 16:23:34: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:34: 2%|▏ | 1/50 [00:00<00:00, 74.38 it/sec, feas=True, obj=-1.77]
INFO - 16:23:34: Optimization result:
INFO - 16:23:34: Optimizer info:
INFO - 16:23:34: Status: 8
INFO - 16:23:34: Message: Positive directional derivative for linesearch
INFO - 16:23:34: Solution:
INFO - 16:23:34: The solution is feasible.
INFO - 16:23:34: Objective: -1.7719444451107387
INFO - 16:23:34: Standardized constraints:
INFO - 16:23:34: g_2 = -0.0031126499831755083
INFO - 16:23:34: Design space:
INFO - 16:23:34: +------+-------------+-------+-------------+-------+
INFO - 16:23:34: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:34: +------+-------------+-------+-------------+-------+
INFO - 16:23:34: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:34: +------+-------------+-------+-------------+-------+
INFO - 16:23:34: *** End AerodynamicsScenario execution (time: 0:00:00.015091) ***
INFO - 16:23:34: *** Start StructureScenario execution ***
INFO - 16:23:34: StructureScenario
INFO - 16:23:34: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:34: MDO formulation: MDF
INFO - 16:23:34: Optimization problem:
INFO - 16:23:34: minimize 0.001*-y_4(x_1)
INFO - 16:23:34: with respect to x_1
INFO - 16:23:34: under the inequality constraints
INFO - 16:23:34: g_1(x_1) <= 0
INFO - 16:23:34: over the design space:
INFO - 16:23:34: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:34: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:34: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:34: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:34: | x_1[1] | 0.75 | 0.7806436836765263 | 1.25 | float |
INFO - 16:23:34: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:34: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:34: 2%|▏ | 1/50 [00:00<00:00, 80.82 it/sec, feas=False, obj=-1.77]
INFO - 16:23:34: 4%|▍ | 2/50 [00:00<00:01, 37.17 it/sec, feas=True, obj=-1.74]
WARNING - 16:23:34: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 0.0018314954719615695 is still above the tolerance 1e-06.
INFO - 16:23:34: 6%|▌ | 3/50 [00:00<00:01, 29.88 it/sec, feas=True, obj=-1.74]
INFO - 16:23:34: 8%|▊ | 4/50 [00:00<00:01, 28.51 it/sec, feas=True, obj=-1.74]
INFO - 16:23:34: 10%|█ | 5/50 [00:00<00:01, 27.79 it/sec, feas=True, obj=-1.74]
INFO - 16:23:34: 12%|█▏ | 6/50 [00:00<00:01, 27.31 it/sec, feas=True, obj=-1.74]
INFO - 16:23:34: Optimization result:
INFO - 16:23:34: Optimizer info:
INFO - 16:23:34: Status: None
INFO - 16:23:34: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:34: Solution:
INFO - 16:23:34: The solution is feasible.
INFO - 16:23:34: Objective: -1.7388059433359162
INFO - 16:23:34: Standardized constraints:
INFO - 16:23:34: g_1 = [ 2.22044605e-16 -3.29851444e-03 -1.49608287e-02 -2.51623956e-02
INFO - 16:23:34: -3.32985144e-02 -2.31217081e-01 -8.78291900e-03]
INFO - 16:23:34: Design space:
INFO - 16:23:34: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:34: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:34: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:34: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:34: | x_1[1] | 0.75 | 0.8080816092616823 | 1.25 | float |
INFO - 16:23:34: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:34: *** End StructureScenario execution (time: 0:00:00.222594) ***
INFO - 16:23:34: *** Start PropulsionScenario execution ***
INFO - 16:23:34: PropulsionScenario
INFO - 16:23:34: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:34: MDO formulation: MDF
INFO - 16:23:34: Optimization problem:
INFO - 16:23:34: minimize 0.001*-y_4(x_3)
INFO - 16:23:34: with respect to x_3
INFO - 16:23:34: under the inequality constraints
INFO - 16:23:34: g_3(x_3) <= 0
INFO - 16:23:34: over the design space:
INFO - 16:23:34: +------+-------------+-------------------+-------------+-------+
INFO - 16:23:34: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:34: +------+-------------+-------------------+-------------+-------+
INFO - 16:23:34: | x_3 | 0.1 | 0.193481053267354 | 1 | float |
INFO - 16:23:34: +------+-------------+-------------------+-------------+-------+
INFO - 16:23:34: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:34: 2%|▏ | 1/50 [00:00<00:00, 84.13 it/sec, feas=True, obj=-1.74]
INFO - 16:23:34: Optimization result:
INFO - 16:23:34: Optimizer info:
INFO - 16:23:34: Status: 8
INFO - 16:23:34: Message: Positive directional derivative for linesearch
INFO - 16:23:34: Solution:
INFO - 16:23:34: The solution is feasible.
INFO - 16:23:34: Objective: -1.7388059433359162
INFO - 16:23:34: Standardized constraints:
INFO - 16:23:34: g_3 = [-7.12125937e-01 -2.87874063e-01 3.08642001e-14 -1.54820592e-01]
INFO - 16:23:34: Design space:
INFO - 16:23:34: +------+-------------+-------------------+-------------+-------+
INFO - 16:23:34: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:34: +------+-------------+-------------------+-------------+-------+
INFO - 16:23:34: | x_3 | 0.1 | 0.193481053267354 | 1 | float |
INFO - 16:23:34: +------+-------------+-------------------+-------------+-------+
INFO - 16:23:34: *** End PropulsionScenario execution (time: 0:00:00.013852) ***
INFO - 16:23:34: *** Start AerodynamicsScenario execution ***
INFO - 16:23:34: AerodynamicsScenario
INFO - 16:23:34: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:34: MDO formulation: MDF
INFO - 16:23:34: Optimization problem:
INFO - 16:23:34: minimize 0.001*-y_4(x_2)
INFO - 16:23:34: with respect to x_2
INFO - 16:23:34: under the inequality constraints
INFO - 16:23:34: g_2(x_2) <= 0
INFO - 16:23:34: over the design space:
INFO - 16:23:34: +------+-------------+-------+-------------+-------+
INFO - 16:23:34: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:34: +------+-------------+-------+-------------+-------+
INFO - 16:23:34: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:34: +------+-------------+-------+-------------+-------+
INFO - 16:23:34: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:34: 2%|▏ | 1/50 [00:00<00:00, 106.40 it/sec, feas=True, obj=-1.74]
INFO - 16:23:34: Optimization result:
INFO - 16:23:34: Optimizer info:
INFO - 16:23:34: Status: 8
INFO - 16:23:34: Message: Positive directional derivative for linesearch
INFO - 16:23:34: Solution:
INFO - 16:23:34: The solution is feasible.
INFO - 16:23:34: Objective: -1.7388059433359162
INFO - 16:23:34: Standardized constraints:
INFO - 16:23:34: g_2 = -0.0031126499831755083
INFO - 16:23:34: Design space:
INFO - 16:23:34: +------+-------------+-------+-------------+-------+
INFO - 16:23:34: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:34: +------+-------------+-------+-------------+-------+
INFO - 16:23:34: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:34: +------+-------------+-------+-------------+-------+
INFO - 16:23:34: *** End AerodynamicsScenario execution (time: 0:00:00.010925) ***
INFO - 16:23:34: *** Start StructureScenario execution ***
INFO - 16:23:34: StructureScenario
INFO - 16:23:34: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:34: MDO formulation: MDF
INFO - 16:23:34: Optimization problem:
INFO - 16:23:34: minimize 0.001*-y_4(x_1)
INFO - 16:23:34: with respect to x_1
INFO - 16:23:34: under the inequality constraints
INFO - 16:23:34: g_1(x_1) <= 0
INFO - 16:23:34: over the design space:
INFO - 16:23:34: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:34: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:34: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:34: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:34: | x_1[1] | 0.75 | 0.8080816092616823 | 1.25 | float |
INFO - 16:23:34: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:34: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:34: 2%|▏ | 1/50 [00:00<00:00, 101.09 it/sec, feas=True, obj=-1.74]
INFO - 16:23:34: Optimization result:
INFO - 16:23:34: Optimizer info:
INFO - 16:23:34: Status: 8
INFO - 16:23:34: Message: Positive directional derivative for linesearch
INFO - 16:23:34: Solution:
INFO - 16:23:34: The solution is feasible.
INFO - 16:23:34: Objective: -1.7388059433359162
INFO - 16:23:34: Standardized constraints:
INFO - 16:23:34: g_1 = [ 2.22044605e-16 -3.29851444e-03 -1.49608287e-02 -2.51623956e-02
INFO - 16:23:34: -3.32985144e-02 -2.31217081e-01 -8.78291900e-03]
INFO - 16:23:34: Design space:
INFO - 16:23:34: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:34: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:34: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:34: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:34: | x_1[1] | 0.75 | 0.8080816092616823 | 1.25 | float |
INFO - 16:23:34: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:34: *** End StructureScenario execution (time: 0:00:00.011803) ***
INFO - 16:23:34: 19%|█▉ | 19/100 [00:17<01:14, 1.08 it/sec, feas=True, obj=-1.74]
INFO - 16:23:34: *** Start PropulsionScenario execution ***
INFO - 16:23:34: PropulsionScenario
INFO - 16:23:34: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:34: MDO formulation: MDF
INFO - 16:23:34: Optimization problem:
INFO - 16:23:34: minimize 0.001*-y_4(x_3)
INFO - 16:23:34: with respect to x_3
INFO - 16:23:34: under the inequality constraints
INFO - 16:23:34: g_3(x_3) <= 0
INFO - 16:23:34: over the design space:
INFO - 16:23:34: +------+-------------+-------------------+-------------+-------+
INFO - 16:23:34: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:34: +------+-------------+-------------------+-------------+-------+
INFO - 16:23:34: | x_3 | 0.1 | 0.193481053267354 | 1 | float |
INFO - 16:23:34: +------+-------------+-------------------+-------------+-------+
INFO - 16:23:34: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:34: 2%|▏ | 1/50 [00:00<00:01, 42.16 it/sec, feas=False, obj=-2.19]
INFO - 16:23:34: 4%|▍ | 2/50 [00:00<00:01, 39.01 it/sec, feas=True, obj=-2.16]
WARNING - 16:23:34: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 6.724932466608626e-05 is still above the tolerance 1e-06.
INFO - 16:23:34: 6%|▌ | 3/50 [00:00<00:01, 30.77 it/sec, feas=False, obj=-2.19]
INFO - 16:23:34: 8%|▊ | 4/50 [00:00<00:01, 31.91 it/sec, feas=True, obj=-2.16]
INFO - 16:23:34: 10%|█ | 5/50 [00:00<00:01, 30.65 it/sec, feas=False, obj=-2.18]
INFO - 16:23:34: 12%|█▏ | 6/50 [00:00<00:01, 30.92 it/sec, feas=True, obj=-2.16]
INFO - 16:23:34: 14%|█▍ | 7/50 [00:00<00:01, 30.13 it/sec, feas=False, obj=-2.18]
INFO - 16:23:34: 16%|█▌ | 8/50 [00:00<00:01, 29.64 it/sec, feas=False, obj=-2.17]
INFO - 16:23:34: 18%|█▊ | 9/50 [00:00<00:01, 29.20 it/sec, feas=False, obj=-2.17]
INFO - 16:23:34: 20%|██ | 10/50 [00:00<00:01, 29.79 it/sec, feas=True, obj=-2.16]
INFO - 16:23:34: 22%|██▏ | 11/50 [00:00<00:01, 29.26 it/sec, feas=False, obj=-2.17]
INFO - 16:23:34: 24%|██▍ | 12/50 [00:00<00:01, 28.89 it/sec, feas=False, obj=-2.17]
INFO - 16:23:34: 26%|██▌ | 13/50 [00:00<00:01, 28.48 it/sec, feas=False, obj=-2.17]
INFO - 16:23:34: 28%|██▊ | 14/50 [00:00<00:01, 28.27 it/sec, feas=False, obj=-2.17]
INFO - 16:23:34: 30%|███ | 15/50 [00:00<00:01, 28.69 it/sec, feas=True, obj=-2.16]
INFO - 16:23:34: 32%|███▏ | 16/50 [00:00<00:01, 28.44 it/sec, feas=False, obj=-2.17]
INFO - 16:23:35: 34%|███▍ | 17/50 [00:00<00:01, 28.23 it/sec, feas=False, obj=-2.17]
INFO - 16:23:35: 36%|███▌ | 18/50 [00:00<00:01, 28.04 it/sec, feas=False, obj=-2.17]
INFO - 16:23:35: 38%|███▊ | 19/50 [00:00<00:01, 27.89 it/sec, feas=False, obj=-2.17]
INFO - 16:23:35: 40%|████ | 20/50 [00:00<00:01, 27.73 it/sec, feas=False, obj=-2.16]
INFO - 16:23:35: 42%|████▏ | 21/50 [00:00<00:01, 27.61 it/sec, feas=False, obj=-2.16]
INFO - 16:23:35: 44%|████▍ | 22/50 [00:00<00:01, 27.87 it/sec, feas=False, obj=-2.16]
INFO - 16:23:35: 46%|████▌ | 23/50 [00:00<00:00, 27.75 it/sec, feas=False, obj=-2.16]
INFO - 16:23:35: 48%|████▊ | 24/50 [00:00<00:00, 28.02 it/sec, feas=False, obj=-2.16]
INFO - 16:23:35: 50%|█████ | 25/50 [00:00<00:00, 27.89 it/sec, feas=False, obj=-2.16]
INFO - 16:23:35: 52%|█████▏ | 26/50 [00:00<00:00, 28.09 it/sec, feas=False, obj=-2.16]
INFO - 16:23:35: 54%|█████▍ | 27/50 [00:01<00:00, 26.56 it/sec, feas=False, obj=-2.16]
INFO - 16:23:35: 56%|█████▌ | 28/50 [00:01<00:00, 26.82 it/sec, feas=True, obj=-2.16]
INFO - 16:23:35: 58%|█████▊ | 29/50 [00:01<00:00, 27.03 it/sec, feas=True, obj=-2.16]
INFO - 16:23:35: 60%|██████ | 30/50 [00:01<00:00, 27.25 it/sec, feas=True, obj=-2.16]
INFO - 16:23:35: Optimization result:
INFO - 16:23:35: Optimizer info:
INFO - 16:23:35: Status: None
INFO - 16:23:35: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:35: Solution:
INFO - 16:23:35: The solution is feasible.
INFO - 16:23:35: Objective: -2.1558712473104222
INFO - 16:23:35: Standardized constraints:
INFO - 16:23:35: g_3 = [-7.38342309e-01 -2.61657691e-01 5.28466160e-14 -1.68273579e-01]
INFO - 16:23:35: Design space:
INFO - 16:23:35: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:35: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:35: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:35: | x_3 | 0.1 | 0.1734151094801311 | 1 | float |
INFO - 16:23:35: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:35: *** End PropulsionScenario execution (time: 0:00:01.103628) ***
INFO - 16:23:35: *** Start AerodynamicsScenario execution ***
INFO - 16:23:35: AerodynamicsScenario
INFO - 16:23:35: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:35: MDO formulation: MDF
INFO - 16:23:35: Optimization problem:
INFO - 16:23:35: minimize 0.001*-y_4(x_2)
INFO - 16:23:35: with respect to x_2
INFO - 16:23:35: under the inequality constraints
INFO - 16:23:35: g_2(x_2) <= 0
INFO - 16:23:35: over the design space:
INFO - 16:23:35: +------+-------------+-------+-------------+-------+
INFO - 16:23:35: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:35: +------+-------------+-------+-------------+-------+
INFO - 16:23:35: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:35: +------+-------------+-------+-------------+-------+
INFO - 16:23:35: Solving optimization problem with algorithm SLSQP:
WARNING - 16:23:35: Optimization found no feasible point; the least infeasible point is selected.
INFO - 16:23:35: 2%|▏ | 1/50 [00:00<00:00, 73.13 it/sec, feas=False, obj=-2.16]
INFO - 16:23:35: Optimization result:
INFO - 16:23:35: Optimizer info:
INFO - 16:23:35: Status: 8
INFO - 16:23:35: Message: Positive directional derivative for linesearch
INFO - 16:23:35: Solution:
WARNING - 16:23:35: The solution is not feasible.
INFO - 16:23:35: Objective: -2.1558712473104222
INFO - 16:23:35: Standardized constraints:
INFO - 16:23:35: g_2 = 0.005021430463882259
INFO - 16:23:35: Design space:
INFO - 16:23:35: +------+-------------+-------+-------------+-------+
INFO - 16:23:35: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:35: +------+-------------+-------+-------------+-------+
INFO - 16:23:35: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:35: +------+-------------+-------+-------------+-------+
INFO - 16:23:35: *** End AerodynamicsScenario execution (time: 0:00:00.015456) ***
INFO - 16:23:35: *** Start StructureScenario execution ***
INFO - 16:23:35: StructureScenario
INFO - 16:23:35: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:35: MDO formulation: MDF
INFO - 16:23:35: Optimization problem:
INFO - 16:23:35: minimize 0.001*-y_4(x_1)
INFO - 16:23:35: with respect to x_1
INFO - 16:23:35: under the inequality constraints
INFO - 16:23:35: g_1(x_1) <= 0
INFO - 16:23:35: over the design space:
INFO - 16:23:35: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:35: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:35: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:35: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:35: | x_1[1] | 0.75 | 0.8080816092616823 | 1.25 | float |
INFO - 16:23:35: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:35: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:35: 2%|▏ | 1/50 [00:00<00:00, 76.06 it/sec, feas=True, obj=-2.16]
INFO - 16:23:35: 4%|▍ | 2/50 [00:00<00:01, 33.61 it/sec, feas=True, obj=-2.24]
WARNING - 16:23:35: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 0.0009157477359807847 is still above the tolerance 1e-06.
INFO - 16:23:35: 6%|▌ | 3/50 [00:00<00:01, 27.56 it/sec, feas=True, obj=-2.25]
WARNING - 16:23:35: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 0.0009157477359807847 is still above the tolerance 1e-06.
INFO - 16:23:35: 8%|▊ | 4/50 [00:00<00:01, 25.61 it/sec, feas=True, obj=-2.25]
INFO - 16:23:35: 10%|█ | 5/50 [00:00<00:01, 24.69 it/sec, feas=True, obj=-2.25]
WARNING - 16:23:35: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 0.0009157477359807847 is still above the tolerance 1e-06.
INFO - 16:23:35: 12%|█▏ | 6/50 [00:00<00:01, 23.79 it/sec, feas=True, obj=-2.25]
INFO - 16:23:35: Optimization result:
INFO - 16:23:35: Optimizer info:
INFO - 16:23:35: Status: None
INFO - 16:23:35: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:35: Solution:
INFO - 16:23:35: The solution is feasible.
INFO - 16:23:35: Objective: -2.24620751123417
INFO - 16:23:35: Standardized constraints:
INFO - 16:23:35: g_1 = [-2.14272231e-02 -1.21932682e-02 -1.96106209e-02 -2.79120183e-02
INFO - 16:23:35: -3.50508605e-02 -2.40000000e-01 -1.11022302e-16]
INFO - 16:23:35: Design space:
INFO - 16:23:35: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:35: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:35: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:35: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:35: | x_1[1] | 0.75 | 0.7511952045041477 | 1.25 | float |
INFO - 16:23:35: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:35: *** End StructureScenario execution (time: 0:00:00.254989) ***
INFO - 16:23:35: *** Start PropulsionScenario execution ***
INFO - 16:23:35: PropulsionScenario
INFO - 16:23:35: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:35: MDO formulation: MDF
INFO - 16:23:35: Optimization problem:
INFO - 16:23:35: minimize 0.001*-y_4(x_3)
INFO - 16:23:35: with respect to x_3
INFO - 16:23:35: under the inequality constraints
INFO - 16:23:35: g_3(x_3) <= 0
INFO - 16:23:35: over the design space:
INFO - 16:23:35: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:35: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:35: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:35: | x_3 | 0.1 | 0.1734151094801311 | 1 | float |
INFO - 16:23:35: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:35: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:35: 2%|▏ | 1/50 [00:00<00:00, 105.21 it/sec, feas=True, obj=-2.25]
INFO - 16:23:35: Optimization result:
INFO - 16:23:35: Optimizer info:
INFO - 16:23:35: Status: 8
INFO - 16:23:35: Message: Positive directional derivative for linesearch
INFO - 16:23:35: Solution:
INFO - 16:23:35: The solution is feasible.
INFO - 16:23:35: Objective: -2.24620751123417
INFO - 16:23:35: Standardized constraints:
INFO - 16:23:35: g_3 = [-7.38561473e-01 -2.61438527e-01 5.28466160e-14 -1.68273579e-01]
INFO - 16:23:35: Design space:
INFO - 16:23:35: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:35: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:35: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:35: | x_3 | 0.1 | 0.1734151094801311 | 1 | float |
INFO - 16:23:35: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:35: *** End PropulsionScenario execution (time: 0:00:00.011596) ***
INFO - 16:23:35: *** Start AerodynamicsScenario execution ***
INFO - 16:23:35: AerodynamicsScenario
INFO - 16:23:35: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:35: MDO formulation: MDF
INFO - 16:23:35: Optimization problem:
INFO - 16:23:35: minimize 0.001*-y_4(x_2)
INFO - 16:23:35: with respect to x_2
INFO - 16:23:35: under the inequality constraints
INFO - 16:23:35: g_2(x_2) <= 0
INFO - 16:23:35: over the design space:
INFO - 16:23:35: +------+-------------+-------+-------------+-------+
INFO - 16:23:35: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:35: +------+-------------+-------+-------------+-------+
INFO - 16:23:35: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:35: +------+-------------+-------+-------------+-------+
INFO - 16:23:35: Solving optimization problem with algorithm SLSQP:
WARNING - 16:23:35: Optimization found no feasible point; the least infeasible point is selected.
INFO - 16:23:35: 2%|▏ | 1/50 [00:00<00:00, 104.70 it/sec, feas=False, obj=-2.25]
INFO - 16:23:35: Optimization result:
INFO - 16:23:35: Optimizer info:
INFO - 16:23:35: Status: 8
INFO - 16:23:35: Message: Positive directional derivative for linesearch
INFO - 16:23:35: Solution:
WARNING - 16:23:35: The solution is not feasible.
INFO - 16:23:35: Objective: -2.24620751123417
INFO - 16:23:35: Standardized constraints:
INFO - 16:23:35: g_2 = 0.005021430463882259
INFO - 16:23:35: Design space:
INFO - 16:23:35: +------+-------------+-------+-------------+-------+
INFO - 16:23:35: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:35: +------+-------------+-------+-------------+-------+
INFO - 16:23:35: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:35: +------+-------------+-------+-------------+-------+
INFO - 16:23:35: *** End AerodynamicsScenario execution (time: 0:00:00.011312) ***
INFO - 16:23:35: *** Start StructureScenario execution ***
INFO - 16:23:35: StructureScenario
INFO - 16:23:35: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:35: MDO formulation: MDF
INFO - 16:23:35: Optimization problem:
INFO - 16:23:35: minimize 0.001*-y_4(x_1)
INFO - 16:23:35: with respect to x_1
INFO - 16:23:35: under the inequality constraints
INFO - 16:23:35: g_1(x_1) <= 0
INFO - 16:23:35: over the design space:
INFO - 16:23:35: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:35: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:35: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:35: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:35: | x_1[1] | 0.75 | 0.7511952045041477 | 1.25 | float |
INFO - 16:23:35: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:35: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:35: 2%|▏ | 1/50 [00:00<00:00, 101.16 it/sec, feas=True, obj=-2.25]
INFO - 16:23:35: 4%|▍ | 2/50 [00:00<00:00, 63.23 it/sec, feas=True, obj=-2.25]
INFO - 16:23:35: 6%|▌ | 3/50 [00:00<00:00, 82.30 it/sec, feas=True, obj=-2.25]
INFO - 16:23:35: Optimization result:
INFO - 16:23:35: Optimizer info:
INFO - 16:23:35: Status: None
INFO - 16:23:35: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:35: Solution:
INFO - 16:23:35: The solution is feasible.
INFO - 16:23:35: Objective: -2.2462075112341715
INFO - 16:23:35: Standardized constraints:
INFO - 16:23:35: g_1 = [-2.14272231e-02 -1.21932682e-02 -1.96106209e-02 -2.79120183e-02
INFO - 16:23:35: -3.50508605e-02 -2.40000000e-01 1.11022302e-16]
INFO - 16:23:35: Design space:
INFO - 16:23:35: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:35: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:35: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:35: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:35: | x_1[1] | 0.75 | 0.7511952045041471 | 1.25 | float |
INFO - 16:23:35: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:35: *** End StructureScenario execution (time: 0:00:00.038858) ***
INFO - 16:23:35: 20%|██ | 20/100 [00:18<01:15, 1.05 it/sec, feas=False, obj=-2.25]
INFO - 16:23:35: *** Start PropulsionScenario execution ***
INFO - 16:23:35: PropulsionScenario
INFO - 16:23:35: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:35: MDO formulation: MDF
INFO - 16:23:35: Optimization problem:
INFO - 16:23:35: minimize 0.001*-y_4(x_3)
INFO - 16:23:35: with respect to x_3
INFO - 16:23:35: under the inequality constraints
INFO - 16:23:35: g_3(x_3) <= 0
INFO - 16:23:35: over the design space:
INFO - 16:23:35: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:35: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:35: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:35: | x_3 | 0.1 | 0.1734151094801311 | 1 | float |
INFO - 16:23:35: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:35: Solving optimization problem with algorithm SLSQP:
WARNING - 16:23:35: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 0.00026899729866434503 is still above the tolerance 1e-06.
INFO - 16:23:35: 2%|▏ | 1/50 [00:00<00:01, 33.50 it/sec, feas=True, obj=-1.75]
WARNING - 16:23:35: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 0.0005379945973286901 is still above the tolerance 1e-06.
INFO - 16:23:35: 4%|▍ | 2/50 [00:00<00:01, 25.95 it/sec, feas=True, obj=-1.81]
WARNING - 16:23:36: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 0.0006052439219947763 is still above the tolerance 1e-06.
INFO - 16:23:36: 6%|▌ | 3/50 [00:00<00:01, 24.13 it/sec, feas=True, obj=-1.81]
WARNING - 16:23:36: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 0.0005379945973286901 is still above the tolerance 1e-06.
INFO - 16:23:36: 8%|▊ | 4/50 [00:00<00:01, 25.67 it/sec, feas=True, obj=-1.81]
INFO - 16:23:36: Optimization result:
INFO - 16:23:36: Optimizer info:
INFO - 16:23:36: Status: None
INFO - 16:23:36: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:36: Solution:
INFO - 16:23:36: The solution is feasible.
INFO - 16:23:36: Objective: -1.8076914810709601
INFO - 16:23:36: Standardized constraints:
INFO - 16:23:36: g_3 = [-6.98257119e-01 -3.01742881e-01 -1.11022302e-16 -1.55194346e-01]
INFO - 16:23:36: Design space:
INFO - 16:23:36: +------+-------------+-------------------+-------------+-------+
INFO - 16:23:36: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:36: +------+-------------+-------------------+-------------+-------+
INFO - 16:23:36: | x_3 | 0.1 | 0.190188145273489 | 1 | float |
INFO - 16:23:36: +------+-------------+-------------------+-------------+-------+
INFO - 16:23:36: *** End PropulsionScenario execution (time: 0:00:00.158060) ***
INFO - 16:23:36: *** Start AerodynamicsScenario execution ***
INFO - 16:23:36: AerodynamicsScenario
INFO - 16:23:36: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:36: MDO formulation: MDF
INFO - 16:23:36: Optimization problem:
INFO - 16:23:36: minimize 0.001*-y_4(x_2)
INFO - 16:23:36: with respect to x_2
INFO - 16:23:36: under the inequality constraints
INFO - 16:23:36: g_2(x_2) <= 0
INFO - 16:23:36: over the design space:
INFO - 16:23:36: +------+-------------+-------+-------------+-------+
INFO - 16:23:36: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:36: +------+-------------+-------+-------------+-------+
INFO - 16:23:36: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:36: +------+-------------+-------+-------------+-------+
INFO - 16:23:36: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:36: 2%|▏ | 1/50 [00:00<00:00, 77.82 it/sec, feas=True, obj=-1.81]
INFO - 16:23:36: Optimization result:
INFO - 16:23:36: Optimizer info:
INFO - 16:23:36: Status: 8
INFO - 16:23:36: Message: Positive directional derivative for linesearch
INFO - 16:23:36: Solution:
INFO - 16:23:36: The solution is feasible.
INFO - 16:23:36: Objective: -1.8076914810709601
INFO - 16:23:36: Standardized constraints:
INFO - 16:23:36: g_2 = -0.005118161063181859
INFO - 16:23:36: Design space:
INFO - 16:23:36: +------+-------------+-------+-------------+-------+
INFO - 16:23:36: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:36: +------+-------------+-------+-------------+-------+
INFO - 16:23:36: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:36: +------+-------------+-------+-------------+-------+
INFO - 16:23:36: *** End AerodynamicsScenario execution (time: 0:00:00.014415) ***
INFO - 16:23:36: *** Start StructureScenario execution ***
INFO - 16:23:36: StructureScenario
INFO - 16:23:36: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:36: MDO formulation: MDF
INFO - 16:23:36: Optimization problem:
INFO - 16:23:36: minimize 0.001*-y_4(x_1)
INFO - 16:23:36: with respect to x_1
INFO - 16:23:36: under the inequality constraints
INFO - 16:23:36: g_1(x_1) <= 0
INFO - 16:23:36: over the design space:
INFO - 16:23:36: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:36: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:36: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:36: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:36: | x_1[1] | 0.75 | 0.7511952045041471 | 1.25 | float |
INFO - 16:23:36: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:36: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:36: 2%|▏ | 1/50 [00:00<00:00, 96.97 it/sec, feas=False, obj=-1.81]
INFO - 16:23:36: 4%|▍ | 2/50 [00:00<00:01, 39.00 it/sec, feas=True, obj=-1.71]
INFO - 16:23:36: 6%|▌ | 3/50 [00:00<00:01, 32.96 it/sec, feas=True, obj=-1.72]
INFO - 16:23:36: 8%|▊ | 4/50 [00:00<00:01, 30.25 it/sec, feas=True, obj=-1.72]
INFO - 16:23:36: 10%|█ | 5/50 [00:00<00:01, 28.62 it/sec, feas=True, obj=-1.72]
INFO - 16:23:36: 12%|█▏ | 6/50 [00:00<00:01, 30.10 it/sec, feas=True, obj=-1.72]
INFO - 16:23:36: 14%|█▍ | 7/50 [00:00<00:01, 31.06 it/sec, feas=True, obj=-1.72]
INFO - 16:23:36: Optimization result:
INFO - 16:23:36: Optimizer info:
INFO - 16:23:36: Status: None
INFO - 16:23:36: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:36: Solution:
INFO - 16:23:36: The solution is feasible.
INFO - 16:23:36: Objective: -1.7190120099062236
INFO - 16:23:36: Standardized constraints:
INFO - 16:23:36: g_1 = [ 6.52811138e-14 -4.69095511e-03 -1.65273245e-02 -2.66662315e-02
INFO - 16:23:36: -3.46909551e-02 -2.25164458e-01 -1.48355421e-02]
INFO - 16:23:36: Design space:
INFO - 16:23:36: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:36: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:36: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:36: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:36: | x_1[1] | 0.75 | 0.8264638086878571 | 1.25 | float |
INFO - 16:23:36: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:36: *** End StructureScenario execution (time: 0:00:00.227813) ***
INFO - 16:23:36: *** Start PropulsionScenario execution ***
INFO - 16:23:36: PropulsionScenario
INFO - 16:23:36: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:36: MDO formulation: MDF
INFO - 16:23:36: Optimization problem:
INFO - 16:23:36: minimize 0.001*-y_4(x_3)
INFO - 16:23:36: with respect to x_3
INFO - 16:23:36: under the inequality constraints
INFO - 16:23:36: g_3(x_3) <= 0
INFO - 16:23:36: over the design space:
INFO - 16:23:36: +------+-------------+-------------------+-------------+-------+
INFO - 16:23:36: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:36: +------+-------------+-------------------+-------------+-------+
INFO - 16:23:36: | x_3 | 0.1 | 0.190188145273489 | 1 | float |
INFO - 16:23:36: +------+-------------+-------------------+-------------+-------+
INFO - 16:23:36: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:36: 2%|▏ | 1/50 [00:00<00:00, 77.39 it/sec, feas=True, obj=-1.72]
INFO - 16:23:36: Optimization result:
INFO - 16:23:36: Optimizer info:
INFO - 16:23:36: Status: 8
INFO - 16:23:36: Message: Positive directional derivative for linesearch
INFO - 16:23:36: Solution:
INFO - 16:23:36: The solution is feasible.
INFO - 16:23:36: Objective: -1.719012009906224
INFO - 16:23:36: Standardized constraints:
INFO - 16:23:36: g_3 = [-0.69792227 -0.30207773 0. -0.15519435]
INFO - 16:23:36: Design space:
INFO - 16:23:36: +------+-------------+-------------------+-------------+-------+
INFO - 16:23:36: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:36: +------+-------------+-------------------+-------------+-------+
INFO - 16:23:36: | x_3 | 0.1 | 0.190188145273489 | 1 | float |
INFO - 16:23:36: +------+-------------+-------------------+-------------+-------+
INFO - 16:23:36: *** End PropulsionScenario execution (time: 0:00:00.014961) ***
INFO - 16:23:36: *** Start AerodynamicsScenario execution ***
INFO - 16:23:36: AerodynamicsScenario
INFO - 16:23:36: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:36: MDO formulation: MDF
INFO - 16:23:36: Optimization problem:
INFO - 16:23:36: minimize 0.001*-y_4(x_2)
INFO - 16:23:36: with respect to x_2
INFO - 16:23:36: under the inequality constraints
INFO - 16:23:36: g_2(x_2) <= 0
INFO - 16:23:36: over the design space:
INFO - 16:23:36: +------+-------------+-------+-------------+-------+
INFO - 16:23:36: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:36: +------+-------------+-------+-------------+-------+
INFO - 16:23:36: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:36: +------+-------------+-------+-------------+-------+
INFO - 16:23:36: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:36: 2%|▏ | 1/50 [00:00<00:00, 107.99 it/sec, feas=True, obj=-1.72]
INFO - 16:23:36: Optimization result:
INFO - 16:23:36: Optimizer info:
INFO - 16:23:36: Status: 8
INFO - 16:23:36: Message: Positive directional derivative for linesearch
INFO - 16:23:36: Solution:
INFO - 16:23:36: The solution is feasible.
INFO - 16:23:36: Objective: -1.719012009906224
INFO - 16:23:36: Standardized constraints:
INFO - 16:23:36: g_2 = -0.005118161063181859
INFO - 16:23:36: Design space:
INFO - 16:23:36: +------+-------------+-------+-------------+-------+
INFO - 16:23:36: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:36: +------+-------------+-------+-------------+-------+
INFO - 16:23:36: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:36: +------+-------------+-------+-------------+-------+
INFO - 16:23:36: *** End AerodynamicsScenario execution (time: 0:00:00.010987) ***
INFO - 16:23:36: *** Start StructureScenario execution ***
INFO - 16:23:36: StructureScenario
INFO - 16:23:36: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:36: MDO formulation: MDF
INFO - 16:23:36: Optimization problem:
INFO - 16:23:36: minimize 0.001*-y_4(x_1)
INFO - 16:23:36: with respect to x_1
INFO - 16:23:36: under the inequality constraints
INFO - 16:23:36: g_1(x_1) <= 0
INFO - 16:23:36: over the design space:
INFO - 16:23:36: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:36: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:36: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:36: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:36: | x_1[1] | 0.75 | 0.8264638086878571 | 1.25 | float |
INFO - 16:23:36: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:36: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:36: 2%|▏ | 1/50 [00:00<00:00, 101.70 it/sec, feas=True, obj=-1.72]
INFO - 16:23:36: Optimization result:
INFO - 16:23:36: Optimizer info:
INFO - 16:23:36: Status: 8
INFO - 16:23:36: Message: Positive directional derivative for linesearch
INFO - 16:23:36: Solution:
INFO - 16:23:36: The solution is feasible.
INFO - 16:23:36: Objective: -1.719012009906224
INFO - 16:23:36: Standardized constraints:
INFO - 16:23:36: g_1 = [ 6.52811138e-14 -4.69095511e-03 -1.65273245e-02 -2.66662315e-02
INFO - 16:23:36: -3.46909551e-02 -2.25164458e-01 -1.48355421e-02]
INFO - 16:23:36: Design space:
INFO - 16:23:36: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:36: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:36: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:36: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:36: | x_1[1] | 0.75 | 0.8264638086878571 | 1.25 | float |
INFO - 16:23:36: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:36: *** End StructureScenario execution (time: 0:00:00.011912) ***
INFO - 16:23:36: 21%|██ | 21/100 [00:19<01:13, 1.08 it/sec, feas=True, obj=-1.72]
INFO - 16:23:36: *** Start PropulsionScenario execution ***
INFO - 16:23:36: PropulsionScenario
INFO - 16:23:36: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:36: MDO formulation: MDF
INFO - 16:23:36: Optimization problem:
INFO - 16:23:36: minimize 0.001*-y_4(x_3)
INFO - 16:23:36: with respect to x_3
INFO - 16:23:36: under the inequality constraints
INFO - 16:23:36: g_3(x_3) <= 0
INFO - 16:23:36: over the design space:
INFO - 16:23:36: +------+-------------+-------------------+-------------+-------+
INFO - 16:23:36: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:36: +------+-------------+-------------------+-------------+-------+
INFO - 16:23:36: | x_3 | 0.1 | 0.190188145273489 | 1 | float |
INFO - 16:23:36: +------+-------------+-------------------+-------------+-------+
INFO - 16:23:36: Solving optimization problem with algorithm SLSQP:
WARNING - 16:23:36: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 6.724932466608626e-05 is still above the tolerance 1e-06.
INFO - 16:23:36: 2%|▏ | 1/50 [00:00<00:01, 32.84 it/sec, feas=False, obj=-2.02]
INFO - 16:23:36: 4%|▍ | 2/50 [00:00<00:01, 39.28 it/sec, feas=True, obj=-1.99]
INFO - 16:23:36: 6%|▌ | 3/50 [00:00<00:01, 34.39 it/sec, feas=False, obj=-2.02]
INFO - 16:23:36: 8%|▊ | 4/50 [00:00<00:01, 32.01 it/sec, feas=True, obj=-1.99]
INFO - 16:23:36: 10%|█ | 5/50 [00:00<00:01, 31.01 it/sec, feas=True, obj=-1.99]
INFO - 16:23:36: 12%|█▏ | 6/50 [00:00<00:01, 30.26 it/sec, feas=True, obj=-1.99]
INFO - 16:23:36: Optimization result:
INFO - 16:23:36: Optimizer info:
INFO - 16:23:36: Status: None
INFO - 16:23:36: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:36: Solution:
INFO - 16:23:36: The solution is feasible.
INFO - 16:23:36: Objective: -1.9929129782359707
INFO - 16:23:36: Standardized constraints:
INFO - 16:23:36: g_3 = [-7.71436602e-01 -2.28563398e-01 3.55271368e-15 -1.69666795e-01]
INFO - 16:23:36: Design space:
INFO - 16:23:36: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:36: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:36: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:36: | x_3 | 0.1 | 0.1717165375293956 | 1 | float |
INFO - 16:23:36: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:36: *** End PropulsionScenario execution (time: 0:00:00.200838) ***
INFO - 16:23:36: *** Start AerodynamicsScenario execution ***
INFO - 16:23:36: AerodynamicsScenario
INFO - 16:23:36: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:36: MDO formulation: MDF
INFO - 16:23:36: Optimization problem:
INFO - 16:23:36: minimize 0.001*-y_4(x_2)
INFO - 16:23:36: with respect to x_2
INFO - 16:23:36: under the inequality constraints
INFO - 16:23:36: g_2(x_2) <= 0
INFO - 16:23:36: over the design space:
INFO - 16:23:36: +------+-------------+-------+-------------+-------+
INFO - 16:23:36: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:36: +------+-------------+-------+-------------+-------+
INFO - 16:23:36: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:36: +------+-------------+-------+-------------+-------+
INFO - 16:23:36: Solving optimization problem with algorithm SLSQP:
WARNING - 16:23:36: Optimization found no feasible point; the least infeasible point is selected.
INFO - 16:23:36: 2%|▏ | 1/50 [00:00<00:00, 102.29 it/sec, feas=False, obj=-1.99]
INFO - 16:23:36: Optimization result:
INFO - 16:23:36: Optimizer info:
INFO - 16:23:36: Status: 8
INFO - 16:23:36: Message: Positive directional derivative for linesearch
INFO - 16:23:36: Solution:
WARNING - 16:23:36: The solution is not feasible.
INFO - 16:23:36: Objective: -1.9929129782359707
INFO - 16:23:36: Standardized constraints:
INFO - 16:23:36: g_2 = 0.0020301145386960595
INFO - 16:23:36: Design space:
INFO - 16:23:36: +------+-------------+-------+-------------+-------+
INFO - 16:23:36: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:36: +------+-------------+-------+-------------+-------+
INFO - 16:23:36: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:36: +------+-------------+-------+-------------+-------+
INFO - 16:23:36: *** End AerodynamicsScenario execution (time: 0:00:00.013676) ***
INFO - 16:23:36: *** Start StructureScenario execution ***
INFO - 16:23:36: StructureScenario
INFO - 16:23:36: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:36: MDO formulation: MDF
INFO - 16:23:36: Optimization problem:
INFO - 16:23:36: minimize 0.001*-y_4(x_1)
INFO - 16:23:36: with respect to x_1
INFO - 16:23:36: under the inequality constraints
INFO - 16:23:36: g_1(x_1) <= 0
INFO - 16:23:36: over the design space:
INFO - 16:23:36: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:36: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:36: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:36: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:36: | x_1[1] | 0.75 | 0.8264638086878571 | 1.25 | float |
INFO - 16:23:36: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:36: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:36: 2%|▏ | 1/50 [00:00<00:00, 95.31 it/sec, feas=True, obj=-1.99]
INFO - 16:23:36: 4%|▍ | 2/50 [00:00<00:01, 37.21 it/sec, feas=True, obj=-2.05]
INFO - 16:23:36: 6%|▌ | 3/50 [00:00<00:01, 30.84 it/sec, feas=True, obj=-2.05]
INFO - 16:23:36: 8%|▊ | 4/50 [00:00<00:01, 28.63 it/sec, feas=True, obj=-2.05]
WARNING - 16:23:36: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 0.0009157477359807847 is still above the tolerance 1e-06.
INFO - 16:23:36: 10%|█ | 5/50 [00:00<00:01, 26.52 it/sec, feas=True, obj=-2.05]
INFO - 16:23:36: 12%|█▏ | 6/50 [00:00<00:01, 27.97 it/sec, feas=True, obj=-2.05]
INFO - 16:23:36: Optimization result:
INFO - 16:23:36: Optimizer info:
INFO - 16:23:36: Status: None
INFO - 16:23:36: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:36: Solution:
INFO - 16:23:36: The solution is feasible.
INFO - 16:23:36: Objective: -2.0527073350764615
INFO - 16:23:36: Standardized constraints:
INFO - 16:23:36: g_1 = [-1.79937220e-02 -1.10083737e-02 -1.91359899e-02 -2.77310526e-02
INFO - 16:23:36: -3.50104664e-02 -2.40000000e-01 1.64314118e-11]
INFO - 16:23:36: Design space:
INFO - 16:23:36: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:36: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:36: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:36: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:36: | x_1[1] | 0.75 | 0.7806436836242986 | 1.25 | float |
INFO - 16:23:36: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:36: *** End StructureScenario execution (time: 0:00:00.218575) ***
INFO - 16:23:36: *** Start PropulsionScenario execution ***
INFO - 16:23:36: PropulsionScenario
INFO - 16:23:36: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:36: MDO formulation: MDF
INFO - 16:23:36: Optimization problem:
INFO - 16:23:36: minimize 0.001*-y_4(x_3)
INFO - 16:23:36: with respect to x_3
INFO - 16:23:36: under the inequality constraints
INFO - 16:23:36: g_3(x_3) <= 0
INFO - 16:23:36: over the design space:
INFO - 16:23:36: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:36: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:36: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:36: | x_3 | 0.1 | 0.1717165375293956 | 1 | float |
INFO - 16:23:36: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:36: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:36: 2%|▏ | 1/50 [00:00<00:00, 74.38 it/sec, feas=True, obj=-2.05]
INFO - 16:23:36: Optimization result:
INFO - 16:23:36: Optimizer info:
INFO - 16:23:36: Status: 8
INFO - 16:23:36: Message: Positive directional derivative for linesearch
INFO - 16:23:36: Solution:
INFO - 16:23:36: The solution is feasible.
INFO - 16:23:36: Objective: -2.0527073350764615
INFO - 16:23:36: Standardized constraints:
INFO - 16:23:36: g_3 = [-7.71634020e-01 -2.28365980e-01 3.55271368e-15 -1.69666795e-01]
INFO - 16:23:36: Design space:
INFO - 16:23:36: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:36: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:36: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:36: | x_3 | 0.1 | 0.1717165375293956 | 1 | float |
INFO - 16:23:36: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:36: *** End PropulsionScenario execution (time: 0:00:00.015500) ***
INFO - 16:23:36: *** Start AerodynamicsScenario execution ***
INFO - 16:23:36: AerodynamicsScenario
INFO - 16:23:36: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:36: MDO formulation: MDF
INFO - 16:23:36: Optimization problem:
INFO - 16:23:36: minimize 0.001*-y_4(x_2)
INFO - 16:23:36: with respect to x_2
INFO - 16:23:36: under the inequality constraints
INFO - 16:23:36: g_2(x_2) <= 0
INFO - 16:23:36: over the design space:
INFO - 16:23:36: +------+-------------+-------+-------------+-------+
INFO - 16:23:36: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:36: +------+-------------+-------+-------------+-------+
INFO - 16:23:36: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:36: +------+-------------+-------+-------------+-------+
INFO - 16:23:36: Solving optimization problem with algorithm SLSQP:
WARNING - 16:23:36: Optimization found no feasible point; the least infeasible point is selected.
INFO - 16:23:36: 2%|▏ | 1/50 [00:00<00:00, 103.43 it/sec, feas=False, obj=-2.05]
INFO - 16:23:36: Optimization result:
INFO - 16:23:36: Optimizer info:
INFO - 16:23:36: Status: 8
INFO - 16:23:36: Message: Positive directional derivative for linesearch
INFO - 16:23:36: Solution:
WARNING - 16:23:36: The solution is not feasible.
INFO - 16:23:36: Objective: -2.0527073350764615
INFO - 16:23:36: Standardized constraints:
INFO - 16:23:36: g_2 = 0.0020301145386960595
INFO - 16:23:36: Design space:
INFO - 16:23:36: +------+-------------+-------+-------------+-------+
INFO - 16:23:36: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:36: +------+-------------+-------+-------------+-------+
INFO - 16:23:36: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:36: +------+-------------+-------+-------------+-------+
INFO - 16:23:36: *** End AerodynamicsScenario execution (time: 0:00:00.011299) ***
INFO - 16:23:36: *** Start StructureScenario execution ***
INFO - 16:23:36: StructureScenario
INFO - 16:23:36: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:36: MDO formulation: MDF
INFO - 16:23:36: Optimization problem:
INFO - 16:23:36: minimize 0.001*-y_4(x_1)
INFO - 16:23:36: with respect to x_1
INFO - 16:23:36: under the inequality constraints
INFO - 16:23:36: g_1(x_1) <= 0
INFO - 16:23:36: over the design space:
INFO - 16:23:36: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:36: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:36: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:36: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:36: | x_1[1] | 0.75 | 0.7806436836242986 | 1.25 | float |
INFO - 16:23:36: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:36: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:36: 2%|▏ | 1/50 [00:00<00:00, 98.23 it/sec, feas=True, obj=-2.05]
INFO - 16:23:36: Optimization result:
INFO - 16:23:36: Optimizer info:
INFO - 16:23:36: Status: 8
INFO - 16:23:36: Message: Positive directional derivative for linesearch
INFO - 16:23:36: Solution:
INFO - 16:23:36: The solution is feasible.
INFO - 16:23:36: Objective: -2.0527073350764615
INFO - 16:23:36: Standardized constraints:
INFO - 16:23:36: g_1 = [-1.79937220e-02 -1.10083737e-02 -1.91359899e-02 -2.77310526e-02
INFO - 16:23:36: -3.50104664e-02 -2.40000000e-01 1.64314118e-11]
INFO - 16:23:36: Design space:
INFO - 16:23:36: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:36: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:36: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:36: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:36: | x_1[1] | 0.75 | 0.7806436836242986 | 1.25 | float |
INFO - 16:23:36: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:36: *** End StructureScenario execution (time: 0:00:00.012277) ***
INFO - 16:23:36: 22%|██▏ | 22/100 [00:20<01:10, 1.10 it/sec, feas=False, obj=-2.05]
INFO - 16:23:36: *** Start PropulsionScenario execution ***
INFO - 16:23:36: PropulsionScenario
INFO - 16:23:36: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:36: MDO formulation: MDF
INFO - 16:23:36: Optimization problem:
INFO - 16:23:36: minimize 0.001*-y_4(x_3)
INFO - 16:23:36: with respect to x_3
INFO - 16:23:36: under the inequality constraints
INFO - 16:23:36: g_3(x_3) <= 0
INFO - 16:23:36: over the design space:
INFO - 16:23:36: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:36: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:36: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:36: | x_3 | 0.1 | 0.1717165375293956 | 1 | float |
INFO - 16:23:36: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:36: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:36: 2%|▏ | 1/50 [00:00<00:01, 36.34 it/sec, feas=False, obj=-2.33]
INFO - 16:23:36: 4%|▍ | 2/50 [00:00<00:01, 35.36 it/sec, feas=True, obj=-2.3]
INFO - 16:23:37: 6%|▌ | 3/50 [00:00<00:01, 29.37 it/sec, feas=False, obj=-2.33]
INFO - 16:23:37: 8%|▊ | 4/50 [00:00<00:01, 27.23 it/sec, feas=True, obj=-2.3]
INFO - 16:23:37: 10%|█ | 5/50 [00:00<00:01, 28.45 it/sec, feas=True, obj=-2.3]
INFO - 16:23:37: 12%|█▏ | 6/50 [00:00<00:01, 29.42 it/sec, feas=True, obj=-2.3]
INFO - 16:23:37: Optimization result:
INFO - 16:23:37: Optimizer info:
INFO - 16:23:37: Status: None
INFO - 16:23:37: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:37: Solution:
INFO - 16:23:37: The solution is feasible.
INFO - 16:23:37: Objective: -2.303366404064033
INFO - 16:23:37: Standardized constraints:
INFO - 16:23:37: g_3 = [-8.39424638e-01 -1.60575362e-01 1.99840144e-15 -1.82545292e-01]
INFO - 16:23:37: Design space:
INFO - 16:23:37: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:37: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:37: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:37: | x_3 | 0.1 | 0.1569976400427053 | 1 | float |
INFO - 16:23:37: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:37: *** End PropulsionScenario execution (time: 0:00:00.206861) ***
INFO - 16:23:37: *** Start AerodynamicsScenario execution ***
INFO - 16:23:37: AerodynamicsScenario
INFO - 16:23:37: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:37: MDO formulation: MDF
INFO - 16:23:37: Optimization problem:
INFO - 16:23:37: minimize 0.001*-y_4(x_2)
INFO - 16:23:37: with respect to x_2
INFO - 16:23:37: under the inequality constraints
INFO - 16:23:37: g_2(x_2) <= 0
INFO - 16:23:37: over the design space:
INFO - 16:23:37: +------+-------------+-------+-------------+-------+
INFO - 16:23:37: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:37: +------+-------------+-------+-------------+-------+
INFO - 16:23:37: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:37: +------+-------------+-------+-------------+-------+
INFO - 16:23:37: Solving optimization problem with algorithm SLSQP:
WARNING - 16:23:37: Optimization found no feasible point; the least infeasible point is selected.
INFO - 16:23:37: 2%|▏ | 1/50 [00:00<00:00, 71.17 it/sec, feas=False, obj=-2.3]
INFO - 16:23:37: Optimization result:
INFO - 16:23:37: Optimizer info:
INFO - 16:23:37: Status: 8
INFO - 16:23:37: Message: Positive directional derivative for linesearch
INFO - 16:23:37: Solution:
WARNING - 16:23:37: The solution is not feasible.
INFO - 16:23:37: Objective: -2.3033664040640334
INFO - 16:23:37: Standardized constraints:
INFO - 16:23:37: g_2 = 0.005052585125312259
INFO - 16:23:37: Design space:
INFO - 16:23:37: +------+-------------+-------+-------------+-------+
INFO - 16:23:37: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:37: +------+-------------+-------+-------------+-------+
INFO - 16:23:37: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:37: +------+-------------+-------+-------------+-------+
INFO - 16:23:37: *** End AerodynamicsScenario execution (time: 0:00:00.015834) ***
INFO - 16:23:37: *** Start StructureScenario execution ***
INFO - 16:23:37: StructureScenario
INFO - 16:23:37: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:37: MDO formulation: MDF
INFO - 16:23:37: Optimization problem:
INFO - 16:23:37: minimize 0.001*-y_4(x_1)
INFO - 16:23:37: with respect to x_1
INFO - 16:23:37: under the inequality constraints
INFO - 16:23:37: g_1(x_1) <= 0
INFO - 16:23:37: over the design space:
INFO - 16:23:37: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:37: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:37: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:37: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:37: | x_1[1] | 0.75 | 0.7806436836242986 | 1.25 | float |
INFO - 16:23:37: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:37: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:37: 2%|▏ | 1/50 [00:00<00:00, 76.38 it/sec, feas=True, obj=-2.3]
INFO - 16:23:37: Optimization result:
INFO - 16:23:37: Optimizer info:
INFO - 16:23:37: Status: 8
INFO - 16:23:37: Message: Positive directional derivative for linesearch
INFO - 16:23:37: Solution:
INFO - 16:23:37: The solution is feasible.
INFO - 16:23:37: Objective: -2.303366404064033
INFO - 16:23:37: Standardized constraints:
INFO - 16:23:37: g_1 = [-4.28843247e-02 -2.45895893e-02 -2.81922068e-02 -3.44337725e-02
INFO - 16:23:37: -4.02948144e-02 -2.40000000e-01 1.64314118e-11]
INFO - 16:23:37: Design space:
INFO - 16:23:37: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:37: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:37: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:37: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:37: | x_1[1] | 0.75 | 0.7806436836242986 | 1.25 | float |
INFO - 16:23:37: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:37: *** End StructureScenario execution (time: 0:00:00.015482) ***
INFO - 16:23:37: *** Start PropulsionScenario execution ***
INFO - 16:23:37: PropulsionScenario
INFO - 16:23:37: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:37: MDO formulation: MDF
INFO - 16:23:37: Optimization problem:
INFO - 16:23:37: minimize 0.001*-y_4(x_3)
INFO - 16:23:37: with respect to x_3
INFO - 16:23:37: under the inequality constraints
INFO - 16:23:37: g_3(x_3) <= 0
INFO - 16:23:37: over the design space:
INFO - 16:23:37: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:37: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:37: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:37: | x_3 | 0.1 | 0.1569976400427053 | 1 | float |
INFO - 16:23:37: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:37: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:37: 2%|▏ | 1/50 [00:00<00:00, 102.95 it/sec, feas=True, obj=-2.3]
INFO - 16:23:37: 4%|▍ | 2/50 [00:00<00:00, 146.39 it/sec, feas=True, obj=-2.3]
INFO - 16:23:37: 6%|▌ | 3/50 [00:00<00:00, 85.42 it/sec, feas=True, obj=-2.3]
INFO - 16:23:37: Optimization result:
INFO - 16:23:37: Optimizer info:
INFO - 16:23:37: Status: None
INFO - 16:23:37: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:37: Solution:
INFO - 16:23:37: The solution is feasible.
INFO - 16:23:37: Objective: -2.3033664040640334
INFO - 16:23:37: Standardized constraints:
INFO - 16:23:37: g_3 = [-8.39424638e-01 -1.60575362e-01 1.33226763e-15 -1.82545292e-01]
INFO - 16:23:37: Design space:
INFO - 16:23:37: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:37: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:37: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:37: | x_3 | 0.1 | 0.1569976400427052 | 1 | float |
INFO - 16:23:37: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:37: *** End PropulsionScenario execution (time: 0:00:00.037875) ***
INFO - 16:23:37: *** Start AerodynamicsScenario execution ***
INFO - 16:23:37: AerodynamicsScenario
INFO - 16:23:37: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:37: MDO formulation: MDF
INFO - 16:23:37: Optimization problem:
INFO - 16:23:37: minimize 0.001*-y_4(x_2)
INFO - 16:23:37: with respect to x_2
INFO - 16:23:37: under the inequality constraints
INFO - 16:23:37: g_2(x_2) <= 0
INFO - 16:23:37: over the design space:
INFO - 16:23:37: +------+-------------+-------+-------------+-------+
INFO - 16:23:37: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:37: +------+-------------+-------+-------------+-------+
INFO - 16:23:37: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:37: +------+-------------+-------+-------------+-------+
INFO - 16:23:37: Solving optimization problem with algorithm SLSQP:
WARNING - 16:23:37: Optimization found no feasible point; the least infeasible point is selected.
INFO - 16:23:37: 2%|▏ | 1/50 [00:00<00:00, 101.59 it/sec, feas=False, obj=-2.3]
INFO - 16:23:37: Optimization result:
INFO - 16:23:37: Optimizer info:
INFO - 16:23:37: Status: 8
INFO - 16:23:37: Message: Positive directional derivative for linesearch
INFO - 16:23:37: Solution:
WARNING - 16:23:37: The solution is not feasible.
INFO - 16:23:37: Objective: -2.3033664040640334
INFO - 16:23:37: Standardized constraints:
INFO - 16:23:37: g_2 = 0.005052585125312259
INFO - 16:23:37: Design space:
INFO - 16:23:37: +------+-------------+-------+-------------+-------+
INFO - 16:23:37: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:37: +------+-------------+-------+-------------+-------+
INFO - 16:23:37: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:37: +------+-------------+-------+-------------+-------+
INFO - 16:23:37: *** End AerodynamicsScenario execution (time: 0:00:00.011616) ***
INFO - 16:23:37: *** Start StructureScenario execution ***
INFO - 16:23:37: StructureScenario
INFO - 16:23:37: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:37: MDO formulation: MDF
INFO - 16:23:37: Optimization problem:
INFO - 16:23:37: minimize 0.001*-y_4(x_1)
INFO - 16:23:37: with respect to x_1
INFO - 16:23:37: under the inequality constraints
INFO - 16:23:37: g_1(x_1) <= 0
INFO - 16:23:37: over the design space:
INFO - 16:23:37: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:37: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:37: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:37: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:37: | x_1[1] | 0.75 | 0.7806436836242986 | 1.25 | float |
INFO - 16:23:37: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:37: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:37: 2%|▏ | 1/50 [00:00<00:00, 97.00 it/sec, feas=True, obj=-2.3]
INFO - 16:23:37: 4%|▍ | 2/50 [00:00<00:00, 98.77 it/sec, feas=True, obj=-2.3]
INFO - 16:23:37: 6%|▌ | 3/50 [00:00<00:00, 100.16 it/sec, feas=True, obj=-2.3]
INFO - 16:23:37: Optimization result:
INFO - 16:23:37: Optimizer info:
INFO - 16:23:37: Status: None
INFO - 16:23:37: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:37: Solution:
INFO - 16:23:37: The solution is feasible.
INFO - 16:23:37: Objective: -2.3033664040640334
INFO - 16:23:37: Standardized constraints:
INFO - 16:23:37: g_1 = [-4.28843247e-02 -2.45895893e-02 -2.81922068e-02 -3.44337725e-02
INFO - 16:23:37: -4.02948144e-02 -2.40000000e-01 1.64314118e-11]
INFO - 16:23:37: Design space:
INFO - 16:23:37: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:37: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:37: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:37: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:37: | x_1[1] | 0.75 | 0.7806436836242986 | 1.25 | float |
INFO - 16:23:37: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:37: *** End StructureScenario execution (time: 0:00:00.032710) ***
INFO - 16:23:37: 23%|██▎ | 23/100 [00:20<01:08, 1.13 it/sec, feas=False, obj=-2.3]
INFO - 16:23:37: *** Start PropulsionScenario execution ***
INFO - 16:23:37: PropulsionScenario
INFO - 16:23:37: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:37: MDO formulation: MDF
INFO - 16:23:37: Optimization problem:
INFO - 16:23:37: minimize 0.001*-y_4(x_3)
INFO - 16:23:37: with respect to x_3
INFO - 16:23:37: under the inequality constraints
INFO - 16:23:37: g_3(x_3) <= 0
INFO - 16:23:37: over the design space:
INFO - 16:23:37: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:37: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:37: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:37: | x_3 | 0.1 | 0.1569976400427052 | 1 | float |
INFO - 16:23:37: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:37: Solving optimization problem with algorithm SLSQP:
WARNING - 16:23:37: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 6.724932466608626e-05 is still above the tolerance 1e-06.
INFO - 16:23:37: 2%|▏ | 1/50 [00:00<00:01, 31.74 it/sec, feas=True, obj=-1.84]
INFO - 16:23:37: 4%|▍ | 2/50 [00:00<00:01, 25.42 it/sec, feas=True, obj=-1.89]
INFO - 16:23:37: 6%|▌ | 3/50 [00:00<00:01, 24.29 it/sec, feas=True, obj=-1.89]
INFO - 16:23:37: Optimization result:
INFO - 16:23:37: Optimizer info:
INFO - 16:23:37: Status: 8
INFO - 16:23:37: Message: Positive directional derivative for linesearch
INFO - 16:23:37: Solution:
INFO - 16:23:37: The solution is feasible.
INFO - 16:23:37: Objective: -1.8903954110973304
INFO - 16:23:37: Standardized constraints:
INFO - 16:23:37: g_3 = [-7.15980250e-01 -2.84019750e-01 4.99600361e-14 -1.69666795e-01]
INFO - 16:23:37: Design space:
INFO - 16:23:37: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:37: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:37: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:37: | x_3 | 0.1 | 0.1717165375294035 | 1 | float |
INFO - 16:23:37: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:37: *** End PropulsionScenario execution (time: 0:00:00.125877) ***
INFO - 16:23:37: *** Start AerodynamicsScenario execution ***
INFO - 16:23:37: AerodynamicsScenario
INFO - 16:23:37: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:37: MDO formulation: MDF
INFO - 16:23:37: Optimization problem:
INFO - 16:23:37: minimize 0.001*-y_4(x_2)
INFO - 16:23:37: with respect to x_2
INFO - 16:23:37: under the inequality constraints
INFO - 16:23:37: g_2(x_2) <= 0
INFO - 16:23:37: over the design space:
INFO - 16:23:37: +------+-------------+-------+-------------+-------+
INFO - 16:23:37: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:37: +------+-------------+-------+-------------+-------+
INFO - 16:23:37: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:37: +------+-------------+-------+-------------+-------+
INFO - 16:23:37: Solving optimization problem with algorithm SLSQP:
WARNING - 16:23:37: Optimization found no feasible point; the least infeasible point is selected.
INFO - 16:23:37: 2%|▏ | 1/50 [00:00<00:00, 73.62 it/sec, feas=False, obj=-1.89]
INFO - 16:23:37: Optimization result:
INFO - 16:23:37: Optimizer info:
INFO - 16:23:37: Status: 8
INFO - 16:23:37: Message: Positive directional derivative for linesearch
INFO - 16:23:37: Solution:
WARNING - 16:23:37: The solution is not feasible.
INFO - 16:23:37: Objective: -1.8903954110973304
INFO - 16:23:37: Standardized constraints:
INFO - 16:23:37: g_2 = 0.0020301145386960595
INFO - 16:23:37: Design space:
INFO - 16:23:37: +------+-------------+-------+-------------+-------+
INFO - 16:23:37: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:37: +------+-------------+-------+-------------+-------+
INFO - 16:23:37: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:37: +------+-------------+-------+-------------+-------+
INFO - 16:23:37: *** End AerodynamicsScenario execution (time: 0:00:00.015350) ***
INFO - 16:23:37: *** Start StructureScenario execution ***
INFO - 16:23:37: StructureScenario
INFO - 16:23:37: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:37: MDO formulation: MDF
INFO - 16:23:37: Optimization problem:
INFO - 16:23:37: minimize 0.001*-y_4(x_1)
INFO - 16:23:37: with respect to x_1
INFO - 16:23:37: under the inequality constraints
INFO - 16:23:37: g_1(x_1) <= 0
INFO - 16:23:37: over the design space:
INFO - 16:23:37: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:37: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:37: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:37: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:37: | x_1[1] | 0.75 | 0.7806436836242986 | 1.25 | float |
INFO - 16:23:37: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:37: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:37: 2%|▏ | 1/50 [00:00<00:00, 76.97 it/sec, feas=True, obj=-1.89]
INFO - 16:23:37: Optimization result:
INFO - 16:23:37: Optimizer info:
INFO - 16:23:37: Status: 8
INFO - 16:23:37: Message: Positive directional derivative for linesearch
INFO - 16:23:37: Solution:
INFO - 16:23:37: The solution is feasible.
INFO - 16:23:37: Objective: -1.8903954110973304
INFO - 16:23:37: Standardized constraints:
INFO - 16:23:37: g_1 = [-1.79937220e-02 -1.10083737e-02 -1.91359899e-02 -2.77310526e-02
INFO - 16:23:37: -3.50104664e-02 -2.40000000e-01 1.64314118e-11]
INFO - 16:23:37: Design space:
INFO - 16:23:37: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:37: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:37: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:37: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:37: | x_1[1] | 0.75 | 0.7806436836242986 | 1.25 | float |
INFO - 16:23:37: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:37: *** End StructureScenario execution (time: 0:00:00.015025) ***
INFO - 16:23:37: *** Start PropulsionScenario execution ***
INFO - 16:23:37: PropulsionScenario
INFO - 16:23:37: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:37: MDO formulation: MDF
INFO - 16:23:37: Optimization problem:
INFO - 16:23:37: minimize 0.001*-y_4(x_3)
INFO - 16:23:37: with respect to x_3
INFO - 16:23:37: under the inequality constraints
INFO - 16:23:37: g_3(x_3) <= 0
INFO - 16:23:37: over the design space:
INFO - 16:23:37: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:37: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:37: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:37: | x_3 | 0.1 | 0.1717165375294035 | 1 | float |
INFO - 16:23:37: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:37: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:37: 2%|▏ | 1/50 [00:00<00:00, 106.49 it/sec, feas=True, obj=-1.89]
INFO - 16:23:37: Optimization result:
INFO - 16:23:37: Optimizer info:
INFO - 16:23:37: Status: 8
INFO - 16:23:37: Message: Positive directional derivative for linesearch
INFO - 16:23:37: Solution:
INFO - 16:23:37: The solution is feasible.
INFO - 16:23:37: Objective: -1.8903954110973304
INFO - 16:23:37: Standardized constraints:
INFO - 16:23:37: g_3 = [-7.15980250e-01 -2.84019750e-01 4.99600361e-14 -1.69666795e-01]
INFO - 16:23:37: Design space:
INFO - 16:23:37: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:37: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:37: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:37: | x_3 | 0.1 | 0.1717165375294035 | 1 | float |
INFO - 16:23:37: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:37: *** End PropulsionScenario execution (time: 0:00:00.011270) ***
INFO - 16:23:37: *** Start AerodynamicsScenario execution ***
INFO - 16:23:37: AerodynamicsScenario
INFO - 16:23:37: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:37: MDO formulation: MDF
INFO - 16:23:37: Optimization problem:
INFO - 16:23:37: minimize 0.001*-y_4(x_2)
INFO - 16:23:37: with respect to x_2
INFO - 16:23:37: under the inequality constraints
INFO - 16:23:37: g_2(x_2) <= 0
INFO - 16:23:37: over the design space:
INFO - 16:23:37: +------+-------------+-------+-------------+-------+
INFO - 16:23:37: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:37: +------+-------------+-------+-------------+-------+
INFO - 16:23:37: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:37: +------+-------------+-------+-------------+-------+
INFO - 16:23:37: Solving optimization problem with algorithm SLSQP:
WARNING - 16:23:37: Optimization found no feasible point; the least infeasible point is selected.
INFO - 16:23:37: 2%|▏ | 1/50 [00:00<00:00, 106.22 it/sec, feas=False, obj=-1.89]
INFO - 16:23:37: Optimization result:
INFO - 16:23:37: Optimizer info:
INFO - 16:23:37: Status: 8
INFO - 16:23:37: Message: Positive directional derivative for linesearch
INFO - 16:23:37: Solution:
WARNING - 16:23:37: The solution is not feasible.
INFO - 16:23:37: Objective: -1.8903954110973304
INFO - 16:23:37: Standardized constraints:
INFO - 16:23:37: g_2 = 0.0020301145386960595
INFO - 16:23:37: Design space:
INFO - 16:23:37: +------+-------------+-------+-------------+-------+
INFO - 16:23:37: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:37: +------+-------------+-------+-------------+-------+
INFO - 16:23:37: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:37: +------+-------------+-------+-------------+-------+
INFO - 16:23:37: *** End AerodynamicsScenario execution (time: 0:00:00.011068) ***
INFO - 16:23:37: *** Start StructureScenario execution ***
INFO - 16:23:37: StructureScenario
INFO - 16:23:37: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:37: MDO formulation: MDF
INFO - 16:23:37: Optimization problem:
INFO - 16:23:37: minimize 0.001*-y_4(x_1)
INFO - 16:23:37: with respect to x_1
INFO - 16:23:37: under the inequality constraints
INFO - 16:23:37: g_1(x_1) <= 0
INFO - 16:23:37: over the design space:
INFO - 16:23:37: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:37: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:37: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:37: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:37: | x_1[1] | 0.75 | 0.7806436836242986 | 1.25 | float |
INFO - 16:23:37: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:37: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:37: 2%|▏ | 1/50 [00:00<00:00, 100.17 it/sec, feas=True, obj=-1.89]
INFO - 16:23:37: Optimization result:
INFO - 16:23:37: Optimizer info:
INFO - 16:23:37: Status: 8
INFO - 16:23:37: Message: Positive directional derivative for linesearch
INFO - 16:23:37: Solution:
INFO - 16:23:37: The solution is feasible.
INFO - 16:23:37: Objective: -1.8903954110973304
INFO - 16:23:37: Standardized constraints:
INFO - 16:23:37: g_1 = [-1.79937220e-02 -1.10083737e-02 -1.91359899e-02 -2.77310526e-02
INFO - 16:23:37: -3.50104664e-02 -2.40000000e-01 1.64314118e-11]
INFO - 16:23:37: Design space:
INFO - 16:23:37: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:37: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:37: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:37: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:37: | x_1[1] | 0.75 | 0.7806436836242986 | 1.25 | float |
INFO - 16:23:37: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:37: *** End StructureScenario execution (time: 0:00:00.011994) ***
WARNING - 16:23:37: MDAJacobi has reached its maximum number of iterations, but the normalized residual norm 3.865109451355262e-05 is still above the tolerance 1e-06.
INFO - 16:23:37: 24%|██▍ | 24/100 [00:20<01:05, 1.16 it/sec, feas=False, obj=-1.89]
INFO - 16:23:37: *** Start PropulsionScenario execution ***
INFO - 16:23:37: PropulsionScenario
INFO - 16:23:37: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:37: MDO formulation: MDF
INFO - 16:23:37: Optimization problem:
INFO - 16:23:37: minimize 0.001*-y_4(x_3)
INFO - 16:23:37: with respect to x_3
INFO - 16:23:37: under the inequality constraints
INFO - 16:23:37: g_3(x_3) <= 0
INFO - 16:23:37: over the design space:
INFO - 16:23:37: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:37: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:37: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:37: | x_3 | 0.1 | 0.1717165375294035 | 1 | float |
INFO - 16:23:37: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:37: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:37: 2%|▏ | 1/50 [00:00<00:01, 36.15 it/sec, feas=False, obj=-2.3]
INFO - 16:23:37: 4%|▍ | 2/50 [00:00<00:01, 36.47 it/sec, feas=True, obj=-2.28]
INFO - 16:23:37: 6%|▌ | 3/50 [00:00<00:01, 29.52 it/sec, feas=False, obj=-2.3]
INFO - 16:23:37: 8%|▊ | 4/50 [00:00<00:01, 27.62 it/sec, feas=True, obj=-2.28]
INFO - 16:23:37: 10%|█ | 5/50 [00:00<00:01, 29.03 it/sec, feas=True, obj=-2.28]
INFO - 16:23:37: 12%|█▏ | 6/50 [00:00<00:01, 30.08 it/sec, feas=True, obj=-2.28]
INFO - 16:23:37: Optimization result:
INFO - 16:23:37: Optimizer info:
INFO - 16:23:37: Status: None
INFO - 16:23:37: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:37: Solution:
INFO - 16:23:37: The solution is feasible.
INFO - 16:23:37: Objective: -2.27906835162416
INFO - 16:23:37: Standardized constraints:
INFO - 16:23:37: g_3 = [-8.46817151e-01 -1.53182849e-01 7.54951657e-15 -1.82409896e-01]
INFO - 16:23:37: Design space:
INFO - 16:23:37: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:37: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:37: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:37: | x_3 | 0.1 | 0.1571420442204185 | 1 | float |
INFO - 16:23:37: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:37: *** End PropulsionScenario execution (time: 0:00:00.202019) ***
INFO - 16:23:37: *** Start AerodynamicsScenario execution ***
INFO - 16:23:37: AerodynamicsScenario
INFO - 16:23:37: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:37: MDO formulation: MDF
INFO - 16:23:37: Optimization problem:
INFO - 16:23:37: minimize 0.001*-y_4(x_2)
INFO - 16:23:37: with respect to x_2
INFO - 16:23:37: under the inequality constraints
INFO - 16:23:37: g_2(x_2) <= 0
INFO - 16:23:37: over the design space:
INFO - 16:23:37: +------+-------------+-------+-------------+-------+
INFO - 16:23:37: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:37: +------+-------------+-------+-------------+-------+
INFO - 16:23:37: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:37: +------+-------------+-------+-------------+-------+
INFO - 16:23:37: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:37: 2%|▏ | 1/50 [00:00<00:00, 77.33 it/sec, feas=False, obj=-2.28]
INFO - 16:23:37: 4%|▍ | 2/50 [00:00<00:00, 122.03 it/sec, feas=False, obj=-2.28]
INFO - 16:23:37: 6%|▌ | 3/50 [00:00<00:00, 151.82 it/sec, feas=False, obj=-2.28]
INFO - 16:23:37: 8%|▊ | 4/50 [00:00<00:00, 171.83 it/sec, feas=False, obj=-2.28]
INFO - 16:23:37: 10%|█ | 5/50 [00:00<00:00, 186.41 it/sec, feas=False, obj=-2.28]
INFO - 16:23:37: 12%|█▏ | 6/50 [00:00<00:00, 198.18 it/sec, feas=False, obj=-2.28]
INFO - 16:23:37: 14%|█▍ | 7/50 [00:00<00:00, 207.00 it/sec, feas=False, obj=-2.28]
INFO - 16:23:37: 16%|█▌ | 8/50 [00:00<00:00, 213.81 it/sec, feas=False, obj=-2.28]
INFO - 16:23:37: 18%|█▊ | 9/50 [00:00<00:00, 220.54 it/sec, feas=False, obj=-2.28]
INFO - 16:23:37: 20%|██ | 10/50 [00:00<00:00, 225.87 it/sec, feas=False, obj=-2.28]
INFO - 16:23:37: 22%|██▏ | 11/50 [00:00<00:00, 230.65 it/sec, feas=False, obj=-2.28]
INFO - 16:23:37: 24%|██▍ | 12/50 [00:00<00:00, 234.31 it/sec, feas=False, obj=-2.28]
INFO - 16:23:37: 26%|██▌ | 13/50 [00:00<00:00, 227.42 it/sec, feas=False, obj=-2.28]
INFO - 16:23:37: 28%|██▊ | 14/50 [00:00<00:00, 227.01 it/sec, feas=False, obj=-2.28]
INFO - 16:23:37: 30%|███ | 15/50 [00:00<00:00, 230.20 it/sec, feas=False, obj=-2.28]
INFO - 16:23:37: 32%|███▏ | 16/50 [00:00<00:00, 232.94 it/sec, feas=False, obj=-2.28]
INFO - 16:23:37: 34%|███▍ | 17/50 [00:00<00:00, 235.39 it/sec, feas=False, obj=-2.28]
INFO - 16:23:37: 36%|███▌ | 18/50 [00:00<00:00, 237.83 it/sec, feas=False, obj=-2.28]
INFO - 16:23:37: 38%|███▊ | 19/50 [00:00<00:00, 239.80 it/sec, feas=False, obj=-2.28]
WARNING - 16:23:37: Optimization found no feasible point; the least infeasible point is selected.
INFO - 16:23:37: 40%|████ | 20/50 [00:00<00:00, 191.54 it/sec, feas=False, obj=-2.28]
INFO - 16:23:37: Optimization result:
INFO - 16:23:37: Optimizer info:
INFO - 16:23:37: Status: 8
INFO - 16:23:37: Message: Positive directional derivative for linesearch
INFO - 16:23:37: Solution:
WARNING - 16:23:37: The solution is not feasible.
INFO - 16:23:37: Objective: -2.279068351624159
INFO - 16:23:37: Standardized constraints:
INFO - 16:23:37: g_2 = 0.001905298206935191
INFO - 16:23:37: Design space:
INFO - 16:23:37: +------+-------------+-------+-------------+-------+
INFO - 16:23:37: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:37: +------+-------------+-------+-------------+-------+
INFO - 16:23:37: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:37: +------+-------------+-------+-------------+-------+
INFO - 16:23:37: *** End AerodynamicsScenario execution (time: 0:00:00.106117) ***
INFO - 16:23:37: *** Start StructureScenario execution ***
INFO - 16:23:37: StructureScenario
INFO - 16:23:37: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:37: MDO formulation: MDF
INFO - 16:23:37: Optimization problem:
INFO - 16:23:37: minimize 0.001*-y_4(x_1)
INFO - 16:23:37: with respect to x_1
INFO - 16:23:37: under the inequality constraints
INFO - 16:23:37: g_1(x_1) <= 0
INFO - 16:23:37: over the design space:
INFO - 16:23:37: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:37: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:37: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:37: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:37: | x_1[1] | 0.75 | 0.7806436836242986 | 1.25 | float |
INFO - 16:23:37: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:37: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:37: 2%|▏ | 1/50 [00:00<00:00, 83.01 it/sec, feas=True, obj=-2.28]
INFO - 16:23:37: Optimization result:
INFO - 16:23:37: Optimizer info:
INFO - 16:23:37: Status: 8
INFO - 16:23:37: Message: Positive directional derivative for linesearch
INFO - 16:23:37: Solution:
INFO - 16:23:37: The solution is feasible.
INFO - 16:23:37: Objective: -2.27906835162416
INFO - 16:23:37: Standardized constraints:
INFO - 16:23:37: g_1 = [-1.69781125e-02 -1.04529781e-02 -1.87650722e-02 -2.74562204e-02
INFO - 16:23:37: -3.47936073e-02 -2.40000000e-01 1.64314118e-11]
INFO - 16:23:37: Design space:
INFO - 16:23:37: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:37: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:37: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:37: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:37: | x_1[1] | 0.75 | 0.7806436836242986 | 1.25 | float |
INFO - 16:23:37: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:37: *** End StructureScenario execution (time: 0:00:00.013984) ***
INFO - 16:23:37: *** Start PropulsionScenario execution ***
INFO - 16:23:37: PropulsionScenario
INFO - 16:23:37: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:37: MDO formulation: MDF
INFO - 16:23:37: Optimization problem:
INFO - 16:23:37: minimize 0.001*-y_4(x_3)
INFO - 16:23:37: with respect to x_3
INFO - 16:23:37: under the inequality constraints
INFO - 16:23:37: g_3(x_3) <= 0
INFO - 16:23:37: over the design space:
INFO - 16:23:37: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:37: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:37: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:37: | x_3 | 0.1 | 0.1571420442204185 | 1 | float |
INFO - 16:23:37: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:37: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:37: 2%|▏ | 1/50 [00:00<00:00, 107.97 it/sec, feas=True, obj=-2.28]
INFO - 16:23:37: 4%|▍ | 2/50 [00:00<00:00, 142.91 it/sec, feas=True, obj=-2.28]
INFO - 16:23:37: 6%|▌ | 3/50 [00:00<00:00, 150.04 it/sec, feas=True, obj=-2.28]
INFO - 16:23:37: Optimization result:
INFO - 16:23:37: Optimizer info:
INFO - 16:23:37: Status: None
INFO - 16:23:37: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:37: Solution:
INFO - 16:23:37: The solution is feasible.
INFO - 16:23:37: Objective: -2.27906835162416
INFO - 16:23:37: Standardized constraints:
INFO - 16:23:37: g_3 = [-8.46817151e-01 -1.53182849e-01 7.54951657e-15 -1.82409896e-01]
INFO - 16:23:37: Design space:
INFO - 16:23:37: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:37: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:37: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:37: | x_3 | 0.1 | 0.1571420442204185 | 1 | float |
INFO - 16:23:37: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:37: *** End PropulsionScenario execution (time: 0:00:00.022252) ***
INFO - 16:23:37: *** Start AerodynamicsScenario execution ***
INFO - 16:23:37: AerodynamicsScenario
INFO - 16:23:37: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:37: MDO formulation: MDF
INFO - 16:23:37: Optimization problem:
INFO - 16:23:37: minimize 0.001*-y_4(x_2)
INFO - 16:23:37: with respect to x_2
INFO - 16:23:37: under the inequality constraints
INFO - 16:23:37: g_2(x_2) <= 0
INFO - 16:23:37: over the design space:
INFO - 16:23:37: +------+-------------+-------+-------------+-------+
INFO - 16:23:37: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:37: +------+-------------+-------+-------------+-------+
INFO - 16:23:37: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:37: +------+-------------+-------+-------------+-------+
INFO - 16:23:37: Solving optimization problem with algorithm SLSQP:
WARNING - 16:23:37: Optimization found no feasible point; the least infeasible point is selected.
INFO - 16:23:37: 2%|▏ | 1/50 [00:00<00:00, 68.88 it/sec, feas=False, obj=-2.28]
INFO - 16:23:37: Optimization result:
INFO - 16:23:37: Optimizer info:
INFO - 16:23:37: Status: 8
INFO - 16:23:37: Message: Positive directional derivative for linesearch
INFO - 16:23:37: Solution:
WARNING - 16:23:37: The solution is not feasible.
INFO - 16:23:37: Objective: -2.27906835162416
INFO - 16:23:37: Standardized constraints:
INFO - 16:23:37: g_2 = 0.001905298206935191
INFO - 16:23:37: Design space:
INFO - 16:23:37: +------+-------------+-------+-------------+-------+
INFO - 16:23:37: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:37: +------+-------------+-------+-------------+-------+
INFO - 16:23:37: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:37: +------+-------------+-------+-------------+-------+
INFO - 16:23:37: *** End AerodynamicsScenario execution (time: 0:00:00.016181) ***
INFO - 16:23:37: *** Start StructureScenario execution ***
INFO - 16:23:37: StructureScenario
INFO - 16:23:37: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:37: MDO formulation: MDF
INFO - 16:23:37: Optimization problem:
INFO - 16:23:37: minimize 0.001*-y_4(x_1)
INFO - 16:23:37: with respect to x_1
INFO - 16:23:37: under the inequality constraints
INFO - 16:23:37: g_1(x_1) <= 0
INFO - 16:23:37: over the design space:
INFO - 16:23:37: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:37: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:37: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:37: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:37: | x_1[1] | 0.75 | 0.7806436836242986 | 1.25 | float |
INFO - 16:23:37: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:37: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:37: 2%|▏ | 1/50 [00:00<00:00, 102.22 it/sec, feas=True, obj=-2.28]
INFO - 16:23:37: Optimization result:
INFO - 16:23:37: Optimizer info:
INFO - 16:23:37: Status: 8
INFO - 16:23:37: Message: Positive directional derivative for linesearch
INFO - 16:23:37: Solution:
INFO - 16:23:37: The solution is feasible.
INFO - 16:23:37: Objective: -2.27906835162416
INFO - 16:23:37: Standardized constraints:
INFO - 16:23:37: g_1 = [-1.69781125e-02 -1.04529781e-02 -1.87650722e-02 -2.74562204e-02
INFO - 16:23:37: -3.47936073e-02 -2.40000000e-01 1.64314118e-11]
INFO - 16:23:37: Design space:
INFO - 16:23:37: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:37: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:37: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:37: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:37: | x_1[1] | 0.75 | 0.7806436836242986 | 1.25 | float |
INFO - 16:23:37: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:37: *** End StructureScenario execution (time: 0:00:00.011698) ***
INFO - 16:23:37: 25%|██▌ | 25/100 [00:21<01:03, 1.19 it/sec, feas=False, obj=-2.28]
INFO - 16:23:37: *** Start PropulsionScenario execution ***
INFO - 16:23:37: PropulsionScenario
INFO - 16:23:37: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:37: MDO formulation: MDF
INFO - 16:23:37: Optimization problem:
INFO - 16:23:37: minimize 0.001*-y_4(x_3)
INFO - 16:23:37: with respect to x_3
INFO - 16:23:37: under the inequality constraints
INFO - 16:23:37: g_3(x_3) <= 0
INFO - 16:23:37: over the design space:
INFO - 16:23:37: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:37: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:37: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:37: | x_3 | 0.1 | 0.1571420442204185 | 1 | float |
INFO - 16:23:37: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:37: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:37: 2%|▏ | 1/50 [00:00<00:01, 38.27 it/sec, feas=True, obj=-2.26]
INFO - 16:23:38: 4%|▍ | 2/50 [00:00<00:01, 29.97 it/sec, feas=True, obj=-2.26]
INFO - 16:23:38: 6%|▌ | 3/50 [00:00<00:01, 27.99 it/sec, feas=True, obj=-2.26]
INFO - 16:23:38: 8%|▊ | 4/50 [00:00<00:01, 29.88 it/sec, feas=True, obj=-2.26]
INFO - 16:23:38: Optimization result:
INFO - 16:23:38: Optimizer info:
INFO - 16:23:38: Status: 8
INFO - 16:23:38: Message: Positive directional derivative for linesearch
INFO - 16:23:38: Solution:
INFO - 16:23:38: The solution is feasible.
INFO - 16:23:38: Objective: -2.258072521384597
INFO - 16:23:38: Standardized constraints:
INFO - 16:23:38: g_3 = [-9.02198302e-01 -9.78016977e-02 2.66453526e-15 -1.81558251e-01]
INFO - 16:23:38: Design space:
INFO - 16:23:38: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:38: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:38: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:38: | x_3 | 0.1 | 0.1580559135944429 | 1 | float |
INFO - 16:23:38: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:38: *** End PropulsionScenario execution (time: 0:00:00.135983) ***
INFO - 16:23:38: *** Start AerodynamicsScenario execution ***
INFO - 16:23:38: AerodynamicsScenario
INFO - 16:23:38: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:38: MDO formulation: MDF
INFO - 16:23:38: Optimization problem:
INFO - 16:23:38: minimize 0.001*-y_4(x_2)
INFO - 16:23:38: with respect to x_2
INFO - 16:23:38: under the inequality constraints
INFO - 16:23:38: g_2(x_2) <= 0
INFO - 16:23:38: over the design space:
INFO - 16:23:38: +------+-------------+-------+-------------+-------+
INFO - 16:23:38: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:38: +------+-------------+-------+-------------+-------+
INFO - 16:23:38: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:38: +------+-------------+-------+-------------+-------+
INFO - 16:23:38: Solving optimization problem with algorithm SLSQP:
WARNING - 16:23:38: Optimization found no feasible point; the least infeasible point is selected.
INFO - 16:23:38: 2%|▏ | 1/50 [00:00<00:00, 63.96 it/sec, feas=False, obj=-2.26]
INFO - 16:23:38: Optimization result:
INFO - 16:23:38: Optimizer info:
INFO - 16:23:38: Status: 8
INFO - 16:23:38: Message: Positive directional derivative for linesearch
INFO - 16:23:38: Solution:
WARNING - 16:23:38: The solution is not feasible.
INFO - 16:23:38: Objective: -2.258072521384597
INFO - 16:23:38: Standardized constraints:
INFO - 16:23:38: g_2 = 0.010000000000000009
INFO - 16:23:38: Design space:
INFO - 16:23:38: +------+-------------+-------+-------------+-------+
INFO - 16:23:38: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:38: +------+-------------+-------+-------------+-------+
INFO - 16:23:38: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:38: +------+-------------+-------+-------------+-------+
INFO - 16:23:38: *** End AerodynamicsScenario execution (time: 0:00:00.017440) ***
INFO - 16:23:38: *** Start StructureScenario execution ***
INFO - 16:23:38: StructureScenario
INFO - 16:23:38: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:38: MDO formulation: MDF
INFO - 16:23:38: Optimization problem:
INFO - 16:23:38: minimize 0.001*-y_4(x_1)
INFO - 16:23:38: with respect to x_1
INFO - 16:23:38: under the inequality constraints
INFO - 16:23:38: g_1(x_1) <= 0
INFO - 16:23:38: over the design space:
INFO - 16:23:38: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:38: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:38: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:38: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:38: | x_1[1] | 0.75 | 0.7806436836242986 | 1.25 | float |
INFO - 16:23:38: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:38: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:38: 2%|▏ | 1/50 [00:00<00:00, 94.66 it/sec, feas=True, obj=-2.26]
INFO - 16:23:38: 4%|▍ | 2/50 [00:00<00:01, 35.51 it/sec, feas=True, obj=-2.29]
INFO - 16:23:38: 6%|▌ | 3/50 [00:00<00:01, 29.56 it/sec, feas=True, obj=-2.29]
INFO - 16:23:38: 8%|▊ | 4/50 [00:00<00:01, 27.44 it/sec, feas=True, obj=-2.29]
INFO - 16:23:38: 10%|█ | 5/50 [00:00<00:01, 26.24 it/sec, feas=True, obj=-2.29]
INFO - 16:23:38: 12%|█▏ | 6/50 [00:00<00:01, 25.52 it/sec, feas=True, obj=-2.29]
WARNING - 16:23:38: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 0.0009157477359807847 is still above the tolerance 1e-06.
INFO - 16:23:38: 14%|█▍ | 7/50 [00:00<00:01, 24.76 it/sec, feas=True, obj=-2.29]
INFO - 16:23:38: 16%|█▌ | 8/50 [00:00<00:01, 24.39 it/sec, feas=True, obj=-2.29]
INFO - 16:23:38: 18%|█▊ | 9/50 [00:00<00:01, 24.10 it/sec, feas=True, obj=-2.29]
INFO - 16:23:38: 20%|██ | 10/50 [00:00<00:01, 23.90 it/sec, feas=True, obj=-2.29]
INFO - 16:23:38: 22%|██▏ | 11/50 [00:00<00:01, 24.62 it/sec, feas=True, obj=-2.29]
INFO - 16:23:38: Optimization result:
INFO - 16:23:38: Optimizer info:
INFO - 16:23:38: Status: None
INFO - 16:23:38: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:38: Solution:
INFO - 16:23:38: The solution is feasible.
INFO - 16:23:38: Objective: -2.294030493059678
INFO - 16:23:38: Standardized constraints:
INFO - 16:23:38: g_1 = [-2.74831610e-02 -1.82092607e-02 -2.48646280e-02 -3.24713900e-02
INFO - 16:23:38: -3.90482070e-02 -2.40000000e-01 3.98570066e-14]
INFO - 16:23:38: Design space:
INFO - 16:23:38: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:38: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:38: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:38: | x_1[0] | 0.1 | 0.2934003507031356 | 0.4 | float |
INFO - 16:23:38: | x_1[1] | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:38: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:38: *** End StructureScenario execution (time: 0:00:00.449657) ***
INFO - 16:23:38: *** Start PropulsionScenario execution ***
INFO - 16:23:38: PropulsionScenario
INFO - 16:23:38: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:38: MDO formulation: MDF
INFO - 16:23:38: Optimization problem:
INFO - 16:23:38: minimize 0.001*-y_4(x_3)
INFO - 16:23:38: with respect to x_3
INFO - 16:23:38: under the inequality constraints
INFO - 16:23:38: g_3(x_3) <= 0
INFO - 16:23:38: over the design space:
INFO - 16:23:38: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:38: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:38: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:38: | x_3 | 0.1 | 0.1580559135944429 | 1 | float |
INFO - 16:23:38: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:38: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:38: 2%|▏ | 1/50 [00:00<00:00, 91.66 it/sec, feas=True, obj=-2.29]
INFO - 16:23:38: Optimization result:
INFO - 16:23:38: Optimizer info:
INFO - 16:23:38: Status: 8
INFO - 16:23:38: Message: Positive directional derivative for linesearch
INFO - 16:23:38: Solution:
INFO - 16:23:38: The solution is feasible.
INFO - 16:23:38: Objective: -2.294030493059678
INFO - 16:23:38: Standardized constraints:
INFO - 16:23:38: g_3 = [-9.02101313e-01 -9.78986872e-02 2.66453526e-15 -1.81558251e-01]
INFO - 16:23:38: Design space:
INFO - 16:23:38: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:38: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:38: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:38: | x_3 | 0.1 | 0.1580559135944429 | 1 | float |
INFO - 16:23:38: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:38: *** End PropulsionScenario execution (time: 0:00:00.012745) ***
INFO - 16:23:38: *** Start AerodynamicsScenario execution ***
INFO - 16:23:38: AerodynamicsScenario
INFO - 16:23:38: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:38: MDO formulation: MDF
INFO - 16:23:38: Optimization problem:
INFO - 16:23:38: minimize 0.001*-y_4(x_2)
INFO - 16:23:38: with respect to x_2
INFO - 16:23:38: under the inequality constraints
INFO - 16:23:38: g_2(x_2) <= 0
INFO - 16:23:38: over the design space:
INFO - 16:23:38: +------+-------------+-------+-------------+-------+
INFO - 16:23:38: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:38: +------+-------------+-------+-------------+-------+
INFO - 16:23:38: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:38: +------+-------------+-------+-------------+-------+
INFO - 16:23:38: Solving optimization problem with algorithm SLSQP:
WARNING - 16:23:38: Optimization found no feasible point; the least infeasible point is selected.
INFO - 16:23:38: 2%|▏ | 1/50 [00:00<00:00, 87.49 it/sec, feas=False, obj=-2.29]
INFO - 16:23:38: Optimization result:
INFO - 16:23:38: Optimizer info:
INFO - 16:23:38: Status: 8
INFO - 16:23:38: Message: Positive directional derivative for linesearch
INFO - 16:23:38: Solution:
WARNING - 16:23:38: The solution is not feasible.
INFO - 16:23:38: Objective: -2.294030493059678
INFO - 16:23:38: Standardized constraints:
INFO - 16:23:38: g_2 = 0.010000000000000009
INFO - 16:23:38: Design space:
INFO - 16:23:38: +------+-------------+-------+-------------+-------+
INFO - 16:23:38: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:38: +------+-------------+-------+-------------+-------+
INFO - 16:23:38: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:38: +------+-------------+-------+-------------+-------+
INFO - 16:23:38: *** End AerodynamicsScenario execution (time: 0:00:00.012891) ***
INFO - 16:23:38: *** Start StructureScenario execution ***
INFO - 16:23:38: StructureScenario
INFO - 16:23:38: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:38: MDO formulation: MDF
INFO - 16:23:38: Optimization problem:
INFO - 16:23:38: minimize 0.001*-y_4(x_1)
INFO - 16:23:38: with respect to x_1
INFO - 16:23:38: under the inequality constraints
INFO - 16:23:38: g_1(x_1) <= 0
INFO - 16:23:38: over the design space:
INFO - 16:23:38: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:38: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:38: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:38: | x_1[0] | 0.1 | 0.2934003507031356 | 0.4 | float |
INFO - 16:23:38: | x_1[1] | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:38: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:38: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:38: 2%|▏ | 1/50 [00:00<00:00, 102.17 it/sec, feas=True, obj=-2.29]
INFO - 16:23:38: 4%|▍ | 2/50 [00:00<00:00, 136.02 it/sec, feas=True, obj=-2.29]
WARNING - 16:23:38: MDAGaussSeidel has reached its maximum number of unsuccessful iterations, but the normalized residual norm 0.0009157477359807847 is still above the tolerance 1e-06.
INFO - 16:23:38: 6%|▌ | 3/50 [00:00<00:00, 119.43 it/sec, feas=True, obj=-2.29]
INFO - 16:23:38: Optimization result:
INFO - 16:23:38: Optimizer info:
INFO - 16:23:38: Status: None
INFO - 16:23:38: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:38: Solution:
INFO - 16:23:38: The solution is feasible.
INFO - 16:23:38: Objective: -2.294030493059678
INFO - 16:23:38: Standardized constraints:
INFO - 16:23:38: g_1 = [-2.74831610e-02 -1.82092607e-02 -2.48646280e-02 -3.24713900e-02
INFO - 16:23:38: -3.90482070e-02 -2.40000000e-01 3.98570066e-14]
INFO - 16:23:38: Design space:
INFO - 16:23:38: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:38: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:38: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:38: | x_1[0] | 0.1 | 0.2934003507031356 | 0.4 | float |
INFO - 16:23:38: | x_1[1] | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:38: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:38: *** End StructureScenario execution (time: 0:00:00.027443) ***
INFO - 16:23:38: 26%|██▌ | 26/100 [00:21<01:01, 1.20 it/sec, feas=False, obj=-2.29]
INFO - 16:23:38: *** Start PropulsionScenario execution ***
INFO - 16:23:38: PropulsionScenario
INFO - 16:23:38: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:38: MDO formulation: MDF
INFO - 16:23:38: Optimization problem:
INFO - 16:23:38: minimize 0.001*-y_4(x_3)
INFO - 16:23:38: with respect to x_3
INFO - 16:23:38: under the inequality constraints
INFO - 16:23:38: g_3(x_3) <= 0
INFO - 16:23:38: over the design space:
INFO - 16:23:38: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:38: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:38: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:38: | x_3 | 0.1 | 0.1580559135944429 | 1 | float |
INFO - 16:23:38: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:38: Solving optimization problem with algorithm SLSQP:
WARNING - 16:23:38: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 0.00026899729866434503 is still above the tolerance 1e-06.
INFO - 16:23:38: 2%|▏ | 1/50 [00:00<00:01, 33.63 it/sec, feas=True, obj=-2.13]
WARNING - 16:23:38: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 0.00026899729866434503 is still above the tolerance 1e-06.
INFO - 16:23:38: 4%|▍ | 2/50 [00:00<00:01, 26.16 it/sec, feas=True, obj=-2.13]
WARNING - 16:23:38: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 0.00026925986319700107 is still above the tolerance 1e-06.
INFO - 16:23:38: 6%|▌ | 3/50 [00:00<00:01, 27.98 it/sec, feas=True, obj=-2.13]
WARNING - 16:23:38: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 0.00026899729866434503 is still above the tolerance 1e-06.
INFO - 16:23:38: 8%|▊ | 4/50 [00:00<00:01, 29.00 it/sec, feas=True, obj=-2.13]
INFO - 16:23:38: Optimization result:
INFO - 16:23:38: Optimizer info:
INFO - 16:23:38: Status: None
INFO - 16:23:38: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:38: Solution:
INFO - 16:23:38: The solution is feasible.
INFO - 16:23:38: Objective: -2.1289562574981797
INFO - 16:23:38: Standardized constraints:
INFO - 16:23:38: g_3 = [-8.43577397e-01 -1.56422603e-01 8.43769499e-15 -1.81327905e-01]
INFO - 16:23:38: Design space:
INFO - 16:23:38: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:38: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:38: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:38: | x_3 | 0.1 | 0.1592933588088026 | 1 | float |
INFO - 16:23:38: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:38: *** End PropulsionScenario execution (time: 0:00:00.142385) ***
INFO - 16:23:38: *** Start AerodynamicsScenario execution ***
INFO - 16:23:38: AerodynamicsScenario
INFO - 16:23:38: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:38: MDO formulation: MDF
INFO - 16:23:38: Optimization problem:
INFO - 16:23:38: minimize 0.001*-y_4(x_2)
INFO - 16:23:38: with respect to x_2
INFO - 16:23:38: under the inequality constraints
INFO - 16:23:38: g_2(x_2) <= 0
INFO - 16:23:38: over the design space:
INFO - 16:23:38: +------+-------------+-------+-------------+-------+
INFO - 16:23:38: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:38: +------+-------------+-------+-------------+-------+
INFO - 16:23:38: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:38: +------+-------------+-------+-------------+-------+
INFO - 16:23:38: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:38: 2%|▏ | 1/50 [00:00<00:00, 71.00 it/sec, feas=True, obj=-2.13]
INFO - 16:23:38: Optimization result:
INFO - 16:23:38: Optimizer info:
INFO - 16:23:38: Status: 8
INFO - 16:23:38: Message: Positive directional derivative for linesearch
INFO - 16:23:38: Solution:
INFO - 16:23:38: The solution is feasible.
INFO - 16:23:38: Objective: -2.1289562574981797
INFO - 16:23:38: Standardized constraints:
INFO - 16:23:38: g_2 = -0.011800480809829317
INFO - 16:23:38: Design space:
INFO - 16:23:38: +------+-------------+-------+-------------+-------+
INFO - 16:23:38: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:38: +------+-------------+-------+-------------+-------+
INFO - 16:23:38: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:38: +------+-------------+-------+-------------+-------+
INFO - 16:23:38: *** End AerodynamicsScenario execution (time: 0:00:00.015780) ***
INFO - 16:23:38: *** Start StructureScenario execution ***
INFO - 16:23:38: StructureScenario
INFO - 16:23:38: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:38: MDO formulation: MDF
INFO - 16:23:38: Optimization problem:
INFO - 16:23:38: minimize 0.001*-y_4(x_1)
INFO - 16:23:38: with respect to x_1
INFO - 16:23:38: under the inequality constraints
INFO - 16:23:38: g_1(x_1) <= 0
INFO - 16:23:38: over the design space:
INFO - 16:23:38: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:38: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:38: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:38: | x_1[0] | 0.1 | 0.2934003507031356 | 0.4 | float |
INFO - 16:23:38: | x_1[1] | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:38: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:38: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:38: 2%|▏ | 1/50 [00:00<00:00, 97.76 it/sec, feas=False, obj=-2.13]
WARNING - 16:23:38: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 0.03846183075879215 is still above the tolerance 1e-06.
INFO - 16:23:38: 4%|▍ | 2/50 [00:00<00:01, 34.29 it/sec, feas=True, obj=-1.92]
INFO - 16:23:38: 6%|▌ | 3/50 [00:00<00:01, 29.28 it/sec, feas=True, obj=-1.96]
INFO - 16:23:38: 8%|▊ | 4/50 [00:00<00:01, 27.57 it/sec, feas=True, obj=-1.96]
INFO - 16:23:38: 10%|█ | 5/50 [00:00<00:01, 26.62 it/sec, feas=True, obj=-1.97]
INFO - 16:23:39: 12%|█▏ | 6/50 [00:00<00:01, 26.37 it/sec, feas=True, obj=-1.99]
INFO - 16:23:39: 14%|█▍ | 7/50 [00:00<00:01, 26.10 it/sec, feas=True, obj=-1.99]
INFO - 16:23:39: 16%|█▌ | 8/50 [00:00<00:01, 26.00 it/sec, feas=True, obj=-1.99]
INFO - 16:23:39: 18%|█▊ | 9/50 [00:00<00:01, 27.20 it/sec, feas=True, obj=-1.99]
INFO - 16:23:39: 20%|██ | 10/50 [00:00<00:01, 28.24 it/sec, feas=True, obj=-1.99]
INFO - 16:23:39: 22%|██▏ | 11/50 [00:00<00:01, 29.16 it/sec, feas=True, obj=-1.99]
INFO - 16:23:39: 24%|██▍ | 12/50 [00:00<00:01, 30.08 it/sec, feas=True, obj=-1.99]
INFO - 16:23:39: 26%|██▌ | 13/50 [00:00<00:01, 30.82 it/sec, feas=True, obj=-1.99]
INFO - 16:23:39: 28%|██▊ | 14/50 [00:00<00:01, 31.47 it/sec, feas=True, obj=-1.99]
INFO - 16:23:39: Optimization result:
INFO - 16:23:39: Optimizer info:
INFO - 16:23:39: Status: None
INFO - 16:23:39: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:39: Solution:
INFO - 16:23:39: The solution is feasible.
INFO - 16:23:39: Objective: -1.9877045601619774
INFO - 16:23:39: Standardized constraints:
INFO - 16:23:39: g_1 = [ 3.99248250e-08 -9.01516078e-03 -2.13920659e-02 -3.13363864e-02
INFO - 16:23:39: -3.90151741e-02 -2.04305745e-01 -3.56942546e-02]
INFO - 16:23:39: Design space:
INFO - 16:23:39: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:39: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:39: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:39: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:39: | x_1[1] | 0.75 | 0.8846932054936161 | 1.25 | float |
INFO - 16:23:39: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:39: *** End StructureScenario execution (time: 0:00:00.447742) ***
INFO - 16:23:39: *** Start PropulsionScenario execution ***
INFO - 16:23:39: PropulsionScenario
INFO - 16:23:39: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:39: MDO formulation: MDF
INFO - 16:23:39: Optimization problem:
INFO - 16:23:39: minimize 0.001*-y_4(x_3)
INFO - 16:23:39: with respect to x_3
INFO - 16:23:39: under the inequality constraints
INFO - 16:23:39: g_3(x_3) <= 0
INFO - 16:23:39: over the design space:
INFO - 16:23:39: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:39: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:39: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:39: | x_3 | 0.1 | 0.1592933588088026 | 1 | float |
INFO - 16:23:39: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:39: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:39: 2%|▏ | 1/50 [00:00<00:00, 89.18 it/sec, feas=True, obj=-1.99]
INFO - 16:23:39: Optimization result:
INFO - 16:23:39: Optimizer info:
INFO - 16:23:39: Status: 8
INFO - 16:23:39: Message: Positive directional derivative for linesearch
INFO - 16:23:39: Solution:
INFO - 16:23:39: The solution is feasible.
INFO - 16:23:39: Objective: -1.9877045601619774
INFO - 16:23:39: Standardized constraints:
INFO - 16:23:39: g_3 = [-8.43143014e-01 -1.56856986e-01 8.43769499e-15 -1.81327905e-01]
INFO - 16:23:39: Design space:
INFO - 16:23:39: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:39: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:39: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:39: | x_3 | 0.1 | 0.1592933588088026 | 1 | float |
INFO - 16:23:39: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:39: *** End PropulsionScenario execution (time: 0:00:00.013223) ***
INFO - 16:23:39: *** Start AerodynamicsScenario execution ***
INFO - 16:23:39: AerodynamicsScenario
INFO - 16:23:39: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:39: MDO formulation: MDF
INFO - 16:23:39: Optimization problem:
INFO - 16:23:39: minimize 0.001*-y_4(x_2)
INFO - 16:23:39: with respect to x_2
INFO - 16:23:39: under the inequality constraints
INFO - 16:23:39: g_2(x_2) <= 0
INFO - 16:23:39: over the design space:
INFO - 16:23:39: +------+-------------+-------+-------------+-------+
INFO - 16:23:39: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:39: +------+-------------+-------+-------------+-------+
INFO - 16:23:39: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:39: +------+-------------+-------+-------------+-------+
INFO - 16:23:39: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:39: 2%|▏ | 1/50 [00:00<00:00, 108.25 it/sec, feas=True, obj=-1.99]
INFO - 16:23:39: Optimization result:
INFO - 16:23:39: Optimizer info:
INFO - 16:23:39: Status: 8
INFO - 16:23:39: Message: Positive directional derivative for linesearch
INFO - 16:23:39: Solution:
INFO - 16:23:39: The solution is feasible.
INFO - 16:23:39: Objective: -1.9877045601619774
INFO - 16:23:39: Standardized constraints:
INFO - 16:23:39: g_2 = -0.011800480809829317
INFO - 16:23:39: Design space:
INFO - 16:23:39: +------+-------------+-------+-------------+-------+
INFO - 16:23:39: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:39: +------+-------------+-------+-------------+-------+
INFO - 16:23:39: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:39: +------+-------------+-------+-------------+-------+
INFO - 16:23:39: *** End AerodynamicsScenario execution (time: 0:00:00.010808) ***
INFO - 16:23:39: *** Start StructureScenario execution ***
INFO - 16:23:39: StructureScenario
INFO - 16:23:39: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:39: MDO formulation: MDF
INFO - 16:23:39: Optimization problem:
INFO - 16:23:39: minimize 0.001*-y_4(x_1)
INFO - 16:23:39: with respect to x_1
INFO - 16:23:39: under the inequality constraints
INFO - 16:23:39: g_1(x_1) <= 0
INFO - 16:23:39: over the design space:
INFO - 16:23:39: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:39: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:39: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:39: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:39: | x_1[1] | 0.75 | 0.8846932054936161 | 1.25 | float |
INFO - 16:23:39: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:39: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:39: 2%|▏ | 1/50 [00:00<00:00, 102.12 it/sec, feas=True, obj=-1.99]
INFO - 16:23:39: 4%|▍ | 2/50 [00:00<00:00, 51.39 it/sec, feas=True, obj=-1.99]
INFO - 16:23:39: 6%|▌ | 3/50 [00:00<00:01, 43.96 it/sec, feas=True, obj=-1.99]
INFO - 16:23:39: 8%|▊ | 4/50 [00:00<00:00, 49.51 it/sec, feas=True, obj=-1.99]
INFO - 16:23:39: Optimization result:
INFO - 16:23:39: Optimizer info:
INFO - 16:23:39: Status: None
INFO - 16:23:39: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:39: Solution:
INFO - 16:23:39: The solution is feasible.
INFO - 16:23:39: Objective: -1.9877045601619774
INFO - 16:23:39: Standardized constraints:
INFO - 16:23:39: g_1 = [ 3.99248250e-08 -9.01516078e-03 -2.13920659e-02 -3.13363864e-02
INFO - 16:23:39: -3.90151741e-02 -2.04305745e-01 -3.56942546e-02]
INFO - 16:23:39: Design space:
INFO - 16:23:39: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:39: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:39: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:39: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:39: | x_1[1] | 0.75 | 0.8846932054936161 | 1.25 | float |
INFO - 16:23:39: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:39: *** End StructureScenario execution (time: 0:00:00.083442) ***
INFO - 16:23:39: 27%|██▋ | 27/100 [00:22<01:00, 1.20 it/sec, feas=True, obj=-1.99]
INFO - 16:23:39: *** Start PropulsionScenario execution ***
INFO - 16:23:39: PropulsionScenario
INFO - 16:23:39: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:39: MDO formulation: MDF
INFO - 16:23:39: Optimization problem:
INFO - 16:23:39: minimize 0.001*-y_4(x_3)
INFO - 16:23:39: with respect to x_3
INFO - 16:23:39: under the inequality constraints
INFO - 16:23:39: g_3(x_3) <= 0
INFO - 16:23:39: over the design space:
INFO - 16:23:39: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:39: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:39: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:39: | x_3 | 0.1 | 0.1592933588088026 | 1 | float |
INFO - 16:23:39: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:39: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:39: 2%|▏ | 1/50 [00:00<00:01, 39.01 it/sec, feas=False, obj=-2.26]
INFO - 16:23:39: 4%|▍ | 2/50 [00:00<00:01, 40.95 it/sec, feas=True, obj=-2.26]
INFO - 16:23:39: 6%|▌ | 3/50 [00:00<00:01, 33.52 it/sec, feas=False, obj=-2.26]
INFO - 16:23:39: 8%|▊ | 4/50 [00:00<00:01, 30.65 it/sec, feas=True, obj=-2.26]
INFO - 16:23:39: Optimization result:
INFO - 16:23:39: Optimizer info:
INFO - 16:23:39: Status: 8
INFO - 16:23:39: Message: Positive directional derivative for linesearch
INFO - 16:23:39: Solution:
INFO - 16:23:39: The solution is feasible.
INFO - 16:23:39: Objective: -2.2592931285993583
INFO - 16:23:39: Standardized constraints:
INFO - 16:23:39: g_3 = [-9.17734908e-01 -8.22650924e-02 2.22044605e-15 -1.83255000e-01]
INFO - 16:23:39: Design space:
INFO - 16:23:39: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:39: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:39: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:39: | x_3 | 0.1 | 0.1562447456462878 | 1 | float |
INFO - 16:23:39: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:39: *** End PropulsionScenario execution (time: 0:00:00.132734) ***
INFO - 16:23:39: *** Start AerodynamicsScenario execution ***
INFO - 16:23:39: AerodynamicsScenario
INFO - 16:23:39: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:39: MDO formulation: MDF
INFO - 16:23:39: Optimization problem:
INFO - 16:23:39: minimize 0.001*-y_4(x_2)
INFO - 16:23:39: with respect to x_2
INFO - 16:23:39: under the inequality constraints
INFO - 16:23:39: g_2(x_2) <= 0
INFO - 16:23:39: over the design space:
INFO - 16:23:39: +------+-------------+-------+-------------+-------+
INFO - 16:23:39: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:39: +------+-------------+-------+-------------+-------+
INFO - 16:23:39: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:39: +------+-------------+-------+-------------+-------+
INFO - 16:23:39: Solving optimization problem with algorithm SLSQP:
WARNING - 16:23:39: Optimization found no feasible point; the least infeasible point is selected.
INFO - 16:23:39: 2%|▏ | 1/50 [00:00<00:00, 65.07 it/sec, feas=False, obj=-2.26]
INFO - 16:23:39: Optimization result:
INFO - 16:23:39: Optimizer info:
INFO - 16:23:39: Status: 8
INFO - 16:23:39: Message: Positive directional derivative for linesearch
INFO - 16:23:39: Solution:
WARNING - 16:23:39: The solution is not feasible.
INFO - 16:23:39: Objective: -2.2592931285993583
INFO - 16:23:39: Standardized constraints:
INFO - 16:23:39: g_2 = 0.010000000000000009
INFO - 16:23:39: Design space:
INFO - 16:23:39: +------+-------------+-------+-------------+-------+
INFO - 16:23:39: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:39: +------+-------------+-------+-------------+-------+
INFO - 16:23:39: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:39: +------+-------------+-------+-------------+-------+
INFO - 16:23:39: *** End AerodynamicsScenario execution (time: 0:00:00.017081) ***
INFO - 16:23:39: *** Start StructureScenario execution ***
INFO - 16:23:39: StructureScenario
INFO - 16:23:39: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:39: MDO formulation: MDF
INFO - 16:23:39: Optimization problem:
INFO - 16:23:39: minimize 0.001*-y_4(x_1)
INFO - 16:23:39: with respect to x_1
INFO - 16:23:39: under the inequality constraints
INFO - 16:23:39: g_1(x_1) <= 0
INFO - 16:23:39: over the design space:
INFO - 16:23:39: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:39: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:39: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:39: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:39: | x_1[1] | 0.75 | 0.8846932054936161 | 1.25 | float |
INFO - 16:23:39: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:39: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:39: 2%|▏ | 1/50 [00:00<00:00, 97.95 it/sec, feas=True, obj=-2.26]
INFO - 16:23:39: 4%|▍ | 2/50 [00:00<00:01, 34.90 it/sec, feas=True, obj=-2.4]
INFO - 16:23:39: 6%|▌ | 3/50 [00:00<00:01, 29.31 it/sec, feas=True, obj=-2.4]
INFO - 16:23:39: 8%|▊ | 4/50 [00:00<00:01, 27.02 it/sec, feas=True, obj=-2.4]
WARNING - 16:23:39: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 0.0018314954719615695 is still above the tolerance 1e-06.
INFO - 16:23:39: 10%|█ | 5/50 [00:00<00:01, 25.66 it/sec, feas=True, obj=-2.4]
INFO - 16:23:39: 12%|█▏ | 6/50 [00:00<00:01, 24.79 it/sec, feas=True, obj=-2.4]
WARNING - 16:23:39: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 0.0009157477359807847 is still above the tolerance 1e-06.
INFO - 16:23:39: 14%|█▍ | 7/50 [00:00<00:01, 24.17 it/sec, feas=True, obj=-2.4]
INFO - 16:23:39: 16%|█▌ | 8/50 [00:00<00:01, 23.88 it/sec, feas=True, obj=-2.4]
INFO - 16:23:39: 18%|█▊ | 9/50 [00:00<00:01, 23.57 it/sec, feas=True, obj=-2.4]
INFO - 16:23:39: 20%|██ | 10/50 [00:00<00:01, 23.40 it/sec, feas=True, obj=-2.4]
WARNING - 16:23:40: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 0.0009157477359807847 is still above the tolerance 1e-06.
INFO - 16:23:40: 22%|██▏ | 11/50 [00:00<00:01, 23.15 it/sec, feas=True, obj=-2.4]
INFO - 16:23:40: Optimization result:
INFO - 16:23:40: Optimizer info:
INFO - 16:23:40: Status: 8
INFO - 16:23:40: Message: Positive directional derivative for linesearch
INFO - 16:23:40: Solution:
INFO - 16:23:40: The solution is feasible.
INFO - 16:23:40: Objective: -2.3970419220121726
INFO - 16:23:40: Standardized constraints:
INFO - 16:23:40: g_1 = [-1.70297592e-02 -1.35160602e-02 -2.21981279e-02 -3.07478221e-02
INFO - 16:23:40: -3.78394738e-02 -2.40000000e-01 9.02611319e-14]
INFO - 16:23:40: Design space:
INFO - 16:23:40: +--------+-------------+-------------------+-------------+-------+
INFO - 16:23:40: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:40: +--------+-------------+-------------------+-------------+-------+
INFO - 16:23:40: | x_1[0] | 0.1 | 0.372360232675136 | 0.4 | float |
INFO - 16:23:40: | x_1[1] | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:40: +--------+-------------+-------------------+-------------+-------+
INFO - 16:23:40: *** End StructureScenario execution (time: 0:00:00.477542) ***
INFO - 16:23:40: *** Start PropulsionScenario execution ***
INFO - 16:23:40: PropulsionScenario
INFO - 16:23:40: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:40: MDO formulation: MDF
INFO - 16:23:40: Optimization problem:
INFO - 16:23:40: minimize 0.001*-y_4(x_3)
INFO - 16:23:40: with respect to x_3
INFO - 16:23:40: under the inequality constraints
INFO - 16:23:40: g_3(x_3) <= 0
INFO - 16:23:40: over the design space:
INFO - 16:23:40: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:40: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:40: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:40: | x_3 | 0.1 | 0.1562447456462878 | 1 | float |
INFO - 16:23:40: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:40: Solving optimization problem with algorithm SLSQP:
WARNING - 16:23:40: MDAGaussSeidel has reached its maximum number of unsuccessful iterations, but the normalized residual norm 6.724932466608626e-05 is still above the tolerance 1e-06.
INFO - 16:23:40: 2%|▏ | 1/50 [00:00<00:00, 52.54 it/sec, feas=True, obj=-2.4]
INFO - 16:23:40: 4%|▍ | 2/50 [00:00<00:00, 82.70 it/sec, feas=True, obj=-2.4]
INFO - 16:23:40: 6%|▌ | 3/50 [00:00<00:00, 103.02 it/sec, feas=True, obj=-2.4]
INFO - 16:23:40: Optimization result:
INFO - 16:23:40: Optimizer info:
INFO - 16:23:40: Status: None
INFO - 16:23:40: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:40: Solution:
INFO - 16:23:40: The solution is feasible.
INFO - 16:23:40: Objective: -2.3970419220121726
INFO - 16:23:40: Standardized constraints:
INFO - 16:23:40: g_3 = [-9.18164425e-01 -8.18355752e-02 4.66293670e-15 -1.83255000e-01]
INFO - 16:23:40: Design space:
INFO - 16:23:40: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:40: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:40: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:40: | x_3 | 0.1 | 0.1562447456462882 | 1 | float |
INFO - 16:23:40: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:40: *** End PropulsionScenario execution (time: 0:00:00.031664) ***
INFO - 16:23:40: *** Start AerodynamicsScenario execution ***
INFO - 16:23:40: AerodynamicsScenario
INFO - 16:23:40: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:40: MDO formulation: MDF
INFO - 16:23:40: Optimization problem:
INFO - 16:23:40: minimize 0.001*-y_4(x_2)
INFO - 16:23:40: with respect to x_2
INFO - 16:23:40: under the inequality constraints
INFO - 16:23:40: g_2(x_2) <= 0
INFO - 16:23:40: over the design space:
INFO - 16:23:40: +------+-------------+-------+-------------+-------+
INFO - 16:23:40: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:40: +------+-------------+-------+-------------+-------+
INFO - 16:23:40: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:40: +------+-------------+-------+-------------+-------+
INFO - 16:23:40: Solving optimization problem with algorithm SLSQP:
WARNING - 16:23:40: Optimization found no feasible point; the least infeasible point is selected.
INFO - 16:23:40: 2%|▏ | 1/50 [00:00<00:00, 78.91 it/sec, feas=False, obj=-2.4]
INFO - 16:23:40: Optimization result:
INFO - 16:23:40: Optimizer info:
INFO - 16:23:40: Status: 8
INFO - 16:23:40: Message: Positive directional derivative for linesearch
INFO - 16:23:40: Solution:
WARNING - 16:23:40: The solution is not feasible.
INFO - 16:23:40: Objective: -2.3970419220121726
INFO - 16:23:40: Standardized constraints:
INFO - 16:23:40: g_2 = 0.010000000000000009
INFO - 16:23:40: Design space:
INFO - 16:23:40: +------+-------------+-------+-------------+-------+
INFO - 16:23:40: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:40: +------+-------------+-------+-------------+-------+
INFO - 16:23:40: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:40: +------+-------------+-------+-------------+-------+
INFO - 16:23:40: *** End AerodynamicsScenario execution (time: 0:00:00.014421) ***
INFO - 16:23:40: *** Start StructureScenario execution ***
INFO - 16:23:40: StructureScenario
INFO - 16:23:40: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:40: MDO formulation: MDF
INFO - 16:23:40: Optimization problem:
INFO - 16:23:40: minimize 0.001*-y_4(x_1)
INFO - 16:23:40: with respect to x_1
INFO - 16:23:40: under the inequality constraints
INFO - 16:23:40: g_1(x_1) <= 0
INFO - 16:23:40: over the design space:
INFO - 16:23:40: +--------+-------------+-------------------+-------------+-------+
INFO - 16:23:40: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:40: +--------+-------------+-------------------+-------------+-------+
INFO - 16:23:40: | x_1[0] | 0.1 | 0.372360232675136 | 0.4 | float |
INFO - 16:23:40: | x_1[1] | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:40: +--------+-------------+-------------------+-------------+-------+
INFO - 16:23:40: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:40: 2%|▏ | 1/50 [00:00<00:00, 85.75 it/sec, feas=True, obj=-2.4]
INFO - 16:23:40: Optimization result:
INFO - 16:23:40: Optimizer info:
INFO - 16:23:40: Status: 8
INFO - 16:23:40: Message: Positive directional derivative for linesearch
INFO - 16:23:40: Solution:
INFO - 16:23:40: The solution is feasible.
INFO - 16:23:40: Objective: -2.3970419220121726
INFO - 16:23:40: Standardized constraints:
INFO - 16:23:40: g_1 = [-1.70297592e-02 -1.35160602e-02 -2.21981279e-02 -3.07478221e-02
INFO - 16:23:40: -3.78394738e-02 -2.40000000e-01 9.02611319e-14]
INFO - 16:23:40: Design space:
INFO - 16:23:40: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:40: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:40: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:40: | x_1[0] | 0.1 | 0.3723602326751361 | 0.4 | float |
INFO - 16:23:40: | x_1[1] | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:40: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:40: *** End StructureScenario execution (time: 0:00:00.013909) ***
INFO - 16:23:40: 28%|██▊ | 28/100 [00:23<00:59, 1.21 it/sec, feas=False, obj=-2.4]
INFO - 16:23:40: *** Start PropulsionScenario execution ***
INFO - 16:23:40: PropulsionScenario
INFO - 16:23:40: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:40: MDO formulation: MDF
INFO - 16:23:40: Optimization problem:
INFO - 16:23:40: minimize 0.001*-y_4(x_3)
INFO - 16:23:40: with respect to x_3
INFO - 16:23:40: under the inequality constraints
INFO - 16:23:40: g_3(x_3) <= 0
INFO - 16:23:40: over the design space:
INFO - 16:23:40: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:40: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:40: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:40: | x_3 | 0.1 | 0.1562447456462882 | 1 | float |
INFO - 16:23:40: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:40: Solving optimization problem with algorithm SLSQP:
WARNING - 16:23:40: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 0.00026899729866434503 is still above the tolerance 1e-06.
INFO - 16:23:40: 2%|▏ | 1/50 [00:00<00:01, 33.26 it/sec, feas=True, obj=-2.08]
WARNING - 16:23:40: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 0.00026899729866434503 is still above the tolerance 1e-06.
INFO - 16:23:40: 4%|▍ | 2/50 [00:00<00:01, 25.77 it/sec, feas=True, obj=-2.09]
WARNING - 16:23:40: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 0.00026899729866434503 is still above the tolerance 1e-06.
INFO - 16:23:40: 6%|▌ | 3/50 [00:00<00:01, 27.64 it/sec, feas=True, obj=-2.09]
WARNING - 16:23:40: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 0.00026899729866434503 is still above the tolerance 1e-06.
INFO - 16:23:40: 8%|▊ | 4/50 [00:00<00:01, 28.67 it/sec, feas=True, obj=-2.09]
INFO - 16:23:40: Optimization result:
INFO - 16:23:40: Optimizer info:
INFO - 16:23:40: Status: None
INFO - 16:23:40: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:40: Solution:
INFO - 16:23:40: The solution is feasible.
INFO - 16:23:40: Objective: -2.0859137445900084
INFO - 16:23:40: Standardized constraints:
INFO - 16:23:40: g_3 = [-8.24403381e-01 -1.75596619e-01 -2.22044605e-15 -1.82474064e-01]
INFO - 16:23:40: Design space:
INFO - 16:23:40: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:40: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:40: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:40: | x_3 | 0.1 | 0.1613713847316676 | 1 | float |
INFO - 16:23:40: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:40: *** End PropulsionScenario execution (time: 0:00:00.142357) ***
INFO - 16:23:40: *** Start AerodynamicsScenario execution ***
INFO - 16:23:40: AerodynamicsScenario
INFO - 16:23:40: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:40: MDO formulation: MDF
INFO - 16:23:40: Optimization problem:
INFO - 16:23:40: minimize 0.001*-y_4(x_2)
INFO - 16:23:40: with respect to x_2
INFO - 16:23:40: under the inequality constraints
INFO - 16:23:40: g_2(x_2) <= 0
INFO - 16:23:40: over the design space:
INFO - 16:23:40: +------+-------------+-------+-------------+-------+
INFO - 16:23:40: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:40: +------+-------------+-------+-------------+-------+
INFO - 16:23:40: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:40: +------+-------------+-------+-------------+-------+
INFO - 16:23:40: Solving optimization problem with algorithm SLSQP:
WARNING - 16:23:40: Optimization found no feasible point; the least infeasible point is selected.
INFO - 16:23:40: 2%|▏ | 1/50 [00:00<00:00, 67.26 it/sec, feas=False, obj=-2.09]
INFO - 16:23:40: Optimization result:
INFO - 16:23:40: Optimizer info:
INFO - 16:23:40: Status: 8
INFO - 16:23:40: Message: Positive directional derivative for linesearch
INFO - 16:23:40: Solution:
WARNING - 16:23:40: The solution is not feasible.
INFO - 16:23:40: Objective: -2.0859137445900084
INFO - 16:23:40: Standardized constraints:
INFO - 16:23:40: g_2 = 0.001004384257982771
INFO - 16:23:40: Design space:
INFO - 16:23:40: +------+-------------+-------+-------------+-------+
INFO - 16:23:40: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:40: +------+-------------+-------+-------------+-------+
INFO - 16:23:40: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:40: +------+-------------+-------+-------------+-------+
INFO - 16:23:40: *** End AerodynamicsScenario execution (time: 0:00:00.016723) ***
INFO - 16:23:40: *** Start StructureScenario execution ***
INFO - 16:23:40: StructureScenario
INFO - 16:23:40: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:40: MDO formulation: MDF
INFO - 16:23:40: Optimization problem:
INFO - 16:23:40: minimize 0.001*-y_4(x_1)
INFO - 16:23:40: with respect to x_1
INFO - 16:23:40: under the inequality constraints
INFO - 16:23:40: g_1(x_1) <= 0
INFO - 16:23:40: over the design space:
INFO - 16:23:40: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:40: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:40: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:40: | x_1[0] | 0.1 | 0.3723602326751361 | 0.4 | float |
INFO - 16:23:40: | x_1[1] | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:40: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:40: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:40: 2%|▏ | 1/50 [00:00<00:00, 96.03 it/sec, feas=False, obj=-2.09]
INFO - 16:23:40: 4%|▍ | 2/50 [00:00<00:01, 37.21 it/sec, feas=True, obj=-1.93]
INFO - 16:23:40: 6%|▌ | 3/50 [00:00<00:01, 31.75 it/sec, feas=True, obj=-1.95]
INFO - 16:23:40: 8%|▊ | 4/50 [00:00<00:01, 31.35 it/sec, feas=True, obj=-1.99]
INFO - 16:23:40: 10%|█ | 5/50 [00:00<00:01, 29.85 it/sec, feas=True, obj=-2.04]
INFO - 16:23:40: 12%|█▏ | 6/50 [00:00<00:01, 28.82 it/sec, feas=True, obj=-2.05]
INFO - 16:23:40: 14%|█▍ | 7/50 [00:00<00:01, 28.09 it/sec, feas=True, obj=-2.05]
INFO - 16:23:40: 16%|█▌ | 8/50 [00:00<00:01, 29.23 it/sec, feas=True, obj=-2.05]
INFO - 16:23:40: 18%|█▊ | 9/50 [00:00<00:01, 30.20 it/sec, feas=True, obj=-2.05]
INFO - 16:23:40: 20%|██ | 10/50 [00:00<00:01, 30.83 it/sec, feas=True, obj=-2.05]
INFO - 16:23:40: 22%|██▏ | 11/50 [00:00<00:01, 31.40 it/sec, feas=True, obj=-2.05]
INFO - 16:23:40: 24%|██▍ | 12/50 [00:00<00:01, 32.02 it/sec, feas=True, obj=-2.05]
WARNING - 16:23:40: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 0.0009157477359807847 is still above the tolerance 1e-06.
INFO - 16:23:40: 26%|██▌ | 13/50 [00:00<00:01, 32.11 it/sec, feas=True, obj=-2.05]
INFO - 16:23:40: 28%|██▊ | 14/50 [00:00<00:01, 31.38 it/sec, feas=True, obj=-2.05]
INFO - 16:23:40: Optimization result:
INFO - 16:23:40: Optimizer info:
INFO - 16:23:40: Status: None
INFO - 16:23:40: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:40: Solution:
INFO - 16:23:40: The solution is feasible.
INFO - 16:23:40: Objective: -2.0472886348986767
INFO - 16:23:40: Standardized constraints:
INFO - 16:23:40: g_1 = [-9.67635700e-03 -6.45698230e-03 -1.60950158e-02 -2.54771066e-02
INFO - 16:23:40: -3.32315300e-02 -2.40000018e-01 1.79571151e-08]
INFO - 16:23:40: Design space:
INFO - 16:23:40: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:40: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:40: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:40: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:40: | x_1[1] | 0.75 | 0.7806436265998381 | 1.25 | float |
INFO - 16:23:40: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:40: *** End StructureScenario execution (time: 0:00:00.448924) ***
INFO - 16:23:40: *** Start PropulsionScenario execution ***
INFO - 16:23:40: PropulsionScenario
INFO - 16:23:40: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:40: MDO formulation: MDF
INFO - 16:23:40: Optimization problem:
INFO - 16:23:40: minimize 0.001*-y_4(x_3)
INFO - 16:23:40: with respect to x_3
INFO - 16:23:40: under the inequality constraints
INFO - 16:23:40: g_3(x_3) <= 0
INFO - 16:23:40: over the design space:
INFO - 16:23:40: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:40: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:40: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:40: | x_3 | 0.1 | 0.1613713847316676 | 1 | float |
INFO - 16:23:40: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:40: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:40: 2%|▏ | 1/50 [00:00<00:00, 90.62 it/sec, feas=True, obj=-2.05]
INFO - 16:23:40: 4%|▍ | 2/50 [00:00<00:00, 55.78 it/sec, feas=True, obj=-2.05]
INFO - 16:23:40: 6%|▌ | 3/50 [00:00<00:00, 71.21 it/sec, feas=True, obj=-2.05]
INFO - 16:23:40: Optimization result:
INFO - 16:23:40: Optimizer info:
INFO - 16:23:40: Status: None
INFO - 16:23:40: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:40: Solution:
INFO - 16:23:40: The solution is feasible.
INFO - 16:23:40: Objective: -2.047288634898677
INFO - 16:23:40: Standardized constraints:
INFO - 16:23:40: g_3 = [-8.24560795e-01 -1.75439205e-01 4.44089210e-16 -1.82474064e-01]
INFO - 16:23:40: Design space:
INFO - 16:23:40: +------+-------------+-------------------+-------------+-------+
INFO - 16:23:40: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:40: +------+-------------+-------------------+-------------+-------+
INFO - 16:23:40: | x_3 | 0.1 | 0.161371384731668 | 1 | float |
INFO - 16:23:40: +------+-------------+-------------------+-------------+-------+
INFO - 16:23:40: *** End PropulsionScenario execution (time: 0:00:00.044659) ***
INFO - 16:23:40: *** Start AerodynamicsScenario execution ***
INFO - 16:23:40: AerodynamicsScenario
INFO - 16:23:40: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:40: MDO formulation: MDF
INFO - 16:23:40: Optimization problem:
INFO - 16:23:40: minimize 0.001*-y_4(x_2)
INFO - 16:23:40: with respect to x_2
INFO - 16:23:40: under the inequality constraints
INFO - 16:23:40: g_2(x_2) <= 0
INFO - 16:23:40: over the design space:
INFO - 16:23:40: +------+-------------+-------+-------------+-------+
INFO - 16:23:40: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:40: +------+-------------+-------+-------------+-------+
INFO - 16:23:40: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:40: +------+-------------+-------+-------------+-------+
INFO - 16:23:40: Solving optimization problem with algorithm SLSQP:
WARNING - 16:23:40: Optimization found no feasible point; the least infeasible point is selected.
INFO - 16:23:40: 2%|▏ | 1/50 [00:00<00:00, 78.76 it/sec, feas=False, obj=-2.05]
INFO - 16:23:40: Optimization result:
INFO - 16:23:40: Optimizer info:
INFO - 16:23:40: Status: 8
INFO - 16:23:40: Message: Positive directional derivative for linesearch
INFO - 16:23:40: Solution:
WARNING - 16:23:40: The solution is not feasible.
INFO - 16:23:40: Objective: -2.047288634898677
INFO - 16:23:40: Standardized constraints:
INFO - 16:23:40: g_2 = 0.001004384257982771
INFO - 16:23:40: Design space:
INFO - 16:23:40: +------+-------------+-------+-------------+-------+
INFO - 16:23:40: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:40: +------+-------------+-------+-------------+-------+
INFO - 16:23:40: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:40: +------+-------------+-------+-------------+-------+
INFO - 16:23:40: *** End AerodynamicsScenario execution (time: 0:00:00.014503) ***
INFO - 16:23:40: *** Start StructureScenario execution ***
INFO - 16:23:40: StructureScenario
INFO - 16:23:40: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:40: MDO formulation: MDF
INFO - 16:23:40: Optimization problem:
INFO - 16:23:40: minimize 0.001*-y_4(x_1)
INFO - 16:23:40: with respect to x_1
INFO - 16:23:40: under the inequality constraints
INFO - 16:23:40: g_1(x_1) <= 0
INFO - 16:23:40: over the design space:
INFO - 16:23:40: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:40: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:40: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:40: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:40: | x_1[1] | 0.75 | 0.7806436265998381 | 1.25 | float |
INFO - 16:23:40: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:40: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:40: 2%|▏ | 1/50 [00:00<00:00, 101.74 it/sec, feas=True, obj=-2.05]
WARNING - 16:23:40: MDAGaussSeidel has reached its maximum number of unsuccessful iterations, but the normalized residual norm 0.0009157477359807847 is still above the tolerance 1e-06.
INFO - 16:23:40: 4%|▍ | 2/50 [00:00<00:01, 40.92 it/sec, feas=True, obj=-2.05]
INFO - 16:23:40: 6%|▌ | 3/50 [00:00<00:01, 37.82 it/sec, feas=True, obj=-2.05]
INFO - 16:23:40: 8%|▊ | 4/50 [00:00<00:01, 36.16 it/sec, feas=True, obj=-2.05]
INFO - 16:23:40: Optimization result:
INFO - 16:23:40: Optimizer info:
INFO - 16:23:40: Status: None
INFO - 16:23:40: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:40: Solution:
INFO - 16:23:40: The solution is feasible.
INFO - 16:23:40: Objective: -2.047288634898677
INFO - 16:23:40: Standardized constraints:
INFO - 16:23:40: g_1 = [-9.67635700e-03 -6.45698230e-03 -1.60950158e-02 -2.54771066e-02
INFO - 16:23:40: -3.32315300e-02 -2.40000018e-01 1.79571151e-08]
INFO - 16:23:40: Design space:
INFO - 16:23:40: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:40: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:40: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:40: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:40: | x_1[1] | 0.75 | 0.7806436265998381 | 1.25 | float |
INFO - 16:23:40: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:40: *** End StructureScenario execution (time: 0:00:00.113388) ***
INFO - 16:23:40: 29%|██▉ | 29/100 [00:24<00:58, 1.21 it/sec, feas=False, obj=-2.05]
INFO - 16:23:40: *** Start PropulsionScenario execution ***
INFO - 16:23:40: PropulsionScenario
INFO - 16:23:40: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:40: MDO formulation: MDF
INFO - 16:23:40: Optimization problem:
INFO - 16:23:40: minimize 0.001*-y_4(x_3)
INFO - 16:23:40: with respect to x_3
INFO - 16:23:40: under the inequality constraints
INFO - 16:23:40: g_3(x_3) <= 0
INFO - 16:23:40: over the design space:
INFO - 16:23:40: +------+-------------+-------------------+-------------+-------+
INFO - 16:23:40: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:40: +------+-------------+-------------------+-------------+-------+
INFO - 16:23:40: | x_3 | 0.1 | 0.161371384731668 | 1 | float |
INFO - 16:23:40: +------+-------------+-------------------+-------------+-------+
INFO - 16:23:40: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:40: 2%|▏ | 1/50 [00:00<00:01, 38.67 it/sec, feas=False, obj=-2.26]
INFO - 16:23:41: 4%|▍ | 2/50 [00:00<00:01, 38.59 it/sec, feas=True, obj=-2.26]
INFO - 16:23:41: 6%|▌ | 3/50 [00:00<00:01, 32.11 it/sec, feas=False, obj=-2.26]
INFO - 16:23:41: 8%|▊ | 4/50 [00:00<00:01, 29.47 it/sec, feas=True, obj=-2.26]
INFO - 16:23:41: Optimization result:
INFO - 16:23:41: Optimizer info:
INFO - 16:23:41: Status: 8
INFO - 16:23:41: Message: Positive directional derivative for linesearch
INFO - 16:23:41: Solution:
INFO - 16:23:41: The solution is feasible.
INFO - 16:23:41: Objective: -2.256566092279192
INFO - 16:23:41: Standardized constraints:
INFO - 16:23:41: g_3 = [-9.29697350e-01 -7.03026502e-02 2.88657986e-15 -1.81558251e-01]
INFO - 16:23:41: Design space:
INFO - 16:23:41: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:41: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:41: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:41: | x_3 | 0.1 | 0.1601494065626361 | 1 | float |
INFO - 16:23:41: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:41: *** End PropulsionScenario execution (time: 0:00:00.138019) ***
INFO - 16:23:41: *** Start AerodynamicsScenario execution ***
INFO - 16:23:41: AerodynamicsScenario
INFO - 16:23:41: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:41: MDO formulation: MDF
INFO - 16:23:41: Optimization problem:
INFO - 16:23:41: minimize 0.001*-y_4(x_2)
INFO - 16:23:41: with respect to x_2
INFO - 16:23:41: under the inequality constraints
INFO - 16:23:41: g_2(x_2) <= 0
INFO - 16:23:41: over the design space:
INFO - 16:23:41: +------+-------------+-------+-------------+-------+
INFO - 16:23:41: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:41: +------+-------------+-------+-------------+-------+
INFO - 16:23:41: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:41: +------+-------------+-------+-------------+-------+
INFO - 16:23:41: Solving optimization problem with algorithm SLSQP:
WARNING - 16:23:41: Optimization found no feasible point; the least infeasible point is selected.
INFO - 16:23:41: 2%|▏ | 1/50 [00:00<00:00, 66.38 it/sec, feas=False, obj=-2.26]
INFO - 16:23:41: Optimization result:
INFO - 16:23:41: Optimizer info:
INFO - 16:23:41: Status: 8
INFO - 16:23:41: Message: Positive directional derivative for linesearch
INFO - 16:23:41: Solution:
WARNING - 16:23:41: The solution is not feasible.
INFO - 16:23:41: Objective: -2.256566092279192
INFO - 16:23:41: Standardized constraints:
INFO - 16:23:41: g_2 = 0.007491760801586533
INFO - 16:23:41: Design space:
INFO - 16:23:41: +------+-------------+-------+-------------+-------+
INFO - 16:23:41: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:41: +------+-------------+-------+-------------+-------+
INFO - 16:23:41: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:41: +------+-------------+-------+-------------+-------+
INFO - 16:23:41: *** End AerodynamicsScenario execution (time: 0:00:00.016652) ***
INFO - 16:23:41: *** Start StructureScenario execution ***
INFO - 16:23:41: StructureScenario
INFO - 16:23:41: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:41: MDO formulation: MDF
INFO - 16:23:41: Optimization problem:
INFO - 16:23:41: minimize 0.001*-y_4(x_1)
INFO - 16:23:41: with respect to x_1
INFO - 16:23:41: under the inequality constraints
INFO - 16:23:41: g_1(x_1) <= 0
INFO - 16:23:41: over the design space:
INFO - 16:23:41: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:41: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:41: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:41: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:41: | x_1[1] | 0.75 | 0.7806436265998381 | 1.25 | float |
INFO - 16:23:41: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:41: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:41: 2%|▏ | 1/50 [00:00<00:00, 97.63 it/sec, feas=True, obj=-2.26]
INFO - 16:23:41: 4%|▍ | 2/50 [00:00<00:01, 36.37 it/sec, feas=True, obj=-2.29]
WARNING - 16:23:41: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 0.0018314954719615695 is still above the tolerance 1e-06.
INFO - 16:23:41: 6%|▌ | 3/50 [00:00<00:01, 29.37 it/sec, feas=True, obj=-2.29]
INFO - 16:23:41: 8%|▊ | 4/50 [00:00<00:01, 27.28 it/sec, feas=True, obj=-2.29]
INFO - 16:23:41: 10%|█ | 5/50 [00:00<00:01, 26.02 it/sec, feas=True, obj=-2.29]
INFO - 16:23:41: 12%|█▏ | 6/50 [00:00<00:01, 25.27 it/sec, feas=True, obj=-2.29]
INFO - 16:23:41: 14%|█▍ | 7/50 [00:00<00:01, 24.74 it/sec, feas=True, obj=-2.29]
INFO - 16:23:41: 16%|█▌ | 8/50 [00:00<00:01, 24.27 it/sec, feas=True, obj=-2.29]
INFO - 16:23:41: 18%|█▊ | 9/50 [00:00<00:01, 24.00 it/sec, feas=True, obj=-2.29]
INFO - 16:23:41: 20%|██ | 10/50 [00:00<00:01, 23.78 it/sec, feas=True, obj=-2.29]
INFO - 16:23:41: 22%|██▏ | 11/50 [00:00<00:01, 23.62 it/sec, feas=True, obj=-2.29]
INFO - 16:23:41: Optimization result:
INFO - 16:23:41: Optimizer info:
INFO - 16:23:41: Status: 8
INFO - 16:23:41: Message: Positive directional derivative for linesearch
INFO - 16:23:41: Solution:
INFO - 16:23:41: The solution is feasible.
INFO - 16:23:41: Objective: -2.2931663364498625
INFO - 16:23:41: Standardized constraints:
INFO - 16:23:41: g_1 = [ 0. -0.00472998 -0.01657122 -0.02670837 -0.03472998 -0.2363848
INFO - 16:23:41: -0.0036152 ]
INFO - 16:23:41: Design space:
INFO - 16:23:41: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:41: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:41: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:41: | x_1[0] | 0.1 | 0.3899149694330776 | 0.4 | float |
INFO - 16:23:41: | x_1[1] | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:41: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:41: *** End StructureScenario execution (time: 0:00:00.468215) ***
INFO - 16:23:41: *** Start PropulsionScenario execution ***
INFO - 16:23:41: PropulsionScenario
INFO - 16:23:41: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:41: MDO formulation: MDF
INFO - 16:23:41: Optimization problem:
INFO - 16:23:41: minimize 0.001*-y_4(x_3)
INFO - 16:23:41: with respect to x_3
INFO - 16:23:41: under the inequality constraints
INFO - 16:23:41: g_3(x_3) <= 0
INFO - 16:23:41: over the design space:
INFO - 16:23:41: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:41: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:41: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:41: | x_3 | 0.1 | 0.1601494065626361 | 1 | float |
INFO - 16:23:41: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:41: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:41: 2%|▏ | 1/50 [00:00<00:00, 108.86 it/sec, feas=True, obj=-2.29]
INFO - 16:23:41: 4%|▍ | 2/50 [00:00<00:00, 61.45 it/sec, feas=True, obj=-2.29]
INFO - 16:23:41: 6%|▌ | 3/50 [00:00<00:00, 77.46 it/sec, feas=True, obj=-2.29]
INFO - 16:23:41: Optimization result:
INFO - 16:23:41: Optimizer info:
INFO - 16:23:41: Status: None
INFO - 16:23:41: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:41: Solution:
INFO - 16:23:41: The solution is feasible.
INFO - 16:23:41: Objective: -2.2931663364499015
INFO - 16:23:41: Standardized constraints:
INFO - 16:23:41: g_3 = [-9.29554070e-01 -7.04459300e-02 1.38777878e-13 -1.81558251e-01]
INFO - 16:23:41: Design space:
INFO - 16:23:41: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:41: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:41: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:41: | x_3 | 0.1 | 0.1601494065626578 | 1 | float |
INFO - 16:23:41: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:41: *** End PropulsionScenario execution (time: 0:00:00.041240) ***
INFO - 16:23:41: *** Start AerodynamicsScenario execution ***
INFO - 16:23:41: AerodynamicsScenario
INFO - 16:23:41: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:41: MDO formulation: MDF
INFO - 16:23:41: Optimization problem:
INFO - 16:23:41: minimize 0.001*-y_4(x_2)
INFO - 16:23:41: with respect to x_2
INFO - 16:23:41: under the inequality constraints
INFO - 16:23:41: g_2(x_2) <= 0
INFO - 16:23:41: over the design space:
INFO - 16:23:41: +------+-------------+-------+-------------+-------+
INFO - 16:23:41: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:41: +------+-------------+-------+-------------+-------+
INFO - 16:23:41: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:41: +------+-------------+-------+-------------+-------+
INFO - 16:23:41: Solving optimization problem with algorithm SLSQP:
WARNING - 16:23:41: Optimization found no feasible point; the least infeasible point is selected.
INFO - 16:23:41: 2%|▏ | 1/50 [00:00<00:00, 76.38 it/sec, feas=False, obj=-2.29]
INFO - 16:23:41: Optimization result:
INFO - 16:23:41: Optimizer info:
INFO - 16:23:41: Status: 8
INFO - 16:23:41: Message: Positive directional derivative for linesearch
INFO - 16:23:41: Solution:
WARNING - 16:23:41: The solution is not feasible.
INFO - 16:23:41: Objective: -2.2931663364499015
INFO - 16:23:41: Standardized constraints:
INFO - 16:23:41: g_2 = 0.007491760801586533
INFO - 16:23:41: Design space:
INFO - 16:23:41: +------+-------------+-------+-------------+-------+
INFO - 16:23:41: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:41: +------+-------------+-------+-------------+-------+
INFO - 16:23:41: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:41: +------+-------------+-------+-------------+-------+
INFO - 16:23:41: *** End AerodynamicsScenario execution (time: 0:00:00.014790) ***
INFO - 16:23:41: *** Start StructureScenario execution ***
INFO - 16:23:41: StructureScenario
INFO - 16:23:41: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:41: MDO formulation: MDF
INFO - 16:23:41: Optimization problem:
INFO - 16:23:41: minimize 0.001*-y_4(x_1)
INFO - 16:23:41: with respect to x_1
INFO - 16:23:41: under the inequality constraints
INFO - 16:23:41: g_1(x_1) <= 0
INFO - 16:23:41: over the design space:
INFO - 16:23:41: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:41: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:41: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:41: | x_1[0] | 0.1 | 0.3899149694330776 | 0.4 | float |
INFO - 16:23:41: | x_1[1] | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:41: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:41: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:41: 2%|▏ | 1/50 [00:00<00:00, 86.98 it/sec, feas=True, obj=-2.29]
INFO - 16:23:41: Optimization result:
INFO - 16:23:41: Optimizer info:
INFO - 16:23:41: Status: 8
INFO - 16:23:41: Message: Positive directional derivative for linesearch
INFO - 16:23:41: Solution:
INFO - 16:23:41: The solution is feasible.
INFO - 16:23:41: Objective: -2.2931663364499015
INFO - 16:23:41: Standardized constraints:
INFO - 16:23:41: g_1 = [ 0. -0.00472998 -0.01657122 -0.02670837 -0.03472998 -0.2363848
INFO - 16:23:41: -0.0036152 ]
INFO - 16:23:41: Design space:
INFO - 16:23:41: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:41: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:41: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:41: | x_1[0] | 0.1 | 0.3899149694330777 | 0.4 | float |
INFO - 16:23:41: | x_1[1] | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:41: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:41: *** End StructureScenario execution (time: 0:00:00.013488) ***
INFO - 16:23:41: 30%|███ | 30/100 [00:24<00:57, 1.21 it/sec, feas=False, obj=-2.29]
INFO - 16:23:41: *** Start PropulsionScenario execution ***
INFO - 16:23:41: PropulsionScenario
INFO - 16:23:41: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:41: MDO formulation: MDF
INFO - 16:23:41: Optimization problem:
INFO - 16:23:41: minimize 0.001*-y_4(x_3)
INFO - 16:23:41: with respect to x_3
INFO - 16:23:41: under the inequality constraints
INFO - 16:23:41: g_3(x_3) <= 0
INFO - 16:23:41: over the design space:
INFO - 16:23:41: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:41: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:41: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:41: | x_3 | 0.1 | 0.1601494065626578 | 1 | float |
INFO - 16:23:41: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:41: Solving optimization problem with algorithm SLSQP:
WARNING - 16:23:41: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 0.0014122358179878111 is still above the tolerance 1e-06.
INFO - 16:23:41: 2%|▏ | 1/50 [00:00<00:01, 33.35 it/sec, feas=True, obj=-2.12]
WARNING - 16:23:41: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 0.0013786111556547682 is still above the tolerance 1e-06.
INFO - 16:23:41: 4%|▍ | 2/50 [00:00<00:01, 25.85 it/sec, feas=True, obj=-2.13]
WARNING - 16:23:41: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 0.0014122358179878111 is still above the tolerance 1e-06.
INFO - 16:23:41: 6%|▌ | 3/50 [00:00<00:01, 23.66 it/sec, feas=True, obj=-2.13]
INFO - 16:23:41: Optimization result:
INFO - 16:23:41: Optimizer info:
INFO - 16:23:41: Status: 8
INFO - 16:23:41: Message: Positive directional derivative for linesearch
INFO - 16:23:41: Solution:
INFO - 16:23:41: The solution is feasible.
INFO - 16:23:41: Objective: -2.128856017923058
INFO - 16:23:41: Standardized constraints:
INFO - 16:23:41: g_3 = [-8.53031936e-01 -1.46968064e-01 2.22044605e-16 -1.82328530e-01]
INFO - 16:23:41: Design space:
INFO - 16:23:41: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:41: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:41: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:41: | x_3 | 0.1 | 0.1639712244856577 | 1 | float |
INFO - 16:23:41: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:41: *** End PropulsionScenario execution (time: 0:00:00.128795) ***
INFO - 16:23:41: *** Start AerodynamicsScenario execution ***
INFO - 16:23:41: AerodynamicsScenario
INFO - 16:23:41: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:41: MDO formulation: MDF
INFO - 16:23:41: Optimization problem:
INFO - 16:23:41: minimize 0.001*-y_4(x_2)
INFO - 16:23:41: with respect to x_2
INFO - 16:23:41: under the inequality constraints
INFO - 16:23:41: g_2(x_2) <= 0
INFO - 16:23:41: over the design space:
INFO - 16:23:41: +------+-------------+-------+-------------+-------+
INFO - 16:23:41: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:41: +------+-------------+-------+-------------+-------+
INFO - 16:23:41: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:41: +------+-------------+-------+-------------+-------+
INFO - 16:23:41: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:41: 2%|▏ | 1/50 [00:00<00:00, 87.48 it/sec, feas=True, obj=-2.13]
INFO - 16:23:41: Optimization result:
INFO - 16:23:41: Optimizer info:
INFO - 16:23:41: Status: 8
INFO - 16:23:41: Message: Positive directional derivative for linesearch
INFO - 16:23:41: Solution:
INFO - 16:23:41: The solution is feasible.
INFO - 16:23:41: Objective: -2.128856017923059
INFO - 16:23:41: Standardized constraints:
INFO - 16:23:41: g_2 = -0.005041321670290921
INFO - 16:23:41: Design space:
INFO - 16:23:41: +------+-------------+-------+-------------+-------+
INFO - 16:23:41: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:41: +------+-------------+-------+-------------+-------+
INFO - 16:23:41: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:41: +------+-------------+-------+-------------+-------+
INFO - 16:23:41: *** End AerodynamicsScenario execution (time: 0:00:00.013072) ***
INFO - 16:23:41: *** Start StructureScenario execution ***
INFO - 16:23:41: StructureScenario
INFO - 16:23:41: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:41: MDO formulation: MDF
INFO - 16:23:41: Optimization problem:
INFO - 16:23:41: minimize 0.001*-y_4(x_1)
INFO - 16:23:41: with respect to x_1
INFO - 16:23:41: under the inequality constraints
INFO - 16:23:41: g_1(x_1) <= 0
INFO - 16:23:41: over the design space:
INFO - 16:23:41: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:41: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:41: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:41: | x_1[0] | 0.1 | 0.3899149694330777 | 0.4 | float |
INFO - 16:23:41: | x_1[1] | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:41: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:41: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:41: 2%|▏ | 1/50 [00:00<00:00, 98.54 it/sec, feas=False, obj=-2.13]
INFO - 16:23:41: 4%|▍ | 2/50 [00:00<00:01, 36.92 it/sec, feas=True, obj=-1.95]
INFO - 16:23:41: 6%|▌ | 3/50 [00:00<00:01, 31.25 it/sec, feas=True, obj=-1.97]
INFO - 16:23:41: 8%|▊ | 4/50 [00:00<00:01, 30.53 it/sec, feas=True, obj=-2]
INFO - 16:23:42: 10%|█ | 5/50 [00:00<00:01, 30.22 it/sec, feas=True, obj=-2.03]
INFO - 16:23:42: 12%|█▏ | 6/50 [00:00<00:01, 30.09 it/sec, feas=True, obj=-2.03]
INFO - 16:23:42: 14%|█▍ | 7/50 [00:00<00:01, 30.01 it/sec, feas=True, obj=-2.03]
INFO - 16:23:42: 16%|█▌ | 8/50 [00:00<00:01, 29.78 it/sec, feas=True, obj=-2.03]
INFO - 16:23:42: Optimization result:
INFO - 16:23:42: Optimizer info:
INFO - 16:23:42: Status: 8
INFO - 16:23:42: Message: Positive directional derivative for linesearch
INFO - 16:23:42: Solution:
INFO - 16:23:42: The solution is feasible.
INFO - 16:23:42: Objective: -2.0304374059020165
INFO - 16:23:42: Standardized constraints:
INFO - 16:23:42: g_1 = [ 0. -0.00463878 -0.01646863 -0.02660989 -0.03463878 -0.2253965
INFO - 16:23:42: -0.0146035 ]
INFO - 16:23:42: Design space:
INFO - 16:23:42: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:42: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:42: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:42: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:42: | x_1[1] | 0.75 | 0.8257665790570363 | 1.25 | float |
INFO - 16:23:42: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:42: *** End StructureScenario execution (time: 0:00:00.270916) ***
INFO - 16:23:42: *** Start PropulsionScenario execution ***
INFO - 16:23:42: PropulsionScenario
INFO - 16:23:42: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:42: MDO formulation: MDF
INFO - 16:23:42: Optimization problem:
INFO - 16:23:42: minimize 0.001*-y_4(x_3)
INFO - 16:23:42: with respect to x_3
INFO - 16:23:42: under the inequality constraints
INFO - 16:23:42: g_3(x_3) <= 0
INFO - 16:23:42: over the design space:
INFO - 16:23:42: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:42: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:42: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:42: | x_3 | 0.1 | 0.1639712244856577 | 1 | float |
INFO - 16:23:42: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:42: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:42: 2%|▏ | 1/50 [00:00<00:00, 108.31 it/sec, feas=True, obj=-2.03]
INFO - 16:23:42: Optimization result:
INFO - 16:23:42: Optimizer info:
INFO - 16:23:42: Status: 8
INFO - 16:23:42: Message: Positive directional derivative for linesearch
INFO - 16:23:42: Solution:
INFO - 16:23:42: The solution is feasible.
INFO - 16:23:42: Objective: -2.0304374059020165
INFO - 16:23:42: Standardized constraints:
INFO - 16:23:42: g_3 = [-8.53030466e-01 -1.46969534e-01 2.22044605e-16 -1.82328530e-01]
INFO - 16:23:42: Design space:
INFO - 16:23:42: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:42: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:42: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:42: | x_3 | 0.1 | 0.1639712244856577 | 1 | float |
INFO - 16:23:42: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:42: *** End PropulsionScenario execution (time: 0:00:00.011083) ***
INFO - 16:23:42: *** Start AerodynamicsScenario execution ***
INFO - 16:23:42: AerodynamicsScenario
INFO - 16:23:42: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:42: MDO formulation: MDF
INFO - 16:23:42: Optimization problem:
INFO - 16:23:42: minimize 0.001*-y_4(x_2)
INFO - 16:23:42: with respect to x_2
INFO - 16:23:42: under the inequality constraints
INFO - 16:23:42: g_2(x_2) <= 0
INFO - 16:23:42: over the design space:
INFO - 16:23:42: +------+-------------+-------+-------------+-------+
INFO - 16:23:42: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:42: +------+-------------+-------+-------------+-------+
INFO - 16:23:42: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:42: +------+-------------+-------+-------------+-------+
INFO - 16:23:42: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:42: 2%|▏ | 1/50 [00:00<00:00, 109.10 it/sec, feas=True, obj=-2.03]
INFO - 16:23:42: Optimization result:
INFO - 16:23:42: Optimizer info:
INFO - 16:23:42: Status: 8
INFO - 16:23:42: Message: Positive directional derivative for linesearch
INFO - 16:23:42: Solution:
INFO - 16:23:42: The solution is feasible.
INFO - 16:23:42: Objective: -2.0304374059020165
INFO - 16:23:42: Standardized constraints:
INFO - 16:23:42: g_2 = -0.005041321670290921
INFO - 16:23:42: Design space:
INFO - 16:23:42: +------+-------------+-------+-------------+-------+
INFO - 16:23:42: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:42: +------+-------------+-------+-------------+-------+
INFO - 16:23:42: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:42: +------+-------------+-------+-------------+-------+
INFO - 16:23:42: *** End AerodynamicsScenario execution (time: 0:00:00.010876) ***
INFO - 16:23:42: *** Start StructureScenario execution ***
INFO - 16:23:42: StructureScenario
INFO - 16:23:42: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:42: MDO formulation: MDF
INFO - 16:23:42: Optimization problem:
INFO - 16:23:42: minimize 0.001*-y_4(x_1)
INFO - 16:23:42: with respect to x_1
INFO - 16:23:42: under the inequality constraints
INFO - 16:23:42: g_1(x_1) <= 0
INFO - 16:23:42: over the design space:
INFO - 16:23:42: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:42: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:42: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:42: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:42: | x_1[1] | 0.75 | 0.8257665790570363 | 1.25 | float |
INFO - 16:23:42: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:42: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:42: 2%|▏ | 1/50 [00:00<00:00, 102.64 it/sec, feas=True, obj=-2.03]
INFO - 16:23:42: Optimization result:
INFO - 16:23:42: Optimizer info:
INFO - 16:23:42: Status: 8
INFO - 16:23:42: Message: Positive directional derivative for linesearch
INFO - 16:23:42: Solution:
INFO - 16:23:42: The solution is feasible.
INFO - 16:23:42: Objective: -2.0304374059020165
INFO - 16:23:42: Standardized constraints:
INFO - 16:23:42: g_1 = [ 0. -0.00463878 -0.01646863 -0.02660989 -0.03463878 -0.2253965
INFO - 16:23:42: -0.0146035 ]
INFO - 16:23:42: Design space:
INFO - 16:23:42: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:42: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:42: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:42: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:42: | x_1[1] | 0.75 | 0.8257665790570363 | 1.25 | float |
INFO - 16:23:42: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:42: *** End StructureScenario execution (time: 0:00:00.011716) ***
INFO - 16:23:42: 31%|███ | 31/100 [00:25<00:56, 1.23 it/sec, feas=True, obj=-2.03]
INFO - 16:23:42: *** Start PropulsionScenario execution ***
INFO - 16:23:42: PropulsionScenario
INFO - 16:23:42: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:42: MDO formulation: MDF
INFO - 16:23:42: Optimization problem:
INFO - 16:23:42: minimize 0.001*-y_4(x_3)
INFO - 16:23:42: with respect to x_3
INFO - 16:23:42: under the inequality constraints
INFO - 16:23:42: g_3(x_3) <= 0
INFO - 16:23:42: over the design space:
INFO - 16:23:42: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:42: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:42: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:42: | x_3 | 0.1 | 0.1639712244856577 | 1 | float |
INFO - 16:23:42: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:42: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:42: 2%|▏ | 1/50 [00:00<00:01, 43.87 it/sec, feas=False, obj=-2.04]
INFO - 16:23:42: 4%|▍ | 2/50 [00:00<00:01, 46.62 it/sec, feas=True, obj=-2.03]
INFO - 16:23:42: 6%|▌ | 3/50 [00:00<00:01, 38.00 it/sec, feas=False, obj=-2.03]
INFO - 16:23:42: 8%|▊ | 4/50 [00:00<00:01, 34.70 it/sec, feas=True, obj=-2.03]
INFO - 16:23:42: 10%|█ | 5/50 [00:00<00:01, 32.96 it/sec, feas=True, obj=-2.03]
INFO - 16:23:42: Optimization result:
INFO - 16:23:42: Optimizer info:
INFO - 16:23:42: Status: 8
INFO - 16:23:42: Message: Positive directional derivative for linesearch
INFO - 16:23:42: Solution:
INFO - 16:23:42: The solution is feasible.
INFO - 16:23:42: Objective: -2.027574099735244
INFO - 16:23:42: Standardized constraints:
INFO - 16:23:42: g_3 = [-0.91798843 -0.08201157 0. -0.18155825]
INFO - 16:23:42: Design space:
INFO - 16:23:42: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:42: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:42: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:42: | x_3 | 0.1 | 0.1580559135944425 | 1 | float |
INFO - 16:23:42: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:42: *** End PropulsionScenario execution (time: 0:00:00.153737) ***
INFO - 16:23:42: *** Start AerodynamicsScenario execution ***
INFO - 16:23:42: AerodynamicsScenario
INFO - 16:23:42: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:42: MDO formulation: MDF
INFO - 16:23:42: Optimization problem:
INFO - 16:23:42: minimize 0.001*-y_4(x_2)
INFO - 16:23:42: with respect to x_2
INFO - 16:23:42: under the inequality constraints
INFO - 16:23:42: g_2(x_2) <= 0
INFO - 16:23:42: over the design space:
INFO - 16:23:42: +------+-------------+-------+-------------+-------+
INFO - 16:23:42: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:42: +------+-------------+-------+-------------+-------+
INFO - 16:23:42: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:42: +------+-------------+-------+-------------+-------+
INFO - 16:23:42: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:42: 2%|▏ | 1/50 [00:00<00:00, 104.93 it/sec, feas=True, obj=-2.03]
INFO - 16:23:42: Optimization result:
INFO - 16:23:42: Optimizer info:
INFO - 16:23:42: Status: 8
INFO - 16:23:42: Message: Positive directional derivative for linesearch
INFO - 16:23:42: Solution:
INFO - 16:23:42: The solution is feasible.
INFO - 16:23:42: Objective: -2.027574099735244
INFO - 16:23:42: Standardized constraints:
INFO - 16:23:42: g_2 = -0.021797048634677685
INFO - 16:23:42: Design space:
INFO - 16:23:42: +------+-------------+-------+-------------+-------+
INFO - 16:23:42: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:42: +------+-------------+-------+-------------+-------+
INFO - 16:23:42: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:42: +------+-------------+-------+-------------+-------+
INFO - 16:23:42: *** End AerodynamicsScenario execution (time: 0:00:00.011128) ***
INFO - 16:23:42: *** Start StructureScenario execution ***
INFO - 16:23:42: StructureScenario
INFO - 16:23:42: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:42: MDO formulation: MDF
INFO - 16:23:42: Optimization problem:
INFO - 16:23:42: minimize 0.001*-y_4(x_1)
INFO - 16:23:42: with respect to x_1
INFO - 16:23:42: under the inequality constraints
INFO - 16:23:42: g_1(x_1) <= 0
INFO - 16:23:42: over the design space:
INFO - 16:23:42: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:42: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:42: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:42: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:42: | x_1[1] | 0.75 | 0.8257665790570363 | 1.25 | float |
INFO - 16:23:42: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:42: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:42: 2%|▏ | 1/50 [00:00<00:00, 96.41 it/sec, feas=False, obj=-2.03]
WARNING - 16:23:42: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 1.0109921428344855 is still above the tolerance 1e-06.
INFO - 16:23:42: 4%|▍ | 2/50 [00:00<00:01, 34.10 it/sec, feas=True, obj=-1.9]
WARNING - 16:23:42: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 0.023809991458310725 is still above the tolerance 1e-06.
INFO - 16:23:42: 6%|▌ | 3/50 [00:00<00:01, 28.25 it/sec, feas=True, obj=-1.92]
WARNING - 16:23:42: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 0.021066085763964765 is still above the tolerance 1e-06.
INFO - 16:23:42: 8%|▊ | 4/50 [00:00<00:01, 25.93 it/sec, feas=True, obj=-1.92]
WARNING - 16:23:42: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 0.022894265734702636 is still above the tolerance 1e-06.
INFO - 16:23:42: 10%|█ | 5/50 [00:00<00:01, 24.76 it/sec, feas=True, obj=-1.92]
WARNING - 16:23:42: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 0.02014645019157726 is still above the tolerance 1e-06.
INFO - 16:23:42: 12%|█▏ | 6/50 [00:00<00:01, 24.06 it/sec, feas=True, obj=-1.92]
WARNING - 16:23:42: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 0.02014645019157726 is still above the tolerance 1e-06.
INFO - 16:23:42: 14%|█▍ | 7/50 [00:00<00:01, 24.79 it/sec, feas=True, obj=-1.92]
INFO - 16:23:42: Optimization result:
INFO - 16:23:42: Optimizer info:
INFO - 16:23:42: Status: None
INFO - 16:23:42: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:42: Solution:
INFO - 16:23:42: The solution is feasible.
INFO - 16:23:42: Objective: -1.9210342398497682
INFO - 16:23:42: Standardized constraints:
INFO - 16:23:42: g_1 = [ 5.20317123e-12 -1.49594419e-02 -2.80793721e-02 -3.77561972e-02
INFO - 16:23:42: -4.49594419e-02 -1.70387492e-01 -6.96125075e-02]
INFO - 16:23:42: Design space:
INFO - 16:23:42: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:42: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:42: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:42: | x_1[0] | 0.1 | 0.1000000000000112 | 0.4 | float |
INFO - 16:23:42: | x_1[1] | 0.75 | 0.9636317825762303 | 1.25 | float |
INFO - 16:23:42: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:42: *** End StructureScenario execution (time: 0:00:00.284822) ***
INFO - 16:23:42: *** Start PropulsionScenario execution ***
INFO - 16:23:42: PropulsionScenario
INFO - 16:23:42: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:42: MDO formulation: MDF
INFO - 16:23:42: Optimization problem:
INFO - 16:23:42: minimize 0.001*-y_4(x_3)
INFO - 16:23:42: with respect to x_3
INFO - 16:23:42: under the inequality constraints
INFO - 16:23:42: g_3(x_3) <= 0
INFO - 16:23:42: over the design space:
INFO - 16:23:42: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:42: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:42: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:42: | x_3 | 0.1 | 0.1580559135944425 | 1 | float |
INFO - 16:23:42: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:42: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:42: 2%|▏ | 1/50 [00:00<00:00, 77.23 it/sec, feas=True, obj=-1.92]
INFO - 16:23:42: Optimization result:
INFO - 16:23:42: Optimizer info:
INFO - 16:23:42: Status: 8
INFO - 16:23:42: Message: Positive directional derivative for linesearch
INFO - 16:23:42: Solution:
INFO - 16:23:42: The solution is feasible.
INFO - 16:23:42: Objective: -1.9210342398497666
INFO - 16:23:42: Standardized constraints:
INFO - 16:23:42: g_3 = [-0.91665136 -0.08334864 0. -0.18155825]
INFO - 16:23:42: Design space:
INFO - 16:23:42: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:42: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:42: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:42: | x_3 | 0.1 | 0.1580559135944425 | 1 | float |
INFO - 16:23:42: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:42: *** End PropulsionScenario execution (time: 0:00:00.014849) ***
INFO - 16:23:42: *** Start AerodynamicsScenario execution ***
INFO - 16:23:42: AerodynamicsScenario
INFO - 16:23:42: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:42: MDO formulation: MDF
INFO - 16:23:42: Optimization problem:
INFO - 16:23:42: minimize 0.001*-y_4(x_2)
INFO - 16:23:42: with respect to x_2
INFO - 16:23:42: under the inequality constraints
INFO - 16:23:42: g_2(x_2) <= 0
INFO - 16:23:42: over the design space:
INFO - 16:23:42: +------+-------------+-------+-------------+-------+
INFO - 16:23:42: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:42: +------+-------------+-------+-------------+-------+
INFO - 16:23:42: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:42: +------+-------------+-------+-------------+-------+
INFO - 16:23:42: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:42: 2%|▏ | 1/50 [00:00<00:00, 109.41 it/sec, feas=True, obj=-1.92]
INFO - 16:23:42: Optimization result:
INFO - 16:23:42: Optimizer info:
INFO - 16:23:42: Status: 8
INFO - 16:23:42: Message: Positive directional derivative for linesearch
INFO - 16:23:42: Solution:
INFO - 16:23:42: The solution is feasible.
INFO - 16:23:42: Objective: -1.9210342398497666
INFO - 16:23:42: Standardized constraints:
INFO - 16:23:42: g_2 = -0.021797048634677685
INFO - 16:23:42: Design space:
INFO - 16:23:42: +------+-------------+-------+-------------+-------+
INFO - 16:23:42: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:42: +------+-------------+-------+-------------+-------+
INFO - 16:23:42: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:42: +------+-------------+-------+-------------+-------+
INFO - 16:23:42: *** End AerodynamicsScenario execution (time: 0:00:00.010861) ***
INFO - 16:23:42: *** Start StructureScenario execution ***
INFO - 16:23:42: StructureScenario
INFO - 16:23:42: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:42: MDO formulation: MDF
INFO - 16:23:42: Optimization problem:
INFO - 16:23:42: minimize 0.001*-y_4(x_1)
INFO - 16:23:42: with respect to x_1
INFO - 16:23:42: under the inequality constraints
INFO - 16:23:42: g_1(x_1) <= 0
INFO - 16:23:42: over the design space:
INFO - 16:23:42: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:42: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:42: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:42: | x_1[0] | 0.1 | 0.1000000000000112 | 0.4 | float |
INFO - 16:23:42: | x_1[1] | 0.75 | 0.9636317825762303 | 1.25 | float |
INFO - 16:23:42: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:42: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:42: 2%|▏ | 1/50 [00:00<00:00, 102.69 it/sec, feas=True, obj=-1.92]
INFO - 16:23:42: 4%|▍ | 2/50 [00:00<00:00, 53.49 it/sec, feas=True, obj=-1.92]
INFO - 16:23:42: 6%|▌ | 3/50 [00:00<00:00, 61.61 it/sec, feas=True, obj=-1.92]
INFO - 16:23:42: Optimization result:
INFO - 16:23:42: Optimizer info:
INFO - 16:23:42: Status: None
INFO - 16:23:42: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:42: Solution:
INFO - 16:23:42: The solution is feasible.
INFO - 16:23:42: Objective: -1.9210342398497666
INFO - 16:23:42: Standardized constraints:
INFO - 16:23:42: g_1 = [ 5.20317123e-12 -1.49594419e-02 -2.80793721e-02 -3.77561972e-02
INFO - 16:23:42: -4.49594419e-02 -1.70387492e-01 -6.96125075e-02]
INFO - 16:23:42: Design space:
INFO - 16:23:42: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:42: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:42: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:42: | x_1[0] | 0.1 | 0.1000000000000112 | 0.4 | float |
INFO - 16:23:42: | x_1[1] | 0.75 | 0.9636317825762303 | 1.25 | float |
INFO - 16:23:42: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:42: *** End StructureScenario execution (time: 0:00:00.051111) ***
INFO - 16:23:42: 32%|███▏ | 32/100 [00:25<00:54, 1.24 it/sec, feas=True, obj=-1.92]
INFO - 16:23:42: *** Start PropulsionScenario execution ***
INFO - 16:23:42: PropulsionScenario
INFO - 16:23:42: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:42: MDO formulation: MDF
INFO - 16:23:42: Optimization problem:
INFO - 16:23:42: minimize 0.001*-y_4(x_3)
INFO - 16:23:42: with respect to x_3
INFO - 16:23:42: under the inequality constraints
INFO - 16:23:42: g_3(x_3) <= 0
INFO - 16:23:42: over the design space:
INFO - 16:23:42: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:42: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:42: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:42: | x_3 | 0.1 | 0.1580559135944425 | 1 | float |
INFO - 16:23:42: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:42: Solving optimization problem with algorithm SLSQP:
WARNING - 16:23:42: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 0.0010759891946573801 is still above the tolerance 1e-06.
INFO - 16:23:42: 2%|▏ | 1/50 [00:00<00:01, 33.39 it/sec, feas=True, obj=-2.04]
WARNING - 16:23:42: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 0.0010760548658221801 is still above the tolerance 1e-06.
INFO - 16:23:42: 4%|▍ | 2/50 [00:00<00:01, 25.19 it/sec, feas=True, obj=-2.04]
INFO - 16:23:42: Optimization result:
INFO - 16:23:42: Optimizer info:
INFO - 16:23:42: Status: 8
INFO - 16:23:42: Message: Positive directional derivative for linesearch
INFO - 16:23:42: Solution:
INFO - 16:23:42: The solution is feasible.
INFO - 16:23:42: Objective: -2.043703600544774
INFO - 16:23:42: Standardized constraints:
INFO - 16:23:42: g_3 = [-0.83484031 -0.16515969 0. -0.18055566]
INFO - 16:23:42: Design space:
INFO - 16:23:42: +------+-------------+-------------------+-------------+-------+
INFO - 16:23:42: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:42: +------+-------------+-------------------+-------------+-------+
INFO - 16:23:42: | x_3 | 0.1 | 0.159310949014251 | 1 | float |
INFO - 16:23:42: +------+-------------+-------------------+-------------+-------+
INFO - 16:23:42: *** End PropulsionScenario execution (time: 0:00:00.081491) ***
INFO - 16:23:42: *** Start AerodynamicsScenario execution ***
INFO - 16:23:42: AerodynamicsScenario
INFO - 16:23:42: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:42: MDO formulation: MDF
INFO - 16:23:42: Optimization problem:
INFO - 16:23:42: minimize 0.001*-y_4(x_2)
INFO - 16:23:42: with respect to x_2
INFO - 16:23:42: under the inequality constraints
INFO - 16:23:42: g_2(x_2) <= 0
INFO - 16:23:42: over the design space:
INFO - 16:23:42: +------+-------------+-------+-------------+-------+
INFO - 16:23:42: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:42: +------+-------------+-------+-------------+-------+
INFO - 16:23:42: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:42: +------+-------------+-------+-------------+-------+
INFO - 16:23:42: Solving optimization problem with algorithm SLSQP:
WARNING - 16:23:42: Optimization found no feasible point; the least infeasible point is selected.
INFO - 16:23:42: 2%|▏ | 1/50 [00:00<00:00, 73.22 it/sec, feas=False, obj=-2.04]
INFO - 16:23:42: Optimization result:
INFO - 16:23:42: Optimizer info:
INFO - 16:23:42: Status: 8
INFO - 16:23:42: Message: Positive directional derivative for linesearch
INFO - 16:23:42: Solution:
WARNING - 16:23:42: The solution is not feasible.
INFO - 16:23:42: Objective: -2.043703600544775
INFO - 16:23:42: Standardized constraints:
INFO - 16:23:42: g_2 = 0.003028135633228457
INFO - 16:23:42: Design space:
INFO - 16:23:42: +------+-------------+-------+-------------+-------+
INFO - 16:23:42: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:42: +------+-------------+-------+-------------+-------+
INFO - 16:23:42: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:42: +------+-------------+-------+-------------+-------+
INFO - 16:23:42: *** End AerodynamicsScenario execution (time: 0:00:00.015361) ***
INFO - 16:23:42: *** Start StructureScenario execution ***
INFO - 16:23:42: StructureScenario
INFO - 16:23:42: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:42: MDO formulation: MDF
INFO - 16:23:42: Optimization problem:
INFO - 16:23:42: minimize 0.001*-y_4(x_1)
INFO - 16:23:42: with respect to x_1
INFO - 16:23:42: under the inequality constraints
INFO - 16:23:42: g_1(x_1) <= 0
INFO - 16:23:42: over the design space:
INFO - 16:23:42: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:42: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:42: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:42: | x_1[0] | 0.1 | 0.1000000000000112 | 0.4 | float |
INFO - 16:23:42: | x_1[1] | 0.75 | 0.9636317825762303 | 1.25 | float |
INFO - 16:23:42: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:42: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:42: 2%|▏ | 1/50 [00:00<00:00, 97.66 it/sec, feas=True, obj=-2.04]
INFO - 16:23:42: 4%|▍ | 2/50 [00:00<00:01, 39.30 it/sec, feas=True, obj=-2.2]
INFO - 16:23:42: 6%|▌ | 3/50 [00:00<00:01, 32.18 it/sec, feas=True, obj=-2.23]
INFO - 16:23:42: 8%|▊ | 4/50 [00:00<00:01, 29.31 it/sec, feas=True, obj=-2.23]
INFO - 16:23:43: 10%|█ | 5/50 [00:00<00:01, 27.94 it/sec, feas=True, obj=-2.23]
INFO - 16:23:43: 12%|█▏ | 6/50 [00:00<00:01, 29.27 it/sec, feas=True, obj=-2.23]
INFO - 16:23:43: 14%|█▍ | 7/50 [00:00<00:01, 30.11 it/sec, feas=True, obj=-2.23]
INFO - 16:23:43: Optimization result:
INFO - 16:23:43: Optimizer info:
INFO - 16:23:43: Status: None
INFO - 16:23:43: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:43: Solution:
INFO - 16:23:43: The solution is feasible.
INFO - 16:23:43: Objective: -2.2273479872973296
INFO - 16:23:43: Standardized constraints:
INFO - 16:23:43: g_1 = [-2.61494710e-02 -1.54648353e-02 -2.21105719e-02 -2.99341914e-02
INFO - 16:23:43: -3.67483450e-02 -2.40000000e-01 4.91662266e-12]
INFO - 16:23:43: Design space:
INFO - 16:23:43: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:43: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:43: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:43: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:43: | x_1[1] | 0.75 | 0.7806436836608989 | 1.25 | float |
INFO - 16:23:43: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:43: *** End StructureScenario execution (time: 0:00:00.235234) ***
INFO - 16:23:43: *** Start PropulsionScenario execution ***
INFO - 16:23:43: PropulsionScenario
INFO - 16:23:43: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:43: MDO formulation: MDF
INFO - 16:23:43: Optimization problem:
INFO - 16:23:43: minimize 0.001*-y_4(x_3)
INFO - 16:23:43: with respect to x_3
INFO - 16:23:43: under the inequality constraints
INFO - 16:23:43: g_3(x_3) <= 0
INFO - 16:23:43: over the design space:
INFO - 16:23:43: +------+-------------+-------------------+-------------+-------+
INFO - 16:23:43: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:43: +------+-------------+-------------------+-------------+-------+
INFO - 16:23:43: | x_3 | 0.1 | 0.159310949014251 | 1 | float |
INFO - 16:23:43: +------+-------------+-------------------+-------------+-------+
INFO - 16:23:43: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:43: 2%|▏ | 1/50 [00:00<00:00, 89.68 it/sec, feas=True, obj=-2.23]
INFO - 16:23:43: Optimization result:
INFO - 16:23:43: Optimizer info:
INFO - 16:23:43: Status: 8
INFO - 16:23:43: Message: Positive directional derivative for linesearch
INFO - 16:23:43: Solution:
INFO - 16:23:43: The solution is feasible.
INFO - 16:23:43: Objective: -2.2273479872973296
INFO - 16:23:43: Standardized constraints:
INFO - 16:23:43: g_3 = [-0.83634294 -0.16365706 0. -0.18055566]
INFO - 16:23:43: Design space:
INFO - 16:23:43: +------+-------------+-------------------+-------------+-------+
INFO - 16:23:43: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:43: +------+-------------+-------------------+-------------+-------+
INFO - 16:23:43: | x_3 | 0.1 | 0.159310949014251 | 1 | float |
INFO - 16:23:43: +------+-------------+-------------------+-------------+-------+
INFO - 16:23:43: *** End PropulsionScenario execution (time: 0:00:00.013124) ***
INFO - 16:23:43: *** Start AerodynamicsScenario execution ***
INFO - 16:23:43: AerodynamicsScenario
INFO - 16:23:43: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:43: MDO formulation: MDF
INFO - 16:23:43: Optimization problem:
INFO - 16:23:43: minimize 0.001*-y_4(x_2)
INFO - 16:23:43: with respect to x_2
INFO - 16:23:43: under the inequality constraints
INFO - 16:23:43: g_2(x_2) <= 0
INFO - 16:23:43: over the design space:
INFO - 16:23:43: +------+-------------+-------+-------------+-------+
INFO - 16:23:43: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:43: +------+-------------+-------+-------------+-------+
INFO - 16:23:43: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:43: +------+-------------+-------+-------------+-------+
INFO - 16:23:43: Solving optimization problem with algorithm SLSQP:
WARNING - 16:23:43: Optimization found no feasible point; the least infeasible point is selected.
INFO - 16:23:43: 2%|▏ | 1/50 [00:00<00:00, 105.82 it/sec, feas=False, obj=-2.23]
INFO - 16:23:43: Optimization result:
INFO - 16:23:43: Optimizer info:
INFO - 16:23:43: Status: 8
INFO - 16:23:43: Message: Positive directional derivative for linesearch
INFO - 16:23:43: Solution:
WARNING - 16:23:43: The solution is not feasible.
INFO - 16:23:43: Objective: -2.2273479872973296
INFO - 16:23:43: Standardized constraints:
INFO - 16:23:43: g_2 = 0.003028135633228457
INFO - 16:23:43: Design space:
INFO - 16:23:43: +------+-------------+-------+-------------+-------+
INFO - 16:23:43: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:43: +------+-------------+-------+-------------+-------+
INFO - 16:23:43: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:43: +------+-------------+-------+-------------+-------+
INFO - 16:23:43: *** End AerodynamicsScenario execution (time: 0:00:00.011144) ***
INFO - 16:23:43: *** Start StructureScenario execution ***
INFO - 16:23:43: StructureScenario
INFO - 16:23:43: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:43: MDO formulation: MDF
INFO - 16:23:43: Optimization problem:
INFO - 16:23:43: minimize 0.001*-y_4(x_1)
INFO - 16:23:43: with respect to x_1
INFO - 16:23:43: under the inequality constraints
INFO - 16:23:43: g_1(x_1) <= 0
INFO - 16:23:43: over the design space:
INFO - 16:23:43: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:43: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:43: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:43: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:43: | x_1[1] | 0.75 | 0.7806436836608989 | 1.25 | float |
INFO - 16:23:43: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:43: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:43: 2%|▏ | 1/50 [00:00<00:00, 101.39 it/sec, feas=True, obj=-2.23]
INFO - 16:23:43: Optimization result:
INFO - 16:23:43: Optimizer info:
INFO - 16:23:43: Status: 8
INFO - 16:23:43: Message: Positive directional derivative for linesearch
INFO - 16:23:43: Solution:
INFO - 16:23:43: The solution is feasible.
INFO - 16:23:43: Objective: -2.2273479872973296
INFO - 16:23:43: Standardized constraints:
INFO - 16:23:43: g_1 = [-2.61494710e-02 -1.54648353e-02 -2.21105719e-02 -2.99341914e-02
INFO - 16:23:43: -3.67483450e-02 -2.40000000e-01 4.91662266e-12]
INFO - 16:23:43: Design space:
INFO - 16:23:43: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:43: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:43: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:43: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:43: | x_1[1] | 0.75 | 0.7806436836608989 | 1.25 | float |
INFO - 16:23:43: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:43: *** End StructureScenario execution (time: 0:00:00.011861) ***
INFO - 16:23:43: 33%|███▎ | 33/100 [00:26<00:53, 1.26 it/sec, feas=False, obj=-2.23]
INFO - 16:23:43: *** Start PropulsionScenario execution ***
INFO - 16:23:43: PropulsionScenario
INFO - 16:23:43: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:43: MDO formulation: MDF
INFO - 16:23:43: Optimization problem:
INFO - 16:23:43: minimize 0.001*-y_4(x_3)
INFO - 16:23:43: with respect to x_3
INFO - 16:23:43: under the inequality constraints
INFO - 16:23:43: g_3(x_3) <= 0
INFO - 16:23:43: over the design space:
INFO - 16:23:43: +------+-------------+-------------------+-------------+-------+
INFO - 16:23:43: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:43: +------+-------------+-------------------+-------------+-------+
INFO - 16:23:43: | x_3 | 0.1 | 0.159310949014251 | 1 | float |
INFO - 16:23:43: +------+-------------+-------------------+-------------+-------+
INFO - 16:23:43: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:43: 2%|▏ | 1/50 [00:00<00:01, 37.76 it/sec, feas=True, obj=-2.07]
INFO - 16:23:43: 4%|▍ | 2/50 [00:00<00:01, 28.72 it/sec, feas=True, obj=-2.08]
INFO - 16:23:43: 6%|▌ | 3/50 [00:00<00:01, 26.94 it/sec, feas=True, obj=-2.08]
INFO - 16:23:43: 8%|▊ | 4/50 [00:00<00:01, 28.49 it/sec, feas=True, obj=-2.08]
INFO - 16:23:43: Optimization result:
INFO - 16:23:43: Optimizer info:
INFO - 16:23:43: Status: None
INFO - 16:23:43: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:43: Solution:
INFO - 16:23:43: The solution is feasible.
INFO - 16:23:43: Objective: -2.080830324295749
INFO - 16:23:43: Standardized constraints:
INFO - 16:23:43: g_3 = [-8.35391342e-01 -1.64608658e-01 -2.22044605e-16 -1.82400511e-01]
INFO - 16:23:43: Design space:
INFO - 16:23:43: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:43: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:43: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:43: | x_3 | 0.1 | 0.1650013694036327 | 1 | float |
INFO - 16:23:43: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:43: *** End PropulsionScenario execution (time: 0:00:00.143102) ***
INFO - 16:23:43: *** Start AerodynamicsScenario execution ***
INFO - 16:23:43: AerodynamicsScenario
INFO - 16:23:43: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:43: MDO formulation: MDF
INFO - 16:23:43: Optimization problem:
INFO - 16:23:43: minimize 0.001*-y_4(x_2)
INFO - 16:23:43: with respect to x_2
INFO - 16:23:43: under the inequality constraints
INFO - 16:23:43: g_2(x_2) <= 0
INFO - 16:23:43: over the design space:
INFO - 16:23:43: +------+-------------+-------+-------------+-------+
INFO - 16:23:43: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:43: +------+-------------+-------+-------------+-------+
INFO - 16:23:43: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:43: +------+-------------+-------+-------------+-------+
INFO - 16:23:43: Solving optimization problem with algorithm SLSQP:
WARNING - 16:23:43: Optimization found no feasible point; the least infeasible point is selected.
INFO - 16:23:43: 2%|▏ | 1/50 [00:00<00:00, 63.50 it/sec, feas=False, obj=-2.08]
INFO - 16:23:43: Optimization result:
INFO - 16:23:43: Optimizer info:
INFO - 16:23:43: Status: 8
INFO - 16:23:43: Message: Positive directional derivative for linesearch
INFO - 16:23:43: Solution:
WARNING - 16:23:43: The solution is not feasible.
INFO - 16:23:43: Objective: -2.080830324295749
INFO - 16:23:43: Standardized constraints:
INFO - 16:23:43: g_2 = 0.002227736507804723
INFO - 16:23:43: Design space:
INFO - 16:23:43: +------+-------------+-------+-------------+-------+
INFO - 16:23:43: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:43: +------+-------------+-------+-------------+-------+
INFO - 16:23:43: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:43: +------+-------------+-------+-------------+-------+
INFO - 16:23:43: *** End AerodynamicsScenario execution (time: 0:00:00.017604) ***
INFO - 16:23:43: *** Start StructureScenario execution ***
INFO - 16:23:43: StructureScenario
INFO - 16:23:43: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:43: MDO formulation: MDF
INFO - 16:23:43: Optimization problem:
INFO - 16:23:43: minimize 0.001*-y_4(x_1)
INFO - 16:23:43: with respect to x_1
INFO - 16:23:43: under the inequality constraints
INFO - 16:23:43: g_1(x_1) <= 0
INFO - 16:23:43: over the design space:
INFO - 16:23:43: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:43: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:43: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:43: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:43: | x_1[1] | 0.75 | 0.7806436836608989 | 1.25 | float |
INFO - 16:23:43: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:43: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:43: 2%|▏ | 1/50 [00:00<00:00, 92.08 it/sec, feas=True, obj=-2.08]
INFO - 16:23:43: Optimization result:
INFO - 16:23:43: Optimizer info:
INFO - 16:23:43: Status: 8
INFO - 16:23:43: Message: Positive directional derivative for linesearch
INFO - 16:23:43: Solution:
INFO - 16:23:43: The solution is feasible.
INFO - 16:23:43: Objective: -2.080830324295749
INFO - 16:23:43: Standardized constraints:
INFO - 16:23:43: g_1 = [-1.96037300e-02 -1.18886178e-02 -1.97237625e-02 -2.81665136e-02
INFO - 16:23:43: -3.53540411e-02 -2.40000000e-01 4.91662266e-12]
INFO - 16:23:43: Design space:
INFO - 16:23:43: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:43: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:43: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:43: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:43: | x_1[1] | 0.75 | 0.7806436836608989 | 1.25 | float |
INFO - 16:23:43: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:43: *** End StructureScenario execution (time: 0:00:00.013283) ***
INFO - 16:23:43: *** Start PropulsionScenario execution ***
INFO - 16:23:43: PropulsionScenario
INFO - 16:23:43: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:43: MDO formulation: MDF
INFO - 16:23:43: Optimization problem:
INFO - 16:23:43: minimize 0.001*-y_4(x_3)
INFO - 16:23:43: with respect to x_3
INFO - 16:23:43: under the inequality constraints
INFO - 16:23:43: g_3(x_3) <= 0
INFO - 16:23:43: over the design space:
INFO - 16:23:43: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:43: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:43: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:43: | x_3 | 0.1 | 0.1650013694036327 | 1 | float |
INFO - 16:23:43: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:43: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:43: 2%|▏ | 1/50 [00:00<00:00, 108.18 it/sec, feas=True, obj=-2.08]
INFO - 16:23:43: Optimization result:
INFO - 16:23:43: Optimizer info:
INFO - 16:23:43: Status: 8
INFO - 16:23:43: Message: Positive directional derivative for linesearch
INFO - 16:23:43: Solution:
INFO - 16:23:43: The solution is feasible.
INFO - 16:23:43: Objective: -2.080830324295749
INFO - 16:23:43: Standardized constraints:
INFO - 16:23:43: g_3 = [-8.35391342e-01 -1.64608658e-01 -2.22044605e-16 -1.82400511e-01]
INFO - 16:23:43: Design space:
INFO - 16:23:43: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:43: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:43: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:43: | x_3 | 0.1 | 0.1650013694036327 | 1 | float |
INFO - 16:23:43: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:43: *** End PropulsionScenario execution (time: 0:00:00.011204) ***
INFO - 16:23:43: *** Start AerodynamicsScenario execution ***
INFO - 16:23:43: AerodynamicsScenario
INFO - 16:23:43: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:43: MDO formulation: MDF
INFO - 16:23:43: Optimization problem:
INFO - 16:23:43: minimize 0.001*-y_4(x_2)
INFO - 16:23:43: with respect to x_2
INFO - 16:23:43: under the inequality constraints
INFO - 16:23:43: g_2(x_2) <= 0
INFO - 16:23:43: over the design space:
INFO - 16:23:43: +------+-------------+-------+-------------+-------+
INFO - 16:23:43: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:43: +------+-------------+-------+-------------+-------+
INFO - 16:23:43: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:43: +------+-------------+-------+-------------+-------+
INFO - 16:23:43: Solving optimization problem with algorithm SLSQP:
WARNING - 16:23:43: Optimization found no feasible point; the least infeasible point is selected.
INFO - 16:23:43: 2%|▏ | 1/50 [00:00<00:00, 88.70 it/sec, feas=False, obj=-2.08]
INFO - 16:23:43: Optimization result:
INFO - 16:23:43: Optimizer info:
INFO - 16:23:43: Status: 8
INFO - 16:23:43: Message: Positive directional derivative for linesearch
INFO - 16:23:43: Solution:
WARNING - 16:23:43: The solution is not feasible.
INFO - 16:23:43: Objective: -2.080830324295749
INFO - 16:23:43: Standardized constraints:
INFO - 16:23:43: g_2 = 0.002227736507804723
INFO - 16:23:43: Design space:
INFO - 16:23:43: +------+-------------+-------+-------------+-------+
INFO - 16:23:43: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:43: +------+-------------+-------+-------------+-------+
INFO - 16:23:43: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:43: +------+-------------+-------+-------------+-------+
INFO - 16:23:43: *** End AerodynamicsScenario execution (time: 0:00:00.012908) ***
INFO - 16:23:43: 34%|███▍ | 34/100 [00:26<00:51, 1.28 it/sec, feas=False, obj=-2.08]
INFO - 16:23:43: *** Start PropulsionScenario execution ***
INFO - 16:23:43: PropulsionScenario
INFO - 16:23:43: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:43: MDO formulation: MDF
INFO - 16:23:43: Optimization problem:
INFO - 16:23:43: minimize 0.001*-y_4(x_3)
INFO - 16:23:43: with respect to x_3
INFO - 16:23:43: under the inequality constraints
INFO - 16:23:43: g_3(x_3) <= 0
INFO - 16:23:43: over the design space:
INFO - 16:23:43: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:43: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:43: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:43: | x_3 | 0.1 | 0.1650013694036327 | 1 | float |
INFO - 16:23:43: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:43: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:43: 2%|▏ | 1/50 [00:00<00:01, 37.32 it/sec, feas=False, obj=-2.26]
WARNING - 16:23:43: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 6.724932466608626e-05 is still above the tolerance 1e-06.
INFO - 16:23:43: 4%|▍ | 2/50 [00:00<00:01, 34.93 it/sec, feas=True, obj=-2.24]
INFO - 16:23:43: 6%|▌ | 3/50 [00:00<00:01, 29.76 it/sec, feas=False, obj=-2.25]
INFO - 16:23:43: 8%|▊ | 4/50 [00:00<00:01, 27.41 it/sec, feas=True, obj=-2.24]
INFO - 16:23:43: Optimization result:
INFO - 16:23:43: Optimizer info:
INFO - 16:23:43: Status: 8
INFO - 16:23:43: Message: Positive directional derivative for linesearch
INFO - 16:23:43: Solution:
INFO - 16:23:43: The solution is feasible.
INFO - 16:23:43: Objective: -2.243451827353745
INFO - 16:23:43: Standardized constraints:
INFO - 16:23:43: g_3 = [-8.34008118e-01 -1.65991882e-01 5.99520433e-15 -1.81558251e-01]
INFO - 16:23:43: Design space:
INFO - 16:23:43: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:43: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:43: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:43: | x_3 | 0.1 | 0.1580559135944434 | 1 | float |
INFO - 16:23:43: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:43: *** End PropulsionScenario execution (time: 0:00:00.148032) ***
INFO - 16:23:43: *** Start AerodynamicsScenario execution ***
INFO - 16:23:43: AerodynamicsScenario
INFO - 16:23:43: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:43: MDO formulation: MDF
INFO - 16:23:43: Optimization problem:
INFO - 16:23:43: minimize 0.001*-y_4(x_2)
INFO - 16:23:43: with respect to x_2
INFO - 16:23:43: under the inequality constraints
INFO - 16:23:43: g_2(x_2) <= 0
INFO - 16:23:43: over the design space:
INFO - 16:23:43: +------+-------------+-------+-------------+-------+
INFO - 16:23:43: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:43: +------+-------------+-------+-------------+-------+
INFO - 16:23:43: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:43: +------+-------------+-------+-------------+-------+
INFO - 16:23:43: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:43: 2%|▏ | 1/50 [00:00<00:00, 76.88 it/sec, feas=True, obj=-2.24]
INFO - 16:23:43: Optimization result:
INFO - 16:23:43: Optimizer info:
INFO - 16:23:43: Status: 8
INFO - 16:23:43: Message: Positive directional derivative for linesearch
INFO - 16:23:43: Solution:
INFO - 16:23:43: The solution is feasible.
INFO - 16:23:43: Objective: -2.2434518273537445
INFO - 16:23:43: Standardized constraints:
INFO - 16:23:43: g_2 = -0.003475465313115933
INFO - 16:23:43: Design space:
INFO - 16:23:43: +------+-------------+-------+-------------+-------+
INFO - 16:23:43: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:43: +------+-------------+-------+-------------+-------+
INFO - 16:23:43: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:43: +------+-------------+-------+-------------+-------+
INFO - 16:23:43: *** End AerodynamicsScenario execution (time: 0:00:00.014733) ***
INFO - 16:23:43: *** Start StructureScenario execution ***
INFO - 16:23:43: StructureScenario
INFO - 16:23:43: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:43: MDO formulation: MDF
INFO - 16:23:43: Optimization problem:
INFO - 16:23:43: minimize 0.001*-y_4(x_1)
INFO - 16:23:43: with respect to x_1
INFO - 16:23:43: under the inequality constraints
INFO - 16:23:43: g_1(x_1) <= 0
INFO - 16:23:43: over the design space:
INFO - 16:23:43: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:43: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:43: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:43: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:43: | x_1[1] | 0.75 | 0.7806436836608989 | 1.25 | float |
INFO - 16:23:43: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:43: Solving optimization problem with algorithm SLSQP:
WARNING - 16:23:43: MDAGaussSeidel has reached its maximum number of unsuccessful iterations, but the normalized residual norm 0.0009157477359807847 is still above the tolerance 1e-06.
INFO - 16:23:43: 2%|▏ | 1/50 [00:00<00:00, 52.81 it/sec, feas=False, obj=-2.24]
INFO - 16:23:43: 4%|▍ | 2/50 [00:00<00:01, 34.75 it/sec, feas=True, obj=-2.2]
INFO - 16:23:43: 6%|▌ | 3/50 [00:00<00:01, 31.80 it/sec, feas=True, obj=-2.2]
INFO - 16:23:43: 8%|▊ | 4/50 [00:00<00:01, 30.20 it/sec, feas=True, obj=-2.2]
INFO - 16:23:43: 10%|█ | 5/50 [00:00<00:01, 29.56 it/sec, feas=True, obj=-2.2]
INFO - 16:23:43: 12%|█▏ | 6/50 [00:00<00:01, 29.16 it/sec, feas=True, obj=-2.2]
INFO - 16:23:43: Optimization result:
INFO - 16:23:43: Optimizer info:
INFO - 16:23:43: Status: None
INFO - 16:23:43: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:43: Solution:
INFO - 16:23:43: The solution is feasible.
INFO - 16:23:43: Objective: -2.200234902138859
INFO - 16:23:43: Standardized constraints:
INFO - 16:23:43: g_1 = [ 1.03961284e-12 -3.55526455e-03 -1.52496726e-02 -2.54396857e-02
INFO - 16:23:43: -3.35552645e-02 -2.30122617e-01 -9.87738314e-03]
INFO - 16:23:43: Design space:
INFO - 16:23:43: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:43: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:43: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:43: | x_1[0] | 0.1 | 0.1000000000000026 | 0.4 | float |
INFO - 16:23:43: | x_1[1] | 0.75 | 0.8114361865723931 | 1.25 | float |
INFO - 16:23:43: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:43: *** End StructureScenario execution (time: 0:00:00.208426) ***
INFO - 16:23:43: *** Start PropulsionScenario execution ***
INFO - 16:23:43: PropulsionScenario
INFO - 16:23:43: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:43: MDO formulation: MDF
INFO - 16:23:43: Optimization problem:
INFO - 16:23:43: minimize 0.001*-y_4(x_3)
INFO - 16:23:43: with respect to x_3
INFO - 16:23:43: under the inequality constraints
INFO - 16:23:43: g_3(x_3) <= 0
INFO - 16:23:43: over the design space:
INFO - 16:23:43: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:43: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:43: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:43: | x_3 | 0.1 | 0.1580559135944434 | 1 | float |
INFO - 16:23:43: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:43: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:43: 2%|▏ | 1/50 [00:00<00:00, 78.64 it/sec, feas=True, obj=-2.2]
INFO - 16:23:43: 4%|▍ | 2/50 [00:00<00:00, 122.49 it/sec, feas=True, obj=-2.2]
INFO - 16:23:43: 6%|▌ | 3/50 [00:00<00:00, 81.33 it/sec, feas=True, obj=-2.2]
INFO - 16:23:43: Optimization result:
INFO - 16:23:43: Optimizer info:
INFO - 16:23:43: Status: 8
INFO - 16:23:43: Message: Positive directional derivative for linesearch
INFO - 16:23:43: Solution:
INFO - 16:23:43: The solution is feasible.
INFO - 16:23:43: Objective: -2.200234902138859
INFO - 16:23:43: Standardized constraints:
INFO - 16:23:43: g_3 = [-8.33890339e-01 -1.66109661e-01 5.99520433e-15 -1.81558251e-01]
INFO - 16:23:43: Design space:
INFO - 16:23:43: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:43: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:43: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:43: | x_3 | 0.1 | 0.1580559135944434 | 1 | float |
INFO - 16:23:43: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:43: *** End PropulsionScenario execution (time: 0:00:00.038852) ***
INFO - 16:23:43: *** Start AerodynamicsScenario execution ***
INFO - 16:23:43: AerodynamicsScenario
INFO - 16:23:43: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:43: MDO formulation: MDF
INFO - 16:23:43: Optimization problem:
INFO - 16:23:43: minimize 0.001*-y_4(x_2)
INFO - 16:23:43: with respect to x_2
INFO - 16:23:43: under the inequality constraints
INFO - 16:23:43: g_2(x_2) <= 0
INFO - 16:23:43: over the design space:
INFO - 16:23:43: +------+-------------+-------+-------------+-------+
INFO - 16:23:43: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:43: +------+-------------+-------+-------------+-------+
INFO - 16:23:43: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:43: +------+-------------+-------+-------------+-------+
INFO - 16:23:43: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:43: 2%|▏ | 1/50 [00:00<00:00, 81.08 it/sec, feas=True, obj=-2.2]
INFO - 16:23:43: Optimization result:
INFO - 16:23:43: Optimizer info:
INFO - 16:23:43: Status: 8
INFO - 16:23:43: Message: Positive directional derivative for linesearch
INFO - 16:23:43: Solution:
INFO - 16:23:43: The solution is feasible.
INFO - 16:23:43: Objective: -2.200234902138859
INFO - 16:23:43: Standardized constraints:
INFO - 16:23:43: g_2 = -0.003475465313115933
INFO - 16:23:43: Design space:
INFO - 16:23:43: +------+-------------+-------+-------------+-------+
INFO - 16:23:43: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:43: +------+-------------+-------+-------------+-------+
INFO - 16:23:43: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:43: +------+-------------+-------+-------------+-------+
INFO - 16:23:43: *** End AerodynamicsScenario execution (time: 0:00:00.014000) ***
INFO - 16:23:43: *** Start StructureScenario execution ***
INFO - 16:23:43: StructureScenario
INFO - 16:23:43: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:43: MDO formulation: MDF
INFO - 16:23:43: Optimization problem:
INFO - 16:23:43: minimize 0.001*-y_4(x_1)
INFO - 16:23:43: with respect to x_1
INFO - 16:23:43: under the inequality constraints
INFO - 16:23:43: g_1(x_1) <= 0
INFO - 16:23:43: over the design space:
INFO - 16:23:43: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:43: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:43: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:43: | x_1[0] | 0.1 | 0.1000000000000026 | 0.4 | float |
INFO - 16:23:43: | x_1[1] | 0.75 | 0.8114361865723931 | 1.25 | float |
INFO - 16:23:43: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:43: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:43: 2%|▏ | 1/50 [00:00<00:00, 103.14 it/sec, feas=True, obj=-2.2]
INFO - 16:23:43: 4%|▍ | 2/50 [00:00<00:00, 58.83 it/sec, feas=True, obj=-2.2]
INFO - 16:23:43: 6%|▌ | 3/50 [00:00<00:00, 51.46 it/sec, feas=True, obj=-2.2]
INFO - 16:23:43: Optimization result:
INFO - 16:23:43: Optimizer info:
INFO - 16:23:43: Status: None
INFO - 16:23:43: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:43: Solution:
INFO - 16:23:43: The solution is feasible.
INFO - 16:23:43: Objective: -2.200234902138859
INFO - 16:23:43: Standardized constraints:
INFO - 16:23:43: g_1 = [ 1.03961284e-12 -3.55526455e-03 -1.52496726e-02 -2.54396857e-02
INFO - 16:23:43: -3.35552645e-02 -2.30122617e-01 -9.87738314e-03]
INFO - 16:23:43: Design space:
INFO - 16:23:43: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:43: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:43: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:43: | x_1[0] | 0.1 | 0.1000000000000026 | 0.4 | float |
INFO - 16:23:43: | x_1[1] | 0.75 | 0.8114361865723931 | 1.25 | float |
INFO - 16:23:43: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:43: *** End StructureScenario execution (time: 0:00:00.061087) ***
INFO - 16:23:43: 35%|███▌ | 35/100 [00:27<00:50, 1.30 it/sec, feas=True, obj=-2.2]
INFO - 16:23:43: *** Start PropulsionScenario execution ***
INFO - 16:23:43: PropulsionScenario
INFO - 16:23:43: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:43: MDO formulation: MDF
INFO - 16:23:43: Optimization problem:
INFO - 16:23:43: minimize 0.001*-y_4(x_3)
INFO - 16:23:43: with respect to x_3
INFO - 16:23:43: under the inequality constraints
INFO - 16:23:43: g_3(x_3) <= 0
INFO - 16:23:43: over the design space:
INFO - 16:23:43: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:43: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:43: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:43: | x_3 | 0.1 | 0.1580559135944434 | 1 | float |
INFO - 16:23:43: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:43: Solving optimization problem with algorithm SLSQP:
WARNING - 16:23:43: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 6.724932466608626e-05 is still above the tolerance 1e-06.
INFO - 16:23:43: 2%|▏ | 1/50 [00:00<00:01, 34.09 it/sec, feas=True, obj=-2.16]
INFO - 16:23:43: 4%|▍ | 2/50 [00:00<00:01, 30.04 it/sec, feas=True, obj=-2.16]
INFO - 16:23:44: 6%|▌ | 3/50 [00:00<00:01, 34.09 it/sec, feas=True, obj=-2.16]
WARNING - 16:23:44: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 6.724932466608626e-05 is still above the tolerance 1e-06.
INFO - 16:23:44: 8%|▊ | 4/50 [00:00<00:01, 34.02 it/sec, feas=True, obj=-2.16]
INFO - 16:23:44: Optimization result:
INFO - 16:23:44: Optimizer info:
INFO - 16:23:44: Status: None
INFO - 16:23:44: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:44: Solution:
INFO - 16:23:44: The solution is feasible.
INFO - 16:23:44: Objective: -2.1638355875245026
INFO - 16:23:44: Standardized constraints:
INFO - 16:23:44: g_3 = [-8.28491773e-01 -1.71508227e-01 -2.10942375e-15 -1.79835339e-01]
INFO - 16:23:44: Design space:
INFO - 16:23:44: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:44: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:44: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:44: | x_3 | 0.1 | 0.1599333647421787 | 1 | float |
INFO - 16:23:44: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:44: *** End PropulsionScenario execution (time: 0:00:00.120224) ***
INFO - 16:23:44: *** Start AerodynamicsScenario execution ***
INFO - 16:23:44: AerodynamicsScenario
INFO - 16:23:44: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:44: MDO formulation: MDF
INFO - 16:23:44: Optimization problem:
INFO - 16:23:44: minimize 0.001*-y_4(x_2)
INFO - 16:23:44: with respect to x_2
INFO - 16:23:44: under the inequality constraints
INFO - 16:23:44: g_2(x_2) <= 0
INFO - 16:23:44: over the design space:
INFO - 16:23:44: +------+-------------+-------+-------------+-------+
INFO - 16:23:44: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:44: +------+-------------+-------+-------------+-------+
INFO - 16:23:44: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:44: +------+-------------+-------+-------------+-------+
INFO - 16:23:44: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:44: 2%|▏ | 1/50 [00:00<00:00, 71.15 it/sec, feas=True, obj=-2.16]
INFO - 16:23:44: Optimization result:
INFO - 16:23:44: Optimizer info:
INFO - 16:23:44: Status: 8
INFO - 16:23:44: Message: Positive directional derivative for linesearch
INFO - 16:23:44: Solution:
INFO - 16:23:44: The solution is feasible.
INFO - 16:23:44: Objective: -2.1638355875245034
INFO - 16:23:44: Standardized constraints:
INFO - 16:23:44: g_2 = 0.0
INFO - 16:23:44: Design space:
INFO - 16:23:44: +------+-------------+-------+-------------+-------+
INFO - 16:23:44: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:44: +------+-------------+-------+-------------+-------+
INFO - 16:23:44: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:44: +------+-------------+-------+-------------+-------+
INFO - 16:23:44: *** End AerodynamicsScenario execution (time: 0:00:00.015630) ***
INFO - 16:23:44: *** Start StructureScenario execution ***
INFO - 16:23:44: StructureScenario
INFO - 16:23:44: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:44: MDO formulation: MDF
INFO - 16:23:44: Optimization problem:
INFO - 16:23:44: minimize 0.001*-y_4(x_1)
INFO - 16:23:44: with respect to x_1
INFO - 16:23:44: under the inequality constraints
INFO - 16:23:44: g_1(x_1) <= 0
INFO - 16:23:44: over the design space:
INFO - 16:23:44: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:44: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:44: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:44: | x_1[0] | 0.1 | 0.1000000000000026 | 0.4 | float |
INFO - 16:23:44: | x_1[1] | 0.75 | 0.8114361865723931 | 1.25 | float |
INFO - 16:23:44: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:44: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:44: 2%|▏ | 1/50 [00:00<00:00, 78.95 it/sec, feas=True, obj=-2.16]
WARNING - 16:23:44: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 0.0018314954719615695 is still above the tolerance 1e-06.
INFO - 16:23:44: 4%|▍ | 2/50 [00:00<00:01, 33.67 it/sec, feas=True, obj=-2.21]
INFO - 16:23:44: 6%|▌ | 3/50 [00:00<00:01, 29.55 it/sec, feas=True, obj=-2.21]
INFO - 16:23:44: 8%|▊ | 4/50 [00:00<00:01, 27.71 it/sec, feas=True, obj=-2.21]
INFO - 16:23:44: 10%|█ | 5/50 [00:00<00:01, 26.75 it/sec, feas=True, obj=-2.21]
INFO - 16:23:44: 12%|█▏ | 6/50 [00:00<00:01, 26.17 it/sec, feas=True, obj=-2.21]
INFO - 16:23:44: Optimization result:
INFO - 16:23:44: Optimizer info:
INFO - 16:23:44: Status: 8
INFO - 16:23:44: Message: Positive directional derivative for linesearch
INFO - 16:23:44: Solution:
INFO - 16:23:44: The solution is feasible.
INFO - 16:23:44: Objective: -2.2058762800855485
INFO - 16:23:44: Standardized constraints:
INFO - 16:23:44: g_1 = [-1.59589593e-03 -2.02868890e-03 -1.31333010e-02 -2.32802973e-02
INFO - 16:23:44: -3.14967236e-02 -2.40000000e-01 1.11022302e-16]
INFO - 16:23:44: Design space:
INFO - 16:23:44: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:44: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:44: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:44: | x_1[0] | 0.1 | 0.1000000000000001 | 0.4 | float |
INFO - 16:23:44: | x_1[1] | 0.75 | 0.7806436836765259 | 1.25 | float |
INFO - 16:23:44: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:44: *** End StructureScenario execution (time: 0:00:00.231415) ***
INFO - 16:23:44: *** Start PropulsionScenario execution ***
INFO - 16:23:44: PropulsionScenario
INFO - 16:23:44: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:44: MDO formulation: MDF
INFO - 16:23:44: Optimization problem:
INFO - 16:23:44: minimize 0.001*-y_4(x_3)
INFO - 16:23:44: with respect to x_3
INFO - 16:23:44: under the inequality constraints
INFO - 16:23:44: g_3(x_3) <= 0
INFO - 16:23:44: over the design space:
INFO - 16:23:44: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:44: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:44: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:44: | x_3 | 0.1 | 0.1599333647421787 | 1 | float |
INFO - 16:23:44: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:44: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:44: 2%|▏ | 1/50 [00:00<00:00, 83.73 it/sec, feas=True, obj=-2.21]
INFO - 16:23:44: Optimization result:
INFO - 16:23:44: Optimizer info:
INFO - 16:23:44: Status: 8
INFO - 16:23:44: Message: Positive directional derivative for linesearch
INFO - 16:23:44: Solution:
INFO - 16:23:44: The solution is feasible.
INFO - 16:23:44: Objective: -2.2058762800855485
INFO - 16:23:44: Standardized constraints:
INFO - 16:23:44: g_3 = [-8.28610774e-01 -1.71389226e-01 -2.10942375e-15 -1.79835339e-01]
INFO - 16:23:44: Design space:
INFO - 16:23:44: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:44: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:44: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:44: | x_3 | 0.1 | 0.1599333647421787 | 1 | float |
INFO - 16:23:44: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:44: *** End PropulsionScenario execution (time: 0:00:00.013915) ***
INFO - 16:23:44: *** Start AerodynamicsScenario execution ***
INFO - 16:23:44: AerodynamicsScenario
INFO - 16:23:44: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:44: MDO formulation: MDF
INFO - 16:23:44: Optimization problem:
INFO - 16:23:44: minimize 0.001*-y_4(x_2)
INFO - 16:23:44: with respect to x_2
INFO - 16:23:44: under the inequality constraints
INFO - 16:23:44: g_2(x_2) <= 0
INFO - 16:23:44: over the design space:
INFO - 16:23:44: +------+-------------+-------+-------------+-------+
INFO - 16:23:44: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:44: +------+-------------+-------+-------------+-------+
INFO - 16:23:44: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:44: +------+-------------+-------+-------------+-------+
INFO - 16:23:44: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:44: 2%|▏ | 1/50 [00:00<00:00, 107.97 it/sec, feas=True, obj=-2.21]
INFO - 16:23:44: Optimization result:
INFO - 16:23:44: Optimizer info:
INFO - 16:23:44: Status: 8
INFO - 16:23:44: Message: Positive directional derivative for linesearch
INFO - 16:23:44: Solution:
INFO - 16:23:44: The solution is feasible.
INFO - 16:23:44: Objective: -2.2058762800855485
INFO - 16:23:44: Standardized constraints:
INFO - 16:23:44: g_2 = 0.0
INFO - 16:23:44: Design space:
INFO - 16:23:44: +------+-------------+-------+-------------+-------+
INFO - 16:23:44: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:44: +------+-------------+-------+-------------+-------+
INFO - 16:23:44: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:44: +------+-------------+-------+-------------+-------+
INFO - 16:23:44: *** End AerodynamicsScenario execution (time: 0:00:00.011051) ***
INFO - 16:23:44: *** Start StructureScenario execution ***
INFO - 16:23:44: StructureScenario
INFO - 16:23:44: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:44: MDO formulation: MDF
INFO - 16:23:44: Optimization problem:
INFO - 16:23:44: minimize 0.001*-y_4(x_1)
INFO - 16:23:44: with respect to x_1
INFO - 16:23:44: under the inequality constraints
INFO - 16:23:44: g_1(x_1) <= 0
INFO - 16:23:44: over the design space:
INFO - 16:23:44: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:44: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:44: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:44: | x_1[0] | 0.1 | 0.1000000000000001 | 0.4 | float |
INFO - 16:23:44: | x_1[1] | 0.75 | 0.7806436836765259 | 1.25 | float |
INFO - 16:23:44: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:44: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:44: 2%|▏ | 1/50 [00:00<00:00, 102.28 it/sec, feas=True, obj=-2.21]
INFO - 16:23:44: 4%|▍ | 2/50 [00:00<00:00, 69.65 it/sec, feas=True, obj=-2.21]
INFO - 16:23:44: 6%|▌ | 3/50 [00:00<00:00, 60.23 it/sec, feas=True, obj=-2.21]
INFO - 16:23:44: Optimization result:
INFO - 16:23:44: Optimizer info:
INFO - 16:23:44: Status: None
INFO - 16:23:44: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:44: Solution:
INFO - 16:23:44: The solution is feasible.
INFO - 16:23:44: Objective: -2.20587628008555
INFO - 16:23:44: Standardized constraints:
INFO - 16:23:44: g_1 = [-1.59589593e-03 -2.02868890e-03 -1.31333010e-02 -2.32802973e-02
INFO - 16:23:44: -3.14967236e-02 -2.40000000e-01 2.22044605e-16]
INFO - 16:23:44: Design space:
INFO - 16:23:44: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:44: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:44: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:44: | x_1[0] | 0.1 | 0.1000000000000001 | 0.4 | float |
INFO - 16:23:44: | x_1[1] | 0.75 | 0.7806436836765256 | 1.25 | float |
INFO - 16:23:44: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:44: *** End StructureScenario execution (time: 0:00:00.052323) ***
INFO - 16:23:44: 36%|███▌ | 36/100 [00:27<00:48, 1.31 it/sec, feas=True, obj=-2.21]
INFO - 16:23:44: *** Start PropulsionScenario execution ***
INFO - 16:23:44: PropulsionScenario
INFO - 16:23:44: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:44: MDO formulation: MDF
INFO - 16:23:44: Optimization problem:
INFO - 16:23:44: minimize 0.001*-y_4(x_3)
INFO - 16:23:44: with respect to x_3
INFO - 16:23:44: under the inequality constraints
INFO - 16:23:44: g_3(x_3) <= 0
INFO - 16:23:44: over the design space:
INFO - 16:23:44: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:44: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:44: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:44: | x_3 | 0.1 | 0.1599333647421787 | 1 | float |
INFO - 16:23:44: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:44: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:44: 2%|▏ | 1/50 [00:00<00:01, 37.78 it/sec, feas=False, obj=-2.31]
INFO - 16:23:44: 4%|▍ | 2/50 [00:00<00:01, 38.11 it/sec, feas=True, obj=-2.3]
INFO - 16:23:44: 6%|▌ | 3/50 [00:00<00:01, 31.41 it/sec, feas=False, obj=-2.31]
INFO - 16:23:44: 8%|▊ | 4/50 [00:00<00:01, 28.85 it/sec, feas=True, obj=-2.3]
INFO - 16:23:44: Optimization result:
INFO - 16:23:44: Optimizer info:
INFO - 16:23:44: Status: 8
INFO - 16:23:44: Message: Positive directional derivative for linesearch
INFO - 16:23:44: Solution:
INFO - 16:23:44: The solution is feasible.
INFO - 16:23:44: Objective: -2.3042574992837066
INFO - 16:23:44: Standardized constraints:
INFO - 16:23:44: g_3 = [-8.29128932e-01 -1.70871068e-01 9.32587341e-15 -1.83032784e-01]
INFO - 16:23:44: Design space:
INFO - 16:23:44: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:44: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:44: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:44: | x_3 | 0.1 | 0.1564797518276684 | 1 | float |
INFO - 16:23:44: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:44: *** End PropulsionScenario execution (time: 0:00:00.140819) ***
INFO - 16:23:44: *** Start AerodynamicsScenario execution ***
INFO - 16:23:44: AerodynamicsScenario
INFO - 16:23:44: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:44: MDO formulation: MDF
INFO - 16:23:44: Optimization problem:
INFO - 16:23:44: minimize 0.001*-y_4(x_2)
INFO - 16:23:44: with respect to x_2
INFO - 16:23:44: under the inequality constraints
INFO - 16:23:44: g_2(x_2) <= 0
INFO - 16:23:44: over the design space:
INFO - 16:23:44: +------+-------------+-------+-------------+-------+
INFO - 16:23:44: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:44: +------+-------------+-------+-------------+-------+
INFO - 16:23:44: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:44: +------+-------------+-------+-------------+-------+
INFO - 16:23:44: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:44: 2%|▏ | 1/50 [00:00<00:00, 77.29 it/sec, feas=True, obj=-2.3]
INFO - 16:23:44: Optimization result:
INFO - 16:23:44: Optimizer info:
INFO - 16:23:44: Status: 8
INFO - 16:23:44: Message: Positive directional derivative for linesearch
INFO - 16:23:44: Solution:
INFO - 16:23:44: The solution is feasible.
INFO - 16:23:44: Objective: -2.3042574992837066
INFO - 16:23:44: Standardized constraints:
INFO - 16:23:44: g_2 = 0.0
INFO - 16:23:44: Design space:
INFO - 16:23:44: +------+-------------+-------+-------------+-------+
INFO - 16:23:44: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:44: +------+-------------+-------+-------------+-------+
INFO - 16:23:44: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:44: +------+-------------+-------+-------------+-------+
INFO - 16:23:44: *** End AerodynamicsScenario execution (time: 0:00:00.014661) ***
INFO - 16:23:44: *** Start StructureScenario execution ***
INFO - 16:23:44: StructureScenario
INFO - 16:23:44: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:44: MDO formulation: MDF
INFO - 16:23:44: Optimization problem:
INFO - 16:23:44: minimize 0.001*-y_4(x_1)
INFO - 16:23:44: with respect to x_1
INFO - 16:23:44: under the inequality constraints
INFO - 16:23:44: g_1(x_1) <= 0
INFO - 16:23:44: over the design space:
INFO - 16:23:44: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:44: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:44: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:44: | x_1[0] | 0.1 | 0.1000000000000001 | 0.4 | float |
INFO - 16:23:44: | x_1[1] | 0.75 | 0.7806436836765256 | 1.25 | float |
INFO - 16:23:44: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:44: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:44: 2%|▏ | 1/50 [00:00<00:00, 77.50 it/sec, feas=True, obj=-2.3]
INFO - 16:23:44: Optimization result:
INFO - 16:23:44: Optimizer info:
INFO - 16:23:44: Status: 8
INFO - 16:23:44: Message: Positive directional derivative for linesearch
INFO - 16:23:44: Solution:
INFO - 16:23:44: The solution is feasible.
INFO - 16:23:44: Objective: -2.3042574992837066
INFO - 16:23:44: Standardized constraints:
INFO - 16:23:44: g_1 = [-1.59589593e-03 -2.02868890e-03 -1.31333010e-02 -2.32802973e-02
INFO - 16:23:44: -3.14967236e-02 -2.40000000e-01 2.22044605e-16]
INFO - 16:23:44: Design space:
INFO - 16:23:44: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:44: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:44: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:44: | x_1[0] | 0.1 | 0.1000000000000001 | 0.4 | float |
INFO - 16:23:44: | x_1[1] | 0.75 | 0.7806436836765256 | 1.25 | float |
INFO - 16:23:44: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:44: *** End StructureScenario execution (time: 0:00:00.014793) ***
INFO - 16:23:44: *** Start PropulsionScenario execution ***
INFO - 16:23:44: PropulsionScenario
INFO - 16:23:44: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:44: MDO formulation: MDF
INFO - 16:23:44: Optimization problem:
INFO - 16:23:44: minimize 0.001*-y_4(x_3)
INFO - 16:23:44: with respect to x_3
INFO - 16:23:44: under the inequality constraints
INFO - 16:23:44: g_3(x_3) <= 0
INFO - 16:23:44: over the design space:
INFO - 16:23:44: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:44: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:44: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:44: | x_3 | 0.1 | 0.1564797518276684 | 1 | float |
INFO - 16:23:44: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:44: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:44: 2%|▏ | 1/50 [00:00<00:00, 109.29 it/sec, feas=True, obj=-2.3]
INFO - 16:23:44: Optimization result:
INFO - 16:23:44: Optimizer info:
INFO - 16:23:44: Status: 8
INFO - 16:23:44: Message: Positive directional derivative for linesearch
INFO - 16:23:44: Solution:
INFO - 16:23:44: The solution is feasible.
INFO - 16:23:44: Objective: -2.3042574992837066
INFO - 16:23:44: Standardized constraints:
INFO - 16:23:44: g_3 = [-8.29128932e-01 -1.70871068e-01 9.32587341e-15 -1.83032784e-01]
INFO - 16:23:44: Design space:
INFO - 16:23:44: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:44: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:44: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:44: | x_3 | 0.1 | 0.1564797518276684 | 1 | float |
INFO - 16:23:44: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:44: *** End PropulsionScenario execution (time: 0:00:00.010795) ***
INFO - 16:23:44: *** Start AerodynamicsScenario execution ***
INFO - 16:23:44: AerodynamicsScenario
INFO - 16:23:44: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:44: MDO formulation: MDF
INFO - 16:23:44: Optimization problem:
INFO - 16:23:44: minimize 0.001*-y_4(x_2)
INFO - 16:23:44: with respect to x_2
INFO - 16:23:44: under the inequality constraints
INFO - 16:23:44: g_2(x_2) <= 0
INFO - 16:23:44: over the design space:
INFO - 16:23:44: +------+-------------+-------+-------------+-------+
INFO - 16:23:44: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:44: +------+-------------+-------+-------------+-------+
INFO - 16:23:44: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:44: +------+-------------+-------+-------------+-------+
INFO - 16:23:44: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:44: 2%|▏ | 1/50 [00:00<00:00, 109.63 it/sec, feas=True, obj=-2.3]
INFO - 16:23:44: Optimization result:
INFO - 16:23:44: Optimizer info:
INFO - 16:23:44: Status: 8
INFO - 16:23:44: Message: Positive directional derivative for linesearch
INFO - 16:23:44: Solution:
INFO - 16:23:44: The solution is feasible.
INFO - 16:23:44: Objective: -2.3042574992837066
INFO - 16:23:44: Standardized constraints:
INFO - 16:23:44: g_2 = 0.0
INFO - 16:23:44: Design space:
INFO - 16:23:44: +------+-------------+-------+-------------+-------+
INFO - 16:23:44: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:44: +------+-------------+-------+-------------+-------+
INFO - 16:23:44: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:44: +------+-------------+-------+-------------+-------+
INFO - 16:23:44: *** End AerodynamicsScenario execution (time: 0:00:00.010640) ***
INFO - 16:23:44: *** Start StructureScenario execution ***
INFO - 16:23:44: StructureScenario
INFO - 16:23:44: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:44: MDO formulation: MDF
INFO - 16:23:44: Optimization problem:
INFO - 16:23:44: minimize 0.001*-y_4(x_1)
INFO - 16:23:44: with respect to x_1
INFO - 16:23:44: under the inequality constraints
INFO - 16:23:44: g_1(x_1) <= 0
INFO - 16:23:44: over the design space:
INFO - 16:23:44: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:44: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:44: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:44: | x_1[0] | 0.1 | 0.1000000000000001 | 0.4 | float |
INFO - 16:23:44: | x_1[1] | 0.75 | 0.7806436836765256 | 1.25 | float |
INFO - 16:23:44: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:44: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:44: 2%|▏ | 1/50 [00:00<00:00, 85.38 it/sec, feas=True, obj=-2.3]
INFO - 16:23:44: Optimization result:
INFO - 16:23:44: Optimizer info:
INFO - 16:23:44: Status: 8
INFO - 16:23:44: Message: Positive directional derivative for linesearch
INFO - 16:23:44: Solution:
INFO - 16:23:44: The solution is feasible.
INFO - 16:23:44: Objective: -2.3042574992837066
INFO - 16:23:44: Standardized constraints:
INFO - 16:23:44: g_1 = [-1.59589593e-03 -2.02868890e-03 -1.31333010e-02 -2.32802973e-02
INFO - 16:23:44: -3.14967236e-02 -2.40000000e-01 2.22044605e-16]
INFO - 16:23:44: Design space:
INFO - 16:23:44: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:44: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:44: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:44: | x_1[0] | 0.1 | 0.1000000000000001 | 0.4 | float |
INFO - 16:23:44: | x_1[1] | 0.75 | 0.7806436836765256 | 1.25 | float |
INFO - 16:23:44: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:44: *** End StructureScenario execution (time: 0:00:00.013610) ***
INFO - 16:23:44: 37%|███▋ | 37/100 [00:27<00:47, 1.33 it/sec, feas=True, obj=-2.3]
INFO - 16:23:44: *** Start PropulsionScenario execution ***
INFO - 16:23:44: PropulsionScenario
INFO - 16:23:44: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:44: MDO formulation: MDF
INFO - 16:23:44: Optimization problem:
INFO - 16:23:44: minimize 0.001*-y_4(x_3)
INFO - 16:23:44: with respect to x_3
INFO - 16:23:44: under the inequality constraints
INFO - 16:23:44: g_3(x_3) <= 0
INFO - 16:23:44: over the design space:
INFO - 16:23:44: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:44: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:44: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:44: | x_3 | 0.1 | 0.1564797518276684 | 1 | float |
INFO - 16:23:44: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:44: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:44: 2%|▏ | 1/50 [00:00<00:01, 37.42 it/sec, feas=True, obj=-2.29]
INFO - 16:23:44: 4%|▍ | 2/50 [00:00<00:01, 38.16 it/sec, feas=True, obj=-2.29]
INFO - 16:23:44: 6%|▌ | 3/50 [00:00<00:01, 31.86 it/sec, feas=True, obj=-2.29]
WARNING - 16:23:44: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 6.724932466608626e-05 is still above the tolerance 1e-06.
INFO - 16:23:44: 8%|▊ | 4/50 [00:00<00:01, 28.09 it/sec, feas=True, obj=-2.29]
INFO - 16:23:44: 10%|█ | 5/50 [00:00<00:01, 27.31 it/sec, feas=True, obj=-2.29]
INFO - 16:23:44: Optimization result:
INFO - 16:23:44: Optimizer info:
INFO - 16:23:44: Status: 8
INFO - 16:23:44: Message: Positive directional derivative for linesearch
INFO - 16:23:44: Solution:
INFO - 16:23:44: The solution is feasible.
INFO - 16:23:44: Objective: -2.291959140638156
INFO - 16:23:44: Standardized constraints:
INFO - 16:23:44: g_3 = [-8.27002123e-01 -1.72997877e-01 5.12863514e-06 -1.83114805e-01]
INFO - 16:23:44: Design space:
INFO - 16:23:44: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:44: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:44: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:44: | x_3 | 0.1 | 0.1564797518276684 | 1 | float |
INFO - 16:23:44: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:44: *** End PropulsionScenario execution (time: 0:00:00.184958) ***
INFO - 16:23:44: *** Start AerodynamicsScenario execution ***
INFO - 16:23:44: AerodynamicsScenario
INFO - 16:23:44: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:44: MDO formulation: MDF
INFO - 16:23:44: Optimization problem:
INFO - 16:23:44: minimize 0.001*-y_4(x_2)
INFO - 16:23:44: with respect to x_2
INFO - 16:23:44: under the inequality constraints
INFO - 16:23:44: g_2(x_2) <= 0
INFO - 16:23:44: over the design space:
INFO - 16:23:44: +------+-------------+-------+-------------+-------+
INFO - 16:23:44: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:44: +------+-------------+-------+-------------+-------+
INFO - 16:23:44: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:44: +------+-------------+-------+-------------+-------+
INFO - 16:23:44: Solving optimization problem with algorithm SLSQP:
WARNING - 16:23:44: Optimization found no feasible point; the least infeasible point is selected.
INFO - 16:23:44: 2%|▏ | 1/50 [00:00<00:00, 76.30 it/sec, feas=False, obj=-2.29]
INFO - 16:23:44: Optimization result:
INFO - 16:23:44: Optimizer info:
INFO - 16:23:44: Status: 8
INFO - 16:23:44: Message: Positive directional derivative for linesearch
INFO - 16:23:44: Solution:
WARNING - 16:23:44: The solution is not feasible.
INFO - 16:23:44: Objective: -2.291959140638156
INFO - 16:23:44: Standardized constraints:
INFO - 16:23:44: g_2 = 0.0023498956921459424
INFO - 16:23:44: Design space:
INFO - 16:23:44: +------+-------------+-------+-------------+-------+
INFO - 16:23:44: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:44: +------+-------------+-------+-------------+-------+
INFO - 16:23:44: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:44: +------+-------------+-------+-------------+-------+
INFO - 16:23:44: *** End AerodynamicsScenario execution (time: 0:00:00.014681) ***
INFO - 16:23:44: *** Start StructureScenario execution ***
INFO - 16:23:44: StructureScenario
INFO - 16:23:44: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:44: MDO formulation: MDF
INFO - 16:23:44: Optimization problem:
INFO - 16:23:44: minimize 0.001*-y_4(x_1)
INFO - 16:23:44: with respect to x_1
INFO - 16:23:44: under the inequality constraints
INFO - 16:23:44: g_1(x_1) <= 0
INFO - 16:23:44: over the design space:
INFO - 16:23:44: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:44: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:44: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:44: | x_1[0] | 0.1 | 0.1000000000000001 | 0.4 | float |
INFO - 16:23:44: | x_1[1] | 0.75 | 0.7806436836765256 | 1.25 | float |
INFO - 16:23:44: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:44: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:44: 2%|▏ | 1/50 [00:00<00:00, 97.06 it/sec, feas=True, obj=-2.29]
INFO - 16:23:44: Optimization result:
INFO - 16:23:44: Optimizer info:
INFO - 16:23:44: Status: 8
INFO - 16:23:44: Message: Positive directional derivative for linesearch
INFO - 16:23:44: Solution:
INFO - 16:23:44: The solution is feasible.
INFO - 16:23:44: Objective: -2.291959140638156
INFO - 16:23:44: Standardized constraints:
INFO - 16:23:44: g_1 = [-2.06001704e-02 -1.24332795e-02 -2.00873969e-02 -2.84358874e-02
INFO - 16:23:44: -3.55665561e-02 -2.40000000e-01 2.22044605e-16]
INFO - 16:23:44: Design space:
INFO - 16:23:44: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:44: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:44: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:44: | x_1[0] | 0.1 | 0.1000000000000001 | 0.4 | float |
INFO - 16:23:44: | x_1[1] | 0.75 | 0.7806436836765256 | 1.25 | float |
INFO - 16:23:44: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:44: *** End StructureScenario execution (time: 0:00:00.012216) ***
INFO - 16:23:44: *** Start PropulsionScenario execution ***
INFO - 16:23:44: PropulsionScenario
INFO - 16:23:44: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:44: MDO formulation: MDF
INFO - 16:23:44: Optimization problem:
INFO - 16:23:44: minimize 0.001*-y_4(x_3)
INFO - 16:23:44: with respect to x_3
INFO - 16:23:44: under the inequality constraints
INFO - 16:23:44: g_3(x_3) <= 0
INFO - 16:23:44: over the design space:
INFO - 16:23:44: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:44: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:44: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:44: | x_3 | 0.1 | 0.1564797518276684 | 1 | float |
INFO - 16:23:44: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:44: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:44: 2%|▏ | 1/50 [00:00<00:00, 109.30 it/sec, feas=True, obj=-2.29]
INFO - 16:23:44: 4%|▍ | 2/50 [00:00<00:00, 83.37 it/sec, feas=True, obj=-2.29]
INFO - 16:23:44: 6%|▌ | 3/50 [00:00<00:00, 53.90 it/sec, feas=True, obj=-2.29]
WARNING - 16:23:44: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 6.724932466608626e-05 is still above the tolerance 1e-06.
INFO - 16:23:44: 8%|▊ | 4/50 [00:00<00:01, 41.49 it/sec, feas=True, obj=-2.29]
INFO - 16:23:44: 10%|█ | 5/50 [00:00<00:01, 44.81 it/sec, feas=True, obj=-2.29]
INFO - 16:23:45: 12%|█▏ | 6/50 [00:00<00:01, 41.80 it/sec, feas=True, obj=-2.29]
INFO - 16:23:45: Optimization result:
INFO - 16:23:45: Optimizer info:
INFO - 16:23:45: Status: None
INFO - 16:23:45: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:45: Solution:
INFO - 16:23:45: The solution is feasible.
INFO - 16:23:45: Objective: -2.291959140638156
INFO - 16:23:45: Standardized constraints:
INFO - 16:23:45: g_3 = [-8.27002123e-01 -1.72997877e-01 5.12863514e-06 -1.83114805e-01]
INFO - 16:23:45: Design space:
INFO - 16:23:45: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:45: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:45: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:45: | x_3 | 0.1 | 0.1564797518276684 | 1 | float |
INFO - 16:23:45: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:45: *** End PropulsionScenario execution (time: 0:00:00.145636) ***
INFO - 16:23:45: 38%|███▊ | 38/100 [00:28<00:45, 1.35 it/sec, feas=False, obj=-2.29]
INFO - 16:23:45: *** Start PropulsionScenario execution ***
INFO - 16:23:45: PropulsionScenario
INFO - 16:23:45: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:45: MDO formulation: MDF
INFO - 16:23:45: Optimization problem:
INFO - 16:23:45: minimize 0.001*-y_4(x_3)
INFO - 16:23:45: with respect to x_3
INFO - 16:23:45: under the inequality constraints
INFO - 16:23:45: g_3(x_3) <= 0
INFO - 16:23:45: over the design space:
INFO - 16:23:45: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:45: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:45: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:45: | x_3 | 0.1 | 0.1564797518276684 | 1 | float |
INFO - 16:23:45: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:45: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:45: 2%|▏ | 1/50 [00:00<00:01, 38.45 it/sec, feas=False, obj=-2.28]
INFO - 16:23:45: 4%|▍ | 2/50 [00:00<00:01, 38.70 it/sec, feas=True, obj=-2.28]
INFO - 16:23:45: 6%|▌ | 3/50 [00:00<00:01, 32.11 it/sec, feas=False, obj=-2.28]
WARNING - 16:23:45: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 6.724932466608626e-05 is still above the tolerance 1e-06.
INFO - 16:23:45: 8%|▊ | 4/50 [00:00<00:01, 28.54 it/sec, feas=True, obj=-2.28]
INFO - 16:23:45: Optimization result:
INFO - 16:23:45: Optimizer info:
INFO - 16:23:45: Status: 8
INFO - 16:23:45: Message: Positive directional derivative for linesearch
INFO - 16:23:45: Solution:
INFO - 16:23:45: The solution is feasible.
INFO - 16:23:45: Objective: -2.2778801336747576
INFO - 16:23:45: Standardized constraints:
INFO - 16:23:45: g_3 = [-0.83658332 -0.16341668 0. -0.1831306 ]
INFO - 16:23:45: Design space:
INFO - 16:23:45: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:45: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:45: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:45: | x_3 | 0.1 | 0.1563852262747091 | 1 | float |
INFO - 16:23:45: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:45: *** End PropulsionScenario execution (time: 0:00:00.142223) ***
INFO - 16:23:45: *** Start AerodynamicsScenario execution ***
INFO - 16:23:45: AerodynamicsScenario
INFO - 16:23:45: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:45: MDO formulation: MDF
INFO - 16:23:45: Optimization problem:
INFO - 16:23:45: minimize 0.001*-y_4(x_2)
INFO - 16:23:45: with respect to x_2
INFO - 16:23:45: under the inequality constraints
INFO - 16:23:45: g_2(x_2) <= 0
INFO - 16:23:45: over the design space:
INFO - 16:23:45: +------+-------------+-------+-------------+-------+
INFO - 16:23:45: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:45: +------+-------------+-------+-------------+-------+
INFO - 16:23:45: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:45: +------+-------------+-------+-------------+-------+
INFO - 16:23:45: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:45: 2%|▏ | 1/50 [00:00<00:00, 78.96 it/sec, feas=True, obj=-2.28]
INFO - 16:23:45: Optimization result:
INFO - 16:23:45: Optimizer info:
INFO - 16:23:45: Status: 8
INFO - 16:23:45: Message: Positive directional derivative for linesearch
INFO - 16:23:45: Solution:
INFO - 16:23:45: The solution is feasible.
INFO - 16:23:45: Objective: -2.2778801336747576
INFO - 16:23:45: Standardized constraints:
INFO - 16:23:45: g_2 = -0.004841296871685996
INFO - 16:23:45: Design space:
INFO - 16:23:45: +------+-------------+-------+-------------+-------+
INFO - 16:23:45: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:45: +------+-------------+-------+-------------+-------+
INFO - 16:23:45: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:45: +------+-------------+-------+-------------+-------+
INFO - 16:23:45: *** End AerodynamicsScenario execution (time: 0:00:00.014174) ***
INFO - 16:23:45: *** Start StructureScenario execution ***
INFO - 16:23:45: StructureScenario
INFO - 16:23:45: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:45: MDO formulation: MDF
INFO - 16:23:45: Optimization problem:
INFO - 16:23:45: minimize 0.001*-y_4(x_1)
INFO - 16:23:45: with respect to x_1
INFO - 16:23:45: under the inequality constraints
INFO - 16:23:45: g_1(x_1) <= 0
INFO - 16:23:45: over the design space:
INFO - 16:23:45: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:45: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:45: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:45: | x_1[0] | 0.1 | 0.1000000000000001 | 0.4 | float |
INFO - 16:23:45: | x_1[1] | 0.75 | 0.7806436836765256 | 1.25 | float |
INFO - 16:23:45: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:45: Solving optimization problem with algorithm SLSQP:
WARNING - 16:23:45: MDAGaussSeidel has reached its maximum number of unsuccessful iterations, but the normalized residual norm 0.0009157477359807847 is still above the tolerance 1e-06.
INFO - 16:23:45: 2%|▏ | 1/50 [00:00<00:00, 53.19 it/sec, feas=False, obj=-2.28]
INFO - 16:23:45: 4%|▍ | 2/50 [00:00<00:01, 38.09 it/sec, feas=True, obj=-2.21]
INFO - 16:23:45: 6%|▌ | 3/50 [00:00<00:01, 34.38 it/sec, feas=True, obj=-2.22]
INFO - 16:23:45: 8%|▊ | 4/50 [00:00<00:01, 32.62 it/sec, feas=True, obj=-2.22]
INFO - 16:23:45: 10%|█ | 5/50 [00:00<00:01, 31.66 it/sec, feas=True, obj=-2.22]
INFO - 16:23:45: 12%|█▏ | 6/50 [00:00<00:01, 31.06 it/sec, feas=True, obj=-2.22]
INFO - 16:23:45: Optimization result:
INFO - 16:23:45: Optimizer info:
INFO - 16:23:45: Status: None
INFO - 16:23:45: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:45: Solution:
INFO - 16:23:45: The solution is feasible.
INFO - 16:23:45: Objective: -2.2172812963553024
INFO - 16:23:45: Standardized constraints:
INFO - 16:23:45: g_1 = [ 0. -0.00450254 -0.01631536 -0.02646274 -0.03450254 -0.22600048
INFO - 16:23:45: -0.01399952]
INFO - 16:23:45: Design space:
INFO - 16:23:45: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:45: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:45: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:45: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:45: | x_1[1] | 0.75 | 0.8239490057569424 | 1.25 | float |
INFO - 16:23:45: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:45: *** End StructureScenario execution (time: 0:00:00.195504) ***
INFO - 16:23:45: *** Start PropulsionScenario execution ***
INFO - 16:23:45: PropulsionScenario
INFO - 16:23:45: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:45: MDO formulation: MDF
INFO - 16:23:45: Optimization problem:
INFO - 16:23:45: minimize 0.001*-y_4(x_3)
INFO - 16:23:45: with respect to x_3
INFO - 16:23:45: under the inequality constraints
INFO - 16:23:45: g_3(x_3) <= 0
INFO - 16:23:45: over the design space:
INFO - 16:23:45: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:45: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:45: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:45: | x_3 | 0.1 | 0.1563852262747091 | 1 | float |
INFO - 16:23:45: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:45: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:45: 2%|▏ | 1/50 [00:00<00:00, 108.99 it/sec, feas=True, obj=-2.22]
INFO - 16:23:45: 4%|▍ | 2/50 [00:00<00:00, 156.28 it/sec, feas=True, obj=-2.22]
INFO - 16:23:45: 6%|▌ | 3/50 [00:00<00:00, 89.79 it/sec, feas=True, obj=-2.22]
INFO - 16:23:45: Optimization result:
INFO - 16:23:45: Optimizer info:
INFO - 16:23:45: Status: None
INFO - 16:23:45: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:45: Solution:
INFO - 16:23:45: The solution is feasible.
INFO - 16:23:45: Objective: -2.2172812963553032
INFO - 16:23:45: Standardized constraints:
INFO - 16:23:45: g_3 = [-8.36407473e-01 -1.63592527e-01 6.21724894e-15 -1.83130596e-01]
INFO - 16:23:45: Design space:
INFO - 16:23:45: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:45: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:45: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:45: | x_3 | 0.1 | 0.1563852262747101 | 1 | float |
INFO - 16:23:45: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:45: *** End PropulsionScenario execution (time: 0:00:00.035549) ***
INFO - 16:23:45: *** Start AerodynamicsScenario execution ***
INFO - 16:23:45: AerodynamicsScenario
INFO - 16:23:45: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:45: MDO formulation: MDF
INFO - 16:23:45: Optimization problem:
INFO - 16:23:45: minimize 0.001*-y_4(x_2)
INFO - 16:23:45: with respect to x_2
INFO - 16:23:45: under the inequality constraints
INFO - 16:23:45: g_2(x_2) <= 0
INFO - 16:23:45: over the design space:
INFO - 16:23:45: +------+-------------+-------+-------------+-------+
INFO - 16:23:45: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:45: +------+-------------+-------+-------------+-------+
INFO - 16:23:45: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:45: +------+-------------+-------+-------------+-------+
INFO - 16:23:45: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:45: 2%|▏ | 1/50 [00:00<00:00, 80.95 it/sec, feas=True, obj=-2.22]
INFO - 16:23:45: Optimization result:
INFO - 16:23:45: Optimizer info:
INFO - 16:23:45: Status: 8
INFO - 16:23:45: Message: Positive directional derivative for linesearch
INFO - 16:23:45: Solution:
INFO - 16:23:45: The solution is feasible.
INFO - 16:23:45: Objective: -2.2172812963553032
INFO - 16:23:45: Standardized constraints:
INFO - 16:23:45: g_2 = -0.004841296871685996
INFO - 16:23:45: Design space:
INFO - 16:23:45: +------+-------------+-------+-------------+-------+
INFO - 16:23:45: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:45: +------+-------------+-------+-------------+-------+
INFO - 16:23:45: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:45: +------+-------------+-------+-------------+-------+
INFO - 16:23:45: *** End AerodynamicsScenario execution (time: 0:00:00.013811) ***
INFO - 16:23:45: *** Start StructureScenario execution ***
INFO - 16:23:45: StructureScenario
INFO - 16:23:45: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:45: MDO formulation: MDF
INFO - 16:23:45: Optimization problem:
INFO - 16:23:45: minimize 0.001*-y_4(x_1)
INFO - 16:23:45: with respect to x_1
INFO - 16:23:45: under the inequality constraints
INFO - 16:23:45: g_1(x_1) <= 0
INFO - 16:23:45: over the design space:
INFO - 16:23:45: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:45: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:45: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:45: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:45: | x_1[1] | 0.75 | 0.8239490057569424 | 1.25 | float |
INFO - 16:23:45: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:45: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:45: 2%|▏ | 1/50 [00:00<00:00, 102.91 it/sec, feas=True, obj=-2.22]
INFO - 16:23:45: Optimization result:
INFO - 16:23:45: Optimizer info:
INFO - 16:23:45: Status: 8
INFO - 16:23:45: Message: Positive directional derivative for linesearch
INFO - 16:23:45: Solution:
INFO - 16:23:45: The solution is feasible.
INFO - 16:23:45: Objective: -2.2172812963553032
INFO - 16:23:45: Standardized constraints:
INFO - 16:23:45: g_1 = [ 0. -0.00450254 -0.01631536 -0.02646274 -0.03450254 -0.22600048
INFO - 16:23:45: -0.01399952]
INFO - 16:23:45: Design space:
INFO - 16:23:45: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:45: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:45: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:45: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:45: | x_1[1] | 0.75 | 0.8239490057569424 | 1.25 | float |
INFO - 16:23:45: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:45: *** End StructureScenario execution (time: 0:00:00.011528) ***
INFO - 16:23:45: 39%|███▉ | 39/100 [00:28<00:44, 1.36 it/sec, feas=True, obj=-2.22]
INFO - 16:23:45: *** Start PropulsionScenario execution ***
INFO - 16:23:45: PropulsionScenario
INFO - 16:23:45: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:45: MDO formulation: MDF
INFO - 16:23:45: Optimization problem:
INFO - 16:23:45: minimize 0.001*-y_4(x_3)
INFO - 16:23:45: with respect to x_3
INFO - 16:23:45: under the inequality constraints
INFO - 16:23:45: g_3(x_3) <= 0
INFO - 16:23:45: over the design space:
INFO - 16:23:45: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:45: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:45: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:45: | x_3 | 0.1 | 0.1563852262747101 | 1 | float |
INFO - 16:23:45: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:45: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:45: 2%|▏ | 1/50 [00:00<00:01, 45.90 it/sec, feas=True, obj=-2.24]
INFO - 16:23:45: 4%|▍ | 2/50 [00:00<00:01, 35.32 it/sec, feas=True, obj=-2.24]
INFO - 16:23:45: 6%|▌ | 3/50 [00:00<00:01, 32.89 it/sec, feas=True, obj=-2.24]
INFO - 16:23:45: 8%|▊ | 4/50 [00:00<00:01, 35.77 it/sec, feas=True, obj=-2.24]
INFO - 16:23:45: Optimization result:
INFO - 16:23:45: Optimizer info:
INFO - 16:23:45: Status: None
INFO - 16:23:45: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:45: Solution:
INFO - 16:23:45: The solution is feasible.
INFO - 16:23:45: Objective: -2.236913939829729
INFO - 16:23:45: Standardized constraints:
INFO - 16:23:45: g_3 = [-8.28243423e-01 -1.71756577e-01 5.10702591e-15 -1.83040421e-01]
INFO - 16:23:45: Design space:
INFO - 16:23:45: +------+-------------+-------------------+-------------+-------+
INFO - 16:23:45: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:45: +------+-------------+-------------------+-------------+-------+
INFO - 16:23:45: | x_3 | 0.1 | 0.156486858916846 | 1 | float |
INFO - 16:23:45: +------+-------------+-------------------+-------------+-------+
INFO - 16:23:45: *** End PropulsionScenario execution (time: 0:00:00.115319) ***
INFO - 16:23:45: *** Start AerodynamicsScenario execution ***
INFO - 16:23:45: AerodynamicsScenario
INFO - 16:23:45: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:45: MDO formulation: MDF
INFO - 16:23:45: Optimization problem:
INFO - 16:23:45: minimize 0.001*-y_4(x_2)
INFO - 16:23:45: with respect to x_2
INFO - 16:23:45: under the inequality constraints
INFO - 16:23:45: g_2(x_2) <= 0
INFO - 16:23:45: over the design space:
INFO - 16:23:45: +------+-------------+-------+-------------+-------+
INFO - 16:23:45: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:45: +------+-------------+-------+-------------+-------+
INFO - 16:23:45: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:45: +------+-------------+-------+-------------+-------+
INFO - 16:23:45: Solving optimization problem with algorithm SLSQP:
WARNING - 16:23:45: Optimization found no feasible point; the least infeasible point is selected.
INFO - 16:23:45: 2%|▏ | 1/50 [00:00<00:00, 66.25 it/sec, feas=False, obj=-2.24]
INFO - 16:23:45: Optimization result:
INFO - 16:23:45: Optimizer info:
INFO - 16:23:45: Status: 8
INFO - 16:23:45: Message: Positive directional derivative for linesearch
INFO - 16:23:45: Solution:
WARNING - 16:23:45: The solution is not feasible.
INFO - 16:23:45: Objective: -2.236913939829729
INFO - 16:23:45: Standardized constraints:
INFO - 16:23:45: g_2 = 0.0024911183675078163
INFO - 16:23:45: Design space:
INFO - 16:23:45: +------+-------------+-------+-------------+-------+
INFO - 16:23:45: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:45: +------+-------------+-------+-------------+-------+
INFO - 16:23:45: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:45: +------+-------------+-------+-------------+-------+
INFO - 16:23:45: *** End AerodynamicsScenario execution (time: 0:00:00.016540) ***
INFO - 16:23:45: *** Start StructureScenario execution ***
INFO - 16:23:45: StructureScenario
INFO - 16:23:45: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:45: MDO formulation: MDF
INFO - 16:23:45: Optimization problem:
INFO - 16:23:45: minimize 0.001*-y_4(x_1)
INFO - 16:23:45: with respect to x_1
INFO - 16:23:45: under the inequality constraints
INFO - 16:23:45: g_1(x_1) <= 0
INFO - 16:23:45: over the design space:
INFO - 16:23:45: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:45: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:45: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:45: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:45: | x_1[1] | 0.75 | 0.8239490057569424 | 1.25 | float |
INFO - 16:23:45: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:45: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:45: 2%|▏ | 1/50 [00:00<00:00, 98.37 it/sec, feas=True, obj=-2.24]
WARNING - 16:23:45: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 0.0009157477359807847 is still above the tolerance 1e-06.
INFO - 16:23:45: 4%|▍ | 2/50 [00:00<00:01, 35.08 it/sec, feas=True, obj=-2.3]
INFO - 16:23:45: 6%|▌ | 3/50 [00:00<00:01, 30.33 it/sec, feas=True, obj=-2.3]
INFO - 16:23:45: 8%|▊ | 4/50 [00:00<00:01, 28.33 it/sec, feas=True, obj=-2.3]
INFO - 16:23:45: 10%|█ | 5/50 [00:00<00:01, 26.98 it/sec, feas=True, obj=-2.3]
INFO - 16:23:45: Optimization result:
INFO - 16:23:45: Optimizer info:
INFO - 16:23:45: Status: 8
INFO - 16:23:45: Message: Positive directional derivative for linesearch
INFO - 16:23:45: Solution:
INFO - 16:23:45: The solution is feasible.
INFO - 16:23:45: Objective: -2.297672157801864
INFO - 16:23:45: Standardized constraints:
INFO - 16:23:45: g_1 = [-2.17532722e-02 -1.30634548e-02 -2.05080686e-02 -2.87474841e-02
INFO - 16:23:45: -3.58123640e-02 -2.40000000e-01 2.65898414e-13]
INFO - 16:23:45: Design space:
INFO - 16:23:45: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:45: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:45: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:45: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:45: | x_1[1] | 0.75 | 0.7806436836756807 | 1.25 | float |
INFO - 16:23:45: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:45: *** End StructureScenario execution (time: 0:00:00.187550) ***
INFO - 16:23:45: *** Start PropulsionScenario execution ***
INFO - 16:23:45: PropulsionScenario
INFO - 16:23:45: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:45: MDO formulation: MDF
INFO - 16:23:45: Optimization problem:
INFO - 16:23:45: minimize 0.001*-y_4(x_3)
INFO - 16:23:45: with respect to x_3
INFO - 16:23:45: under the inequality constraints
INFO - 16:23:45: g_3(x_3) <= 0
INFO - 16:23:45: over the design space:
INFO - 16:23:45: +------+-------------+-------------------+-------------+-------+
INFO - 16:23:45: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:45: +------+-------------+-------------------+-------------+-------+
INFO - 16:23:45: | x_3 | 0.1 | 0.156486858916846 | 1 | float |
INFO - 16:23:45: +------+-------------+-------------------+-------------+-------+
INFO - 16:23:45: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:45: 2%|▏ | 1/50 [00:00<00:00, 108.91 it/sec, feas=True, obj=-2.3]
INFO - 16:23:45: 4%|▍ | 2/50 [00:00<00:00, 155.71 it/sec, feas=True, obj=-2.3]
INFO - 16:23:45: 6%|▌ | 3/50 [00:00<00:00, 89.66 it/sec, feas=True, obj=-2.3]
INFO - 16:23:45: Optimization result:
INFO - 16:23:45: Optimizer info:
INFO - 16:23:45: Status: None
INFO - 16:23:45: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:45: Solution:
INFO - 16:23:45: The solution is feasible.
INFO - 16:23:45: Objective: -2.2976721578018644
INFO - 16:23:45: Standardized constraints:
INFO - 16:23:45: g_3 = [-8.28419848e-01 -1.71580152e-01 4.88498131e-15 -1.83040421e-01]
INFO - 16:23:45: Design space:
INFO - 16:23:45: +------+-------------+-------------------+-------------+-------+
INFO - 16:23:45: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:45: +------+-------------+-------------------+-------------+-------+
INFO - 16:23:45: | x_3 | 0.1 | 0.156486858916846 | 1 | float |
INFO - 16:23:45: +------+-------------+-------------------+-------------+-------+
INFO - 16:23:45: *** End PropulsionScenario execution (time: 0:00:00.035755) ***
INFO - 16:23:45: *** Start AerodynamicsScenario execution ***
INFO - 16:23:45: AerodynamicsScenario
INFO - 16:23:45: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:45: MDO formulation: MDF
INFO - 16:23:45: Optimization problem:
INFO - 16:23:45: minimize 0.001*-y_4(x_2)
INFO - 16:23:45: with respect to x_2
INFO - 16:23:45: under the inequality constraints
INFO - 16:23:45: g_2(x_2) <= 0
INFO - 16:23:45: over the design space:
INFO - 16:23:45: +------+-------------+-------+-------------+-------+
INFO - 16:23:45: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:45: +------+-------------+-------+-------------+-------+
INFO - 16:23:45: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:45: +------+-------------+-------+-------------+-------+
INFO - 16:23:45: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:45: 2%|▏ | 1/50 [00:00<00:00, 108.91 it/sec, feas=False, obj=-2.3]
INFO - 16:23:45: 4%|▍ | 2/50 [00:00<00:00, 172.60 it/sec, feas=False, obj=-2.3]
INFO - 16:23:45: 6%|▌ | 3/50 [00:00<00:00, 213.84 it/sec, feas=False, obj=-2.3]
INFO - 16:23:45: 8%|▊ | 4/50 [00:00<00:00, 242.13 it/sec, feas=False, obj=-2.3]
INFO - 16:23:45: 10%|█ | 5/50 [00:00<00:00, 261.85 it/sec, feas=False, obj=-2.3]
INFO - 16:23:45: 12%|█▏ | 6/50 [00:00<00:00, 277.56 it/sec, feas=False, obj=-2.3]
INFO - 16:23:45: 14%|█▍ | 7/50 [00:00<00:00, 289.55 it/sec, feas=False, obj=-2.3]
INFO - 16:23:45: 16%|█▌ | 8/50 [00:00<00:00, 299.60 it/sec, feas=False, obj=-2.3]
INFO - 16:23:45: 18%|█▊ | 9/50 [00:00<00:00, 309.26 it/sec, feas=False, obj=-2.3]
INFO - 16:23:45: 20%|██ | 10/50 [00:00<00:00, 315.98 it/sec, feas=False, obj=-2.3]
INFO - 16:23:45: 22%|██▏ | 11/50 [00:00<00:00, 323.07 it/sec, feas=False, obj=-2.3]
INFO - 16:23:45: 24%|██▍ | 12/50 [00:00<00:00, 227.76 it/sec, feas=False, obj=-2.3]
INFO - 16:23:45: 26%|██▌ | 13/50 [00:00<00:00, 231.94 it/sec, feas=False, obj=-2.3]
INFO - 16:23:45: 28%|██▊ | 14/50 [00:00<00:00, 239.09 it/sec, feas=False, obj=-2.3]
INFO - 16:23:45: 30%|███ | 15/50 [00:00<00:00, 245.57 it/sec, feas=False, obj=-2.3]
INFO - 16:23:45: 32%|███▏ | 16/50 [00:00<00:00, 251.67 it/sec, feas=False, obj=-2.3]
INFO - 16:23:45: 34%|███▍ | 17/50 [00:00<00:00, 257.03 it/sec, feas=False, obj=-2.3]
INFO - 16:23:45: 36%|███▌ | 18/50 [00:00<00:00, 262.38 it/sec, feas=False, obj=-2.3]
INFO - 16:23:45: 38%|███▊ | 19/50 [00:00<00:00, 267.01 it/sec, feas=False, obj=-2.3]
INFO - 16:23:45: 40%|████ | 20/50 [00:00<00:00, 271.79 it/sec, feas=False, obj=-2.3]
INFO - 16:23:45: 42%|████▏ | 21/50 [00:00<00:00, 275.79 it/sec, feas=False, obj=-2.3]
INFO - 16:23:45: 44%|████▍ | 22/50 [00:00<00:00, 280.35 it/sec, feas=False, obj=-2.3]
INFO - 16:23:45: 46%|████▌ | 23/50 [00:00<00:00, 228.61 it/sec, feas=False, obj=-2.3]
INFO - 16:23:45: 48%|████▊ | 24/50 [00:00<00:00, 231.43 it/sec, feas=False, obj=-2.3]
INFO - 16:23:45: 50%|█████ | 25/50 [00:00<00:00, 235.21 it/sec, feas=False, obj=-2.3]
INFO - 16:23:45: 52%|█████▏ | 26/50 [00:00<00:00, 238.96 it/sec, feas=False, obj=-2.3]
INFO - 16:23:45: 54%|█████▍ | 27/50 [00:00<00:00, 242.54 it/sec, feas=False, obj=-2.3]
INFO - 16:23:45: 56%|█████▌ | 28/50 [00:00<00:00, 246.01 it/sec, feas=False, obj=-2.3]
INFO - 16:23:45: 58%|█████▊ | 29/50 [00:00<00:00, 249.27 it/sec, feas=False, obj=-2.3]
INFO - 16:23:45: 60%|██████ | 30/50 [00:00<00:00, 252.22 it/sec, feas=False, obj=-2.3]
INFO - 16:23:45: 62%|██████▏ | 31/50 [00:00<00:00, 255.23 it/sec, feas=False, obj=-2.3]
INFO - 16:23:45: 64%|██████▍ | 32/50 [00:00<00:00, 258.01 it/sec, feas=False, obj=-2.3]
INFO - 16:23:46: 66%|██████▌ | 33/50 [00:00<00:00, 226.75 it/sec, feas=False, obj=-2.3]
INFO - 16:23:46: 68%|██████▊ | 34/50 [00:00<00:00, 228.81 it/sec, feas=False, obj=-2.3]
INFO - 16:23:46: 70%|███████ | 35/50 [00:00<00:00, 231.58 it/sec, feas=False, obj=-2.3]
INFO - 16:23:46: 72%|███████▏ | 36/50 [00:00<00:00, 234.23 it/sec, feas=False, obj=-2.3]
INFO - 16:23:46: 74%|███████▍ | 37/50 [00:00<00:00, 236.86 it/sec, feas=False, obj=-2.3]
INFO - 16:23:46: 76%|███████▌ | 38/50 [00:00<00:00, 239.33 it/sec, feas=False, obj=-2.3]
INFO - 16:23:46: 78%|███████▊ | 39/50 [00:00<00:00, 241.80 it/sec, feas=False, obj=-2.3]
INFO - 16:23:46: 80%|████████ | 40/50 [00:00<00:00, 244.14 it/sec, feas=False, obj=-2.3]
INFO - 16:23:46: 82%|████████▏ | 41/50 [00:00<00:00, 246.35 it/sec, feas=False, obj=-2.3]
INFO - 16:23:46: 84%|████████▍ | 42/50 [00:00<00:00, 248.56 it/sec, feas=False, obj=-2.3]
INFO - 16:23:46: 86%|████████▌ | 43/50 [00:00<00:00, 226.71 it/sec, feas=False, obj=-2.3]
INFO - 16:23:46: 88%|████████▊ | 44/50 [00:00<00:00, 227.74 it/sec, feas=False, obj=-2.3]
INFO - 16:23:46: 90%|█████████ | 45/50 [00:00<00:00, 229.79 it/sec, feas=False, obj=-2.3]
INFO - 16:23:46: 92%|█████████▏| 46/50 [00:00<00:00, 231.83 it/sec, feas=False, obj=-2.3]
INFO - 16:23:46: 94%|█████████▍| 47/50 [00:00<00:00, 233.89 it/sec, feas=False, obj=-2.3]
WARNING - 16:23:46: Optimization found no feasible point; the least infeasible point is selected.
INFO - 16:23:46: 96%|█████████▌| 48/50 [00:00<00:00, 231.40 it/sec, feas=False, obj=-2.3]
INFO - 16:23:46: Optimization result:
INFO - 16:23:46: Optimizer info:
INFO - 16:23:46: Status: 8
INFO - 16:23:46: Message: Positive directional derivative for linesearch
INFO - 16:23:46: Solution:
WARNING - 16:23:46: The solution is not feasible.
INFO - 16:23:46: Objective: -2.2976721578018644
INFO - 16:23:46: Standardized constraints:
INFO - 16:23:46: g_2 = 0.0024911183675078163
INFO - 16:23:46: Design space:
INFO - 16:23:46: +------+-------------+-------+-------------+-------+
INFO - 16:23:46: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:46: +------+-------------+-------+-------------+-------+
INFO - 16:23:46: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:46: +------+-------------+-------+-------------+-------+
INFO - 16:23:46: *** End AerodynamicsScenario execution (time: 0:00:00.209206) ***
INFO - 16:23:46: *** Start StructureScenario execution ***
INFO - 16:23:46: StructureScenario
INFO - 16:23:46: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:46: MDO formulation: MDF
INFO - 16:23:46: Optimization problem:
INFO - 16:23:46: minimize 0.001*-y_4(x_1)
INFO - 16:23:46: with respect to x_1
INFO - 16:23:46: under the inequality constraints
INFO - 16:23:46: g_1(x_1) <= 0
INFO - 16:23:46: over the design space:
INFO - 16:23:46: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:46: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:46: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:46: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:46: | x_1[1] | 0.75 | 0.7806436836756807 | 1.25 | float |
INFO - 16:23:46: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:46: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:46: 2%|▏ | 1/50 [00:00<00:00, 66.15 it/sec, feas=True, obj=-2.3]
INFO - 16:23:46: Optimization result:
INFO - 16:23:46: Optimizer info:
INFO - 16:23:46: Status: 8
INFO - 16:23:46: Message: Positive directional derivative for linesearch
INFO - 16:23:46: Solution:
INFO - 16:23:46: The solution is feasible.
INFO - 16:23:46: Objective: -2.2976721578018644
INFO - 16:23:46: Standardized constraints:
INFO - 16:23:46: g_1 = [-2.17532722e-02 -1.30634548e-02 -2.05080686e-02 -2.87474841e-02
INFO - 16:23:46: -3.58123640e-02 -2.40000000e-01 2.65898414e-13]
INFO - 16:23:46: Design space:
INFO - 16:23:46: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:46: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:46: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:46: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:46: | x_1[1] | 0.75 | 0.7806436836756807 | 1.25 | float |
INFO - 16:23:46: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:46: *** End StructureScenario execution (time: 0:00:00.017250) ***
INFO - 16:23:46: 40%|████ | 40/100 [00:29<00:43, 1.37 it/sec, feas=False, obj=-2.3]
INFO - 16:23:46: *** Start PropulsionScenario execution ***
INFO - 16:23:46: PropulsionScenario
INFO - 16:23:46: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:46: MDO formulation: MDF
INFO - 16:23:46: Optimization problem:
INFO - 16:23:46: minimize 0.001*-y_4(x_3)
INFO - 16:23:46: with respect to x_3
INFO - 16:23:46: under the inequality constraints
INFO - 16:23:46: g_3(x_3) <= 0
INFO - 16:23:46: over the design space:
INFO - 16:23:46: +------+-------------+-------------------+-------------+-------+
INFO - 16:23:46: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:46: +------+-------------+-------------------+-------------+-------+
INFO - 16:23:46: | x_3 | 0.1 | 0.156486858916846 | 1 | float |
INFO - 16:23:46: +------+-------------+-------------------+-------------+-------+
INFO - 16:23:46: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:46: 2%|▏ | 1/50 [00:00<00:01, 37.30 it/sec, feas=True, obj=-2.29]
INFO - 16:23:46: 4%|▍ | 2/50 [00:00<00:01, 28.10 it/sec, feas=True, obj=-2.29]
INFO - 16:23:46: 6%|▌ | 3/50 [00:00<00:01, 25.76 it/sec, feas=True, obj=-2.29]
INFO - 16:23:46: 8%|▊ | 4/50 [00:00<00:01, 27.77 it/sec, feas=True, obj=-2.29]
INFO - 16:23:46: Optimization result:
INFO - 16:23:46: Optimizer info:
INFO - 16:23:46: Status: None
INFO - 16:23:46: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:46: Solution:
INFO - 16:23:46: The solution is feasible.
INFO - 16:23:46: Objective: -2.292911130133689
INFO - 16:23:46: Standardized constraints:
INFO - 16:23:46: g_3 = [-8.04889850e-01 -1.95110150e-01 2.44249065e-15 -1.82776319e-01]
INFO - 16:23:46: Design space:
INFO - 16:23:46: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:46: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:46: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:46: | x_3 | 0.1 | 0.1567518093648367 | 1 | float |
INFO - 16:23:46: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:46: *** End PropulsionScenario execution (time: 0:00:00.146800) ***
INFO - 16:23:46: *** Start AerodynamicsScenario execution ***
INFO - 16:23:46: AerodynamicsScenario
INFO - 16:23:46: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:46: MDO formulation: MDF
INFO - 16:23:46: Optimization problem:
INFO - 16:23:46: minimize 0.001*-y_4(x_2)
INFO - 16:23:46: with respect to x_2
INFO - 16:23:46: under the inequality constraints
INFO - 16:23:46: g_2(x_2) <= 0
INFO - 16:23:46: over the design space:
INFO - 16:23:46: +------+-------------+-------+-------------+-------+
INFO - 16:23:46: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:46: +------+-------------+-------+-------------+-------+
INFO - 16:23:46: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:46: +------+-------------+-------+-------------+-------+
INFO - 16:23:46: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:46: 2%|▏ | 1/50 [00:00<00:00, 89.17 it/sec, feas=True, obj=-2.29]
INFO - 16:23:46: Optimization result:
INFO - 16:23:46: Optimizer info:
INFO - 16:23:46: Status: 8
INFO - 16:23:46: Message: Positive directional derivative for linesearch
INFO - 16:23:46: Solution:
INFO - 16:23:46: The solution is feasible.
INFO - 16:23:46: Objective: -2.292911130133689
INFO - 16:23:46: Standardized constraints:
INFO - 16:23:46: g_2 = -2.220446049250313e-16
INFO - 16:23:46: Design space:
INFO - 16:23:46: +------+-------------+-------+-------------+-------+
INFO - 16:23:46: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:46: +------+-------------+-------+-------------+-------+
INFO - 16:23:46: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:46: +------+-------------+-------+-------------+-------+
INFO - 16:23:46: *** End AerodynamicsScenario execution (time: 0:00:00.012925) ***
INFO - 16:23:46: *** Start StructureScenario execution ***
INFO - 16:23:46: StructureScenario
INFO - 16:23:46: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:46: MDO formulation: MDF
INFO - 16:23:46: Optimization problem:
INFO - 16:23:46: minimize 0.001*-y_4(x_1)
INFO - 16:23:46: with respect to x_1
INFO - 16:23:46: under the inequality constraints
INFO - 16:23:46: g_1(x_1) <= 0
INFO - 16:23:46: over the design space:
INFO - 16:23:46: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:46: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:46: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:46: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:46: | x_1[1] | 0.75 | 0.7806436836756807 | 1.25 | float |
INFO - 16:23:46: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:46: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:46: 2%|▏ | 1/50 [00:00<00:00, 96.88 it/sec, feas=True, obj=-2.29]
INFO - 16:23:46: Optimization result:
INFO - 16:23:46: Optimizer info:
INFO - 16:23:46: Status: 8
INFO - 16:23:46: Message: Positive directional derivative for linesearch
INFO - 16:23:46: Solution:
INFO - 16:23:46: The solution is feasible.
INFO - 16:23:46: Objective: -2.292911130133689
INFO - 16:23:46: Standardized constraints:
INFO - 16:23:46: g_1 = [-1.59589593e-03 -2.02868890e-03 -1.31333010e-02 -2.32802973e-02
INFO - 16:23:46: -3.14967236e-02 -2.40000000e-01 2.65898414e-13]
INFO - 16:23:46: Design space:
INFO - 16:23:46: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:46: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:46: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:46: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:46: | x_1[1] | 0.75 | 0.7806436836756807 | 1.25 | float |
INFO - 16:23:46: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:46: *** End StructureScenario execution (time: 0:00:00.012282) ***
INFO - 16:23:46: *** Start PropulsionScenario execution ***
INFO - 16:23:46: PropulsionScenario
INFO - 16:23:46: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:46: MDO formulation: MDF
INFO - 16:23:46: Optimization problem:
INFO - 16:23:46: minimize 0.001*-y_4(x_3)
INFO - 16:23:46: with respect to x_3
INFO - 16:23:46: under the inequality constraints
INFO - 16:23:46: g_3(x_3) <= 0
INFO - 16:23:46: over the design space:
INFO - 16:23:46: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:46: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:46: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:46: | x_3 | 0.1 | 0.1567518093648367 | 1 | float |
INFO - 16:23:46: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:46: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:46: 2%|▏ | 1/50 [00:00<00:00, 108.80 it/sec, feas=True, obj=-2.29]
INFO - 16:23:46: Optimization result:
INFO - 16:23:46: Optimizer info:
INFO - 16:23:46: Status: 8
INFO - 16:23:46: Message: Positive directional derivative for linesearch
INFO - 16:23:46: Solution:
INFO - 16:23:46: The solution is feasible.
INFO - 16:23:46: Objective: -2.292911130133689
INFO - 16:23:46: Standardized constraints:
INFO - 16:23:46: g_3 = [-8.04889850e-01 -1.95110150e-01 2.44249065e-15 -1.82776319e-01]
INFO - 16:23:46: Design space:
INFO - 16:23:46: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:46: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:46: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:46: | x_3 | 0.1 | 0.1567518093648367 | 1 | float |
INFO - 16:23:46: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:46: *** End PropulsionScenario execution (time: 0:00:00.010847) ***
INFO - 16:23:46: 41%|████ | 41/100 [00:29<00:42, 1.39 it/sec, feas=True, obj=-2.29]
INFO - 16:23:46: *** Start PropulsionScenario execution ***
INFO - 16:23:46: PropulsionScenario
INFO - 16:23:46: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:46: MDO formulation: MDF
INFO - 16:23:46: Optimization problem:
INFO - 16:23:46: minimize 0.001*-y_4(x_3)
INFO - 16:23:46: with respect to x_3
INFO - 16:23:46: under the inequality constraints
INFO - 16:23:46: g_3(x_3) <= 0
INFO - 16:23:46: over the design space:
INFO - 16:23:46: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:46: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:46: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:46: | x_3 | 0.1 | 0.1567518093648367 | 1 | float |
INFO - 16:23:46: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:46: Solving optimization problem with algorithm SLSQP:
WARNING - 16:23:46: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 6.724932466608626e-05 is still above the tolerance 1e-06.
INFO - 16:23:46: 2%|▏ | 1/50 [00:00<00:01, 33.76 it/sec, feas=True, obj=-2.29]
INFO - 16:23:46: 4%|▍ | 2/50 [00:00<00:01, 27.22 it/sec, feas=True, obj=-2.29]
WARNING - 16:23:46: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 6.724932466608626e-05 is still above the tolerance 1e-06.
INFO - 16:23:46: 6%|▌ | 3/50 [00:00<00:01, 28.92 it/sec, feas=True, obj=-2.29]
WARNING - 16:23:46: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 6.724932466608626e-05 is still above the tolerance 1e-06.
INFO - 16:23:46: 8%|▊ | 4/50 [00:00<00:01, 29.85 it/sec, feas=True, obj=-2.29]
INFO - 16:23:46: Optimization result:
INFO - 16:23:46: Optimizer info:
INFO - 16:23:46: Status: None
INFO - 16:23:46: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:46: Solution:
INFO - 16:23:46: The solution is feasible.
INFO - 16:23:46: Objective: -2.2899901652148573
INFO - 16:23:46: Standardized constraints:
INFO - 16:23:46: g_3 = [-8.23719214e-01 -1.76280786e-01 4.44089210e-16 -1.83166063e-01]
INFO - 16:23:46: Design space:
INFO - 16:23:46: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:46: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:46: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:46: | x_3 | 0.1 | 0.1569972318613097 | 1 | float |
INFO - 16:23:46: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:46: *** End PropulsionScenario execution (time: 0:00:00.136622) ***
INFO - 16:23:46: *** Start AerodynamicsScenario execution ***
INFO - 16:23:46: AerodynamicsScenario
INFO - 16:23:46: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:46: MDO formulation: MDF
INFO - 16:23:46: Optimization problem:
INFO - 16:23:46: minimize 0.001*-y_4(x_2)
INFO - 16:23:46: with respect to x_2
INFO - 16:23:46: under the inequality constraints
INFO - 16:23:46: g_2(x_2) <= 0
INFO - 16:23:46: over the design space:
INFO - 16:23:46: +------+-------------+-------+-------------+-------+
INFO - 16:23:46: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:46: +------+-------------+-------+-------------+-------+
INFO - 16:23:46: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:46: +------+-------------+-------+-------------+-------+
INFO - 16:23:46: Solving optimization problem with algorithm SLSQP:
WARNING - 16:23:46: Optimization found no feasible point; the least infeasible point is selected.
INFO - 16:23:46: 2%|▏ | 1/50 [00:00<00:00, 61.07 it/sec, feas=False, obj=-2.29]
INFO - 16:23:46: Optimization result:
INFO - 16:23:46: Optimizer info:
INFO - 16:23:46: Status: 8
INFO - 16:23:46: Message: Positive directional derivative for linesearch
INFO - 16:23:46: Solution:
WARNING - 16:23:46: The solution is not feasible.
INFO - 16:23:46: Objective: -2.2899901652148578
INFO - 16:23:46: Standardized constraints:
INFO - 16:23:46: g_2 = 0.003099396405821242
INFO - 16:23:46: Design space:
INFO - 16:23:46: +------+-------------+-------+-------------+-------+
INFO - 16:23:46: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:46: +------+-------------+-------+-------------+-------+
INFO - 16:23:46: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:46: +------+-------------+-------+-------------+-------+
INFO - 16:23:46: *** End AerodynamicsScenario execution (time: 0:00:00.017987) ***
INFO - 16:23:46: *** Start StructureScenario execution ***
INFO - 16:23:46: StructureScenario
INFO - 16:23:46: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:46: MDO formulation: MDF
INFO - 16:23:46: Optimization problem:
INFO - 16:23:46: minimize 0.001*-y_4(x_1)
INFO - 16:23:46: with respect to x_1
INFO - 16:23:46: under the inequality constraints
INFO - 16:23:46: g_1(x_1) <= 0
INFO - 16:23:46: over the design space:
INFO - 16:23:46: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:46: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:46: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:46: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:46: | x_1[1] | 0.75 | 0.7806436836756807 | 1.25 | float |
INFO - 16:23:46: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:46: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:46: 2%|▏ | 1/50 [00:00<00:00, 82.61 it/sec, feas=True, obj=-2.29]
WARNING - 16:23:46: MDAGaussSeidel has reached its maximum number of unsuccessful iterations, but the normalized residual norm 0.0009157477359807847 is still above the tolerance 1e-06.
INFO - 16:23:46: 4%|▍ | 2/50 [00:00<00:00, 64.02 it/sec, feas=True, obj=-2.29]
INFO - 16:23:46: 6%|▌ | 3/50 [00:00<00:00, 75.78 it/sec, feas=True, obj=-2.29]
INFO - 16:23:46: Optimization result:
INFO - 16:23:46: Optimizer info:
INFO - 16:23:46: Status: None
INFO - 16:23:46: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:46: Solution:
INFO - 16:23:46: The solution is feasible.
INFO - 16:23:46: Objective: -2.2899901652148573
INFO - 16:23:46: Standardized constraints:
INFO - 16:23:46: g_1 = [-2.67341895e-02 -1.57840942e-02 -2.23235586e-02 -3.00918811e-02
INFO - 16:23:46: -3.68726977e-02 -2.40000000e-01 2.65898414e-13]
INFO - 16:23:46: Design space:
INFO - 16:23:46: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:46: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:46: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:46: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:46: | x_1[1] | 0.75 | 0.7806436836756807 | 1.25 | float |
INFO - 16:23:46: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:46: *** End StructureScenario execution (time: 0:00:00.042013) ***
INFO - 16:23:46: *** Start PropulsionScenario execution ***
INFO - 16:23:46: PropulsionScenario
INFO - 16:23:46: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:46: MDO formulation: MDF
INFO - 16:23:46: Optimization problem:
INFO - 16:23:46: minimize 0.001*-y_4(x_3)
INFO - 16:23:46: with respect to x_3
INFO - 16:23:46: under the inequality constraints
INFO - 16:23:46: g_3(x_3) <= 0
INFO - 16:23:46: over the design space:
INFO - 16:23:46: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:46: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:46: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:46: | x_3 | 0.1 | 0.1569972318613097 | 1 | float |
INFO - 16:23:46: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:46: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:46: 2%|▏ | 1/50 [00:00<00:00, 91.87 it/sec, feas=True, obj=-2.29]
INFO - 16:23:46: Optimization result:
INFO - 16:23:46: Optimizer info:
INFO - 16:23:46: Status: 8
INFO - 16:23:46: Message: Positive directional derivative for linesearch
INFO - 16:23:46: Solution:
INFO - 16:23:46: The solution is feasible.
INFO - 16:23:46: Objective: -2.2899901652148573
INFO - 16:23:46: Standardized constraints:
INFO - 16:23:46: g_3 = [-8.23719214e-01 -1.76280786e-01 4.44089210e-16 -1.83166063e-01]
INFO - 16:23:46: Design space:
INFO - 16:23:46: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:46: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:46: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:46: | x_3 | 0.1 | 0.1569972318613097 | 1 | float |
INFO - 16:23:46: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:46: *** End PropulsionScenario execution (time: 0:00:00.012751) ***
INFO - 16:23:46: *** Start AerodynamicsScenario execution ***
INFO - 16:23:46: AerodynamicsScenario
INFO - 16:23:46: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:46: MDO formulation: MDF
INFO - 16:23:46: Optimization problem:
INFO - 16:23:46: minimize 0.001*-y_4(x_2)
INFO - 16:23:46: with respect to x_2
INFO - 16:23:46: under the inequality constraints
INFO - 16:23:46: g_2(x_2) <= 0
INFO - 16:23:46: over the design space:
INFO - 16:23:46: +------+-------------+-------+-------------+-------+
INFO - 16:23:46: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:46: +------+-------------+-------+-------------+-------+
INFO - 16:23:46: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:46: +------+-------------+-------+-------------+-------+
INFO - 16:23:46: Solving optimization problem with algorithm SLSQP:
WARNING - 16:23:46: Optimization found no feasible point; the least infeasible point is selected.
INFO - 16:23:46: 2%|▏ | 1/50 [00:00<00:00, 88.12 it/sec, feas=False, obj=-2.29]
INFO - 16:23:46: Optimization result:
INFO - 16:23:46: Optimizer info:
INFO - 16:23:46: Status: 8
INFO - 16:23:46: Message: Positive directional derivative for linesearch
INFO - 16:23:46: Solution:
WARNING - 16:23:46: The solution is not feasible.
INFO - 16:23:46: Objective: -2.2899901652148573
INFO - 16:23:46: Standardized constraints:
INFO - 16:23:46: g_2 = 0.003099396405821242
INFO - 16:23:46: Design space:
INFO - 16:23:46: +------+-------------+-------+-------------+-------+
INFO - 16:23:46: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:46: +------+-------------+-------+-------------+-------+
INFO - 16:23:46: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:46: +------+-------------+-------+-------------+-------+
INFO - 16:23:46: *** End AerodynamicsScenario execution (time: 0:00:00.013029) ***
INFO - 16:23:46: *** Start StructureScenario execution ***
INFO - 16:23:46: StructureScenario
INFO - 16:23:46: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:46: MDO formulation: MDF
INFO - 16:23:46: Optimization problem:
INFO - 16:23:46: minimize 0.001*-y_4(x_1)
INFO - 16:23:46: with respect to x_1
INFO - 16:23:46: under the inequality constraints
INFO - 16:23:46: g_1(x_1) <= 0
INFO - 16:23:46: over the design space:
INFO - 16:23:46: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:46: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:46: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:46: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:46: | x_1[1] | 0.75 | 0.7806436836756807 | 1.25 | float |
INFO - 16:23:46: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:46: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:46: 2%|▏ | 1/50 [00:00<00:00, 101.21 it/sec, feas=True, obj=-2.29]
WARNING - 16:23:46: MDAGaussSeidel has reached its maximum number of unsuccessful iterations, but the normalized residual norm 0.0009157477359807847 is still above the tolerance 1e-06.
INFO - 16:23:46: 4%|▍ | 2/50 [00:00<00:00, 78.01 it/sec, feas=True, obj=-2.29]
INFO - 16:23:46: 6%|▌ | 3/50 [00:00<00:00, 91.38 it/sec, feas=True, obj=-2.29]
INFO - 16:23:46: Optimization result:
INFO - 16:23:46: Optimizer info:
INFO - 16:23:46: Status: None
INFO - 16:23:46: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:46: Solution:
INFO - 16:23:46: The solution is feasible.
INFO - 16:23:46: Objective: -2.2899901652148573
INFO - 16:23:46: Standardized constraints:
INFO - 16:23:46: g_1 = [-2.67341895e-02 -1.57840942e-02 -2.23235586e-02 -3.00918811e-02
INFO - 16:23:46: -3.68726977e-02 -2.40000000e-01 2.65898414e-13]
INFO - 16:23:46: Design space:
INFO - 16:23:46: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:46: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:46: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:46: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:46: | x_1[1] | 0.75 | 0.7806436836756807 | 1.25 | float |
INFO - 16:23:46: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:46: *** End StructureScenario execution (time: 0:00:00.035197) ***
INFO - 16:23:46: 42%|████▏ | 42/100 [00:29<00:41, 1.41 it/sec, feas=False, obj=-2.29]
INFO - 16:23:46: *** Start PropulsionScenario execution ***
INFO - 16:23:46: PropulsionScenario
INFO - 16:23:46: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:46: MDO formulation: MDF
INFO - 16:23:46: Optimization problem:
INFO - 16:23:46: minimize 0.001*-y_4(x_3)
INFO - 16:23:46: with respect to x_3
INFO - 16:23:46: under the inequality constraints
INFO - 16:23:46: g_3(x_3) <= 0
INFO - 16:23:46: over the design space:
INFO - 16:23:46: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:46: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:46: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:46: | x_3 | 0.1 | 0.1569972318613097 | 1 | float |
INFO - 16:23:46: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:46: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:46: 2%|▏ | 1/50 [00:00<00:01, 37.21 it/sec, feas=False, obj=-2.31]
INFO - 16:23:46: 4%|▍ | 2/50 [00:00<00:01, 36.97 it/sec, feas=True, obj=-2.31]
WARNING - 16:23:46: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 6.724932466608626e-05 is still above the tolerance 1e-06.
INFO - 16:23:46: 6%|▌ | 3/50 [00:00<00:01, 29.81 it/sec, feas=False, obj=-2.31]
INFO - 16:23:46: 8%|▊ | 4/50 [00:00<00:01, 27.07 it/sec, feas=True, obj=-2.31]
INFO - 16:23:46: Optimization result:
INFO - 16:23:46: Optimizer info:
INFO - 16:23:46: Status: 8
INFO - 16:23:46: Message: Positive directional derivative for linesearch
INFO - 16:23:46: Solution:
INFO - 16:23:46: The solution is feasible.
INFO - 16:23:46: Objective: -2.3052451574521258
INFO - 16:23:46: Standardized constraints:
INFO - 16:23:46: g_3 = [-8.06616137e-01 -1.93383863e-01 2.22044605e-16 -1.83255000e-01]
INFO - 16:23:46: Design space:
INFO - 16:23:46: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:46: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:46: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:46: | x_3 | 0.1 | 0.1562447456462875 | 1 | float |
INFO - 16:23:46: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:46: *** End PropulsionScenario execution (time: 0:00:00.149988) ***
INFO - 16:23:46: *** Start AerodynamicsScenario execution ***
INFO - 16:23:46: AerodynamicsScenario
INFO - 16:23:46: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:46: MDO formulation: MDF
INFO - 16:23:46: Optimization problem:
INFO - 16:23:46: minimize 0.001*-y_4(x_2)
INFO - 16:23:46: with respect to x_2
INFO - 16:23:46: under the inequality constraints
INFO - 16:23:46: g_2(x_2) <= 0
INFO - 16:23:46: over the design space:
INFO - 16:23:46: +------+-------------+-------+-------------+-------+
INFO - 16:23:46: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:46: +------+-------------+-------+-------------+-------+
INFO - 16:23:46: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:46: +------+-------------+-------+-------------+-------+
INFO - 16:23:46: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:46: 2%|▏ | 1/50 [00:00<00:00, 105.43 it/sec, feas=True, obj=-2.31]
INFO - 16:23:46: Optimization result:
INFO - 16:23:46: Optimizer info:
INFO - 16:23:46: Status: 8
INFO - 16:23:46: Message: Positive directional derivative for linesearch
INFO - 16:23:46: Solution:
INFO - 16:23:46: The solution is feasible.
INFO - 16:23:46: Objective: -2.3052451574521258
INFO - 16:23:46: Standardized constraints:
INFO - 16:23:46: g_2 = 0.0
INFO - 16:23:46: Design space:
INFO - 16:23:46: +------+-------------+-------+-------------+-------+
INFO - 16:23:46: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:46: +------+-------------+-------+-------------+-------+
INFO - 16:23:46: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:46: +------+-------------+-------+-------------+-------+
INFO - 16:23:46: *** End AerodynamicsScenario execution (time: 0:00:00.011073) ***
INFO - 16:23:46: *** Start StructureScenario execution ***
INFO - 16:23:46: StructureScenario
INFO - 16:23:46: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:46: MDO formulation: MDF
INFO - 16:23:46: Optimization problem:
INFO - 16:23:46: minimize 0.001*-y_4(x_1)
INFO - 16:23:46: with respect to x_1
INFO - 16:23:46: under the inequality constraints
INFO - 16:23:46: g_1(x_1) <= 0
INFO - 16:23:46: over the design space:
INFO - 16:23:46: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:46: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:46: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:46: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:46: | x_1[1] | 0.75 | 0.7806436836756807 | 1.25 | float |
INFO - 16:23:46: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:46: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:46: 2%|▏ | 1/50 [00:00<00:00, 98.77 it/sec, feas=True, obj=-2.31]
INFO - 16:23:46: 4%|▍ | 2/50 [00:00<00:00, 100.41 it/sec, feas=True, obj=-2.31]
INFO - 16:23:46: 6%|▌ | 3/50 [00:00<00:00, 68.88 it/sec, feas=True, obj=-2.31]
INFO - 16:23:46: Optimization result:
INFO - 16:23:46: Optimizer info:
INFO - 16:23:46: Status: None
INFO - 16:23:46: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:46: Solution:
INFO - 16:23:46: The solution is feasible.
INFO - 16:23:46: Objective: -2.3052451574521258
INFO - 16:23:46: Standardized constraints:
INFO - 16:23:46: g_1 = [-1.59589593e-03 -2.02868890e-03 -1.31333010e-02 -2.32802973e-02
INFO - 16:23:46: -3.14967236e-02 -2.40000000e-01 2.65898414e-13]
INFO - 16:23:46: Design space:
INFO - 16:23:46: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:46: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:46: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:46: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:46: | x_1[1] | 0.75 | 0.7806436836756807 | 1.25 | float |
INFO - 16:23:46: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:46: *** End StructureScenario execution (time: 0:00:00.045919) ***
INFO - 16:23:46: *** Start PropulsionScenario execution ***
INFO - 16:23:46: PropulsionScenario
INFO - 16:23:46: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:46: MDO formulation: MDF
INFO - 16:23:46: Optimization problem:
INFO - 16:23:46: minimize 0.001*-y_4(x_3)
INFO - 16:23:46: with respect to x_3
INFO - 16:23:46: under the inequality constraints
INFO - 16:23:46: g_3(x_3) <= 0
INFO - 16:23:46: over the design space:
INFO - 16:23:46: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:46: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:46: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:46: | x_3 | 0.1 | 0.1562447456462875 | 1 | float |
INFO - 16:23:46: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:46: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:46: 2%|▏ | 1/50 [00:00<00:00, 75.95 it/sec, feas=True, obj=-2.31]
INFO - 16:23:46: Optimization result:
INFO - 16:23:46: Optimizer info:
INFO - 16:23:46: Status: 8
INFO - 16:23:46: Message: Positive directional derivative for linesearch
INFO - 16:23:46: Solution:
INFO - 16:23:46: The solution is feasible.
INFO - 16:23:46: Objective: -2.3052451574521258
INFO - 16:23:46: Standardized constraints:
INFO - 16:23:46: g_3 = [-8.06616137e-01 -1.93383863e-01 2.22044605e-16 -1.83255000e-01]
INFO - 16:23:46: Design space:
INFO - 16:23:46: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:46: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:46: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:46: | x_3 | 0.1 | 0.1562447456462875 | 1 | float |
INFO - 16:23:46: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:46: *** End PropulsionScenario execution (time: 0:00:00.014992) ***
INFO - 16:23:46: 43%|████▎ | 43/100 [00:29<00:39, 1.43 it/sec, feas=True, obj=-2.31]
INFO - 16:23:46: *** Start PropulsionScenario execution ***
INFO - 16:23:46: PropulsionScenario
INFO - 16:23:46: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:46: MDO formulation: MDF
INFO - 16:23:46: Optimization problem:
INFO - 16:23:46: minimize 0.001*-y_4(x_3)
INFO - 16:23:46: with respect to x_3
INFO - 16:23:46: under the inequality constraints
INFO - 16:23:46: g_3(x_3) <= 0
INFO - 16:23:46: over the design space:
INFO - 16:23:46: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:46: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:46: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:46: | x_3 | 0.1 | 0.1562447456462875 | 1 | float |
INFO - 16:23:46: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:46: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:46: 2%|▏ | 1/50 [00:00<00:01, 37.63 it/sec, feas=True, obj=-2.27]
INFO - 16:23:46: 4%|▍ | 2/50 [00:00<00:01, 29.30 it/sec, feas=True, obj=-2.27]
INFO - 16:23:47: 6%|▌ | 3/50 [00:00<00:01, 26.87 it/sec, feas=True, obj=-2.27]
INFO - 16:23:47: Optimization result:
INFO - 16:23:47: Optimizer info:
INFO - 16:23:47: Status: 8
INFO - 16:23:47: Message: Positive directional derivative for linesearch
INFO - 16:23:47: Solution:
INFO - 16:23:47: The solution is feasible.
INFO - 16:23:47: Objective: -2.2684989665435027
INFO - 16:23:47: Standardized constraints:
INFO - 16:23:47: g_3 = [-8.26344733e-01 -1.73655267e-01 2.88657986e-15 -1.83153631e-01]
INFO - 16:23:47: Design space:
INFO - 16:23:47: +------+-------------+-------------------+-------------+-------+
INFO - 16:23:47: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:47: +------+-------------+-------------------+-------------+-------+
INFO - 16:23:47: | x_3 | 0.1 | 0.156624909640078 | 1 | float |
INFO - 16:23:47: +------+-------------+-------------------+-------------+-------+
INFO - 16:23:47: *** End PropulsionScenario execution (time: 0:00:00.113986) ***
INFO - 16:23:47: *** Start AerodynamicsScenario execution ***
INFO - 16:23:47: AerodynamicsScenario
INFO - 16:23:47: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:47: MDO formulation: MDF
INFO - 16:23:47: Optimization problem:
INFO - 16:23:47: minimize 0.001*-y_4(x_2)
INFO - 16:23:47: with respect to x_2
INFO - 16:23:47: under the inequality constraints
INFO - 16:23:47: g_2(x_2) <= 0
INFO - 16:23:47: over the design space:
INFO - 16:23:47: +------+-------------+-------+-------------+-------+
INFO - 16:23:47: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:47: +------+-------------+-------+-------------+-------+
INFO - 16:23:47: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:47: +------+-------------+-------+-------------+-------+
INFO - 16:23:47: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:47: 2%|▏ | 1/50 [00:00<00:00, 75.13 it/sec, feas=False, obj=-2.27]
INFO - 16:23:47: 4%|▍ | 2/50 [00:00<00:00, 119.13 it/sec, feas=False, obj=-2.27]
INFO - 16:23:47: 6%|▌ | 3/50 [00:00<00:00, 147.77 it/sec, feas=False, obj=-2.27]
INFO - 16:23:47: 8%|▊ | 4/50 [00:00<00:00, 167.32 it/sec, feas=False, obj=-2.27]
INFO - 16:23:47: 10%|█ | 5/50 [00:00<00:00, 182.46 it/sec, feas=False, obj=-2.27]
INFO - 16:23:47: 12%|█▏ | 6/50 [00:00<00:00, 194.15 it/sec, feas=False, obj=-2.27]
INFO - 16:23:47: 14%|█▍ | 7/50 [00:00<00:00, 204.13 it/sec, feas=False, obj=-2.27]
WARNING - 16:23:47: Optimization found no feasible point; the least infeasible point is selected.
INFO - 16:23:47: 16%|█▌ | 8/50 [00:00<00:00, 178.44 it/sec, feas=False, obj=-2.27]
INFO - 16:23:47: Optimization result:
INFO - 16:23:47: Optimizer info:
INFO - 16:23:47: Status: 8
INFO - 16:23:47: Message: Positive directional derivative for linesearch
INFO - 16:23:47: Solution:
WARNING - 16:23:47: The solution is not feasible.
INFO - 16:23:47: Objective: -2.2684989665435027
INFO - 16:23:47: Standardized constraints:
INFO - 16:23:47: g_2 = 0.0027615609342461767
INFO - 16:23:47: Design space:
INFO - 16:23:47: +------+-------------+-------+-------------+-------+
INFO - 16:23:47: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:47: +------+-------------+-------+-------------+-------+
INFO - 16:23:47: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:47: +------+-------------+-------+-------------+-------+
INFO - 16:23:47: *** End AerodynamicsScenario execution (time: 0:00:00.046534) ***
INFO - 16:23:47: *** Start StructureScenario execution ***
INFO - 16:23:47: StructureScenario
INFO - 16:23:47: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:47: MDO formulation: MDF
INFO - 16:23:47: Optimization problem:
INFO - 16:23:47: minimize 0.001*-y_4(x_1)
INFO - 16:23:47: with respect to x_1
INFO - 16:23:47: under the inequality constraints
INFO - 16:23:47: g_1(x_1) <= 0
INFO - 16:23:47: over the design space:
INFO - 16:23:47: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:47: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:47: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:47: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:47: | x_1[1] | 0.75 | 0.7806436836756807 | 1.25 | float |
INFO - 16:23:47: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:47: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:47: 2%|▏ | 1/50 [00:00<00:00, 76.24 it/sec, feas=True, obj=-2.27]
INFO - 16:23:47: Optimization result:
INFO - 16:23:47: Optimizer info:
INFO - 16:23:47: Status: 8
INFO - 16:23:47: Message: Positive directional derivative for linesearch
INFO - 16:23:47: Solution:
INFO - 16:23:47: The solution is feasible.
INFO - 16:23:47: Objective: -2.2684989665435027
INFO - 16:23:47: Standardized constraints:
INFO - 16:23:47: g_1 = [-2.39649505e-02 -1.42717917e-02 -2.13145280e-02 -2.93447509e-02
INFO - 16:23:47: -3.62834749e-02 -2.40000000e-01 2.65898414e-13]
INFO - 16:23:47: Design space:
INFO - 16:23:47: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:47: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:47: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:47: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:47: | x_1[1] | 0.75 | 0.7806436836756807 | 1.25 | float |
INFO - 16:23:47: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:47: *** End StructureScenario execution (time: 0:00:00.015115) ***
INFO - 16:23:47: *** Start PropulsionScenario execution ***
INFO - 16:23:47: PropulsionScenario
INFO - 16:23:47: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:47: MDO formulation: MDF
INFO - 16:23:47: Optimization problem:
INFO - 16:23:47: minimize 0.001*-y_4(x_3)
INFO - 16:23:47: with respect to x_3
INFO - 16:23:47: under the inequality constraints
INFO - 16:23:47: g_3(x_3) <= 0
INFO - 16:23:47: over the design space:
INFO - 16:23:47: +------+-------------+-------------------+-------------+-------+
INFO - 16:23:47: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:47: +------+-------------+-------------------+-------------+-------+
INFO - 16:23:47: | x_3 | 0.1 | 0.156624909640078 | 1 | float |
INFO - 16:23:47: +------+-------------+-------------------+-------------+-------+
INFO - 16:23:47: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:47: 2%|▏ | 1/50 [00:00<00:00, 108.88 it/sec, feas=True, obj=-2.27]
INFO - 16:23:47: Optimization result:
INFO - 16:23:47: Optimizer info:
INFO - 16:23:47: Status: 8
INFO - 16:23:47: Message: Positive directional derivative for linesearch
INFO - 16:23:47: Solution:
INFO - 16:23:47: The solution is feasible.
INFO - 16:23:47: Objective: -2.2684989665435027
INFO - 16:23:47: Standardized constraints:
INFO - 16:23:47: g_3 = [-8.26344733e-01 -1.73655267e-01 2.88657986e-15 -1.83153631e-01]
INFO - 16:23:47: Design space:
INFO - 16:23:47: +------+-------------+-------------------+-------------+-------+
INFO - 16:23:47: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:47: +------+-------------+-------------------+-------------+-------+
INFO - 16:23:47: | x_3 | 0.1 | 0.156624909640078 | 1 | float |
INFO - 16:23:47: +------+-------------+-------------------+-------------+-------+
INFO - 16:23:47: *** End PropulsionScenario execution (time: 0:00:00.010999) ***
INFO - 16:23:47: *** Start AerodynamicsScenario execution ***
INFO - 16:23:47: AerodynamicsScenario
INFO - 16:23:47: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:47: MDO formulation: MDF
INFO - 16:23:47: Optimization problem:
INFO - 16:23:47: minimize 0.001*-y_4(x_2)
INFO - 16:23:47: with respect to x_2
INFO - 16:23:47: under the inequality constraints
INFO - 16:23:47: g_2(x_2) <= 0
INFO - 16:23:47: over the design space:
INFO - 16:23:47: +------+-------------+-------+-------------+-------+
INFO - 16:23:47: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:47: +------+-------------+-------+-------------+-------+
INFO - 16:23:47: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:47: +------+-------------+-------+-------------+-------+
INFO - 16:23:47: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:47: 2%|▏ | 1/50 [00:00<00:00, 109.93 it/sec, feas=False, obj=-2.27]
INFO - 16:23:47: 4%|▍ | 2/50 [00:00<00:00, 173.96 it/sec, feas=False, obj=-2.27]
INFO - 16:23:47: 6%|▌ | 3/50 [00:00<00:00, 214.73 it/sec, feas=False, obj=-2.27]
INFO - 16:23:47: 8%|▊ | 4/50 [00:00<00:00, 241.51 it/sec, feas=False, obj=-2.27]
INFO - 16:23:47: 10%|█ | 5/50 [00:00<00:00, 261.96 it/sec, feas=False, obj=-2.27]
INFO - 16:23:47: 12%|█▏ | 6/50 [00:00<00:00, 278.91 it/sec, feas=False, obj=-2.27]
INFO - 16:23:47: 14%|█▍ | 7/50 [00:00<00:00, 294.19 it/sec, feas=False, obj=-2.27]
WARNING - 16:23:47: Optimization found no feasible point; the least infeasible point is selected.
INFO - 16:23:47: 16%|█▌ | 8/50 [00:00<00:00, 239.88 it/sec, feas=False, obj=-2.27]
INFO - 16:23:47: Optimization result:
INFO - 16:23:47: Optimizer info:
INFO - 16:23:47: Status: 8
INFO - 16:23:47: Message: Positive directional derivative for linesearch
INFO - 16:23:47: Solution:
WARNING - 16:23:47: The solution is not feasible.
INFO - 16:23:47: Objective: -2.2684989665435027
INFO - 16:23:47: Standardized constraints:
INFO - 16:23:47: g_2 = 0.0027615609342461767
INFO - 16:23:47: Design space:
INFO - 16:23:47: +------+-------------+-------+-------------+-------+
INFO - 16:23:47: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:47: +------+-------------+-------+-------------+-------+
INFO - 16:23:47: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:47: +------+-------------+-------+-------------+-------+
INFO - 16:23:47: *** End AerodynamicsScenario execution (time: 0:00:00.034907) ***
INFO - 16:23:47: 44%|████▍ | 44/100 [00:30<00:38, 1.45 it/sec, feas=False, obj=-2.27]
INFO - 16:23:47: *** Start PropulsionScenario execution ***
INFO - 16:23:47: PropulsionScenario
INFO - 16:23:47: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:47: MDO formulation: MDF
INFO - 16:23:47: Optimization problem:
INFO - 16:23:47: minimize 0.001*-y_4(x_3)
INFO - 16:23:47: with respect to x_3
INFO - 16:23:47: under the inequality constraints
INFO - 16:23:47: g_3(x_3) <= 0
INFO - 16:23:47: over the design space:
INFO - 16:23:47: +------+-------------+-------------------+-------------+-------+
INFO - 16:23:47: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:47: +------+-------------+-------------------+-------------+-------+
INFO - 16:23:47: | x_3 | 0.1 | 0.156624909640078 | 1 | float |
INFO - 16:23:47: +------+-------------+-------------------+-------------+-------+
INFO - 16:23:47: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:47: 2%|▏ | 1/50 [00:00<00:01, 36.74 it/sec, feas=True, obj=-2.27]
INFO - 16:23:47: 4%|▍ | 2/50 [00:00<00:01, 28.17 it/sec, feas=True, obj=-2.28]
INFO - 16:23:47: Optimization result:
INFO - 16:23:47: Optimizer info:
INFO - 16:23:47: Status: 8
INFO - 16:23:47: Message: Positive directional derivative for linesearch
INFO - 16:23:47: Solution:
INFO - 16:23:47: The solution is feasible.
INFO - 16:23:47: Objective: -2.275157793684183
INFO - 16:23:47: Standardized constraints:
INFO - 16:23:47: g_3 = [-8.05308988e-01 -1.94691012e-01 3.77475828e-15 -1.82294914e-01]
INFO - 16:23:47: Design space:
INFO - 16:23:47: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:47: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:47: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:47: | x_3 | 0.1 | 0.1572648677482919 | 1 | float |
INFO - 16:23:47: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:47: *** End PropulsionScenario execution (time: 0:00:00.073305) ***
INFO - 16:23:47: *** Start AerodynamicsScenario execution ***
INFO - 16:23:47: AerodynamicsScenario
INFO - 16:23:47: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:47: MDO formulation: MDF
INFO - 16:23:47: Optimization problem:
INFO - 16:23:47: minimize 0.001*-y_4(x_2)
INFO - 16:23:47: with respect to x_2
INFO - 16:23:47: under the inequality constraints
INFO - 16:23:47: g_2(x_2) <= 0
INFO - 16:23:47: over the design space:
INFO - 16:23:47: +------+-------------+-------+-------------+-------+
INFO - 16:23:47: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:47: +------+-------------+-------+-------------+-------+
INFO - 16:23:47: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:47: +------+-------------+-------+-------------+-------+
INFO - 16:23:47: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:47: 2%|▏ | 1/50 [00:00<00:00, 102.24 it/sec, feas=True, obj=-2.28]
INFO - 16:23:47: Optimization result:
INFO - 16:23:47: Optimizer info:
INFO - 16:23:47: Status: 8
INFO - 16:23:47: Message: Positive directional derivative for linesearch
INFO - 16:23:47: Solution:
INFO - 16:23:47: The solution is feasible.
INFO - 16:23:47: Objective: -2.275157793684183
INFO - 16:23:47: Standardized constraints:
INFO - 16:23:47: g_2 = 0.0
INFO - 16:23:47: Design space:
INFO - 16:23:47: +------+-------------+-------+-------------+-------+
INFO - 16:23:47: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:47: +------+-------------+-------+-------------+-------+
INFO - 16:23:47: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:47: +------+-------------+-------+-------------+-------+
INFO - 16:23:47: *** End AerodynamicsScenario execution (time: 0:00:00.011564) ***
INFO - 16:23:47: *** Start StructureScenario execution ***
INFO - 16:23:47: StructureScenario
INFO - 16:23:47: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:47: MDO formulation: MDF
INFO - 16:23:47: Optimization problem:
INFO - 16:23:47: minimize 0.001*-y_4(x_1)
INFO - 16:23:47: with respect to x_1
INFO - 16:23:47: under the inequality constraints
INFO - 16:23:47: g_1(x_1) <= 0
INFO - 16:23:47: over the design space:
INFO - 16:23:47: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:47: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:47: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:47: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:47: | x_1[1] | 0.75 | 0.7806436836756807 | 1.25 | float |
INFO - 16:23:47: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:47: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:47: 2%|▏ | 1/50 [00:00<00:00, 96.11 it/sec, feas=True, obj=-2.28]
INFO - 16:23:47: 4%|▍ | 2/50 [00:00<00:00, 97.89 it/sec, feas=True, obj=-2.28]
INFO - 16:23:47: 6%|▌ | 3/50 [00:00<00:00, 103.86 it/sec, feas=True, obj=-2.28]
INFO - 16:23:47: Optimization result:
INFO - 16:23:47: Optimizer info:
INFO - 16:23:47: Status: None
INFO - 16:23:47: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:47: Solution:
INFO - 16:23:47: The solution is feasible.
INFO - 16:23:47: Objective: -2.275157793684183
INFO - 16:23:47: Standardized constraints:
INFO - 16:23:47: g_1 = [-1.59589593e-03 -2.02868890e-03 -1.31333010e-02 -2.32802973e-02
INFO - 16:23:47: -3.14967236e-02 -2.40000000e-01 2.65898414e-13]
INFO - 16:23:47: Design space:
INFO - 16:23:47: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:47: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:47: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:47: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:47: | x_1[1] | 0.75 | 0.7806436836756807 | 1.25 | float |
INFO - 16:23:47: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:47: *** End StructureScenario execution (time: 0:00:00.031562) ***
INFO - 16:23:47: *** Start PropulsionScenario execution ***
INFO - 16:23:47: PropulsionScenario
INFO - 16:23:47: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:47: MDO formulation: MDF
INFO - 16:23:47: Optimization problem:
INFO - 16:23:47: minimize 0.001*-y_4(x_3)
INFO - 16:23:47: with respect to x_3
INFO - 16:23:47: under the inequality constraints
INFO - 16:23:47: g_3(x_3) <= 0
INFO - 16:23:47: over the design space:
INFO - 16:23:47: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:47: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:47: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:47: | x_3 | 0.1 | 0.1572648677482919 | 1 | float |
INFO - 16:23:47: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:47: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:47: 2%|▏ | 1/50 [00:00<00:00, 91.39 it/sec, feas=True, obj=-2.28]
INFO - 16:23:47: Optimization result:
INFO - 16:23:47: Optimizer info:
INFO - 16:23:47: Status: 8
INFO - 16:23:47: Message: Positive directional derivative for linesearch
INFO - 16:23:47: Solution:
INFO - 16:23:47: The solution is feasible.
INFO - 16:23:47: Objective: -2.275157793684183
INFO - 16:23:47: Standardized constraints:
INFO - 16:23:47: g_3 = [-8.05308988e-01 -1.94691012e-01 3.77475828e-15 -1.82294914e-01]
INFO - 16:23:47: Design space:
INFO - 16:23:47: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:47: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:47: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:47: | x_3 | 0.1 | 0.1572648677482919 | 1 | float |
INFO - 16:23:47: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:47: *** End PropulsionScenario execution (time: 0:00:00.012898) ***
INFO - 16:23:47: 45%|████▌ | 45/100 [00:30<00:37, 1.48 it/sec, feas=True, obj=-2.28]
INFO - 16:23:47: *** Start PropulsionScenario execution ***
INFO - 16:23:47: PropulsionScenario
INFO - 16:23:47: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:47: MDO formulation: MDF
INFO - 16:23:47: Optimization problem:
INFO - 16:23:47: minimize 0.001*-y_4(x_3)
INFO - 16:23:47: with respect to x_3
INFO - 16:23:47: under the inequality constraints
INFO - 16:23:47: g_3(x_3) <= 0
INFO - 16:23:47: over the design space:
INFO - 16:23:47: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:47: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:47: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:47: | x_3 | 0.1 | 0.1572648677482919 | 1 | float |
INFO - 16:23:47: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:47: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:47: 2%|▏ | 1/50 [00:00<00:01, 37.11 it/sec, feas=True, obj=-2.24]
INFO - 16:23:47: 4%|▍ | 2/50 [00:00<00:01, 28.42 it/sec, feas=True, obj=-2.24]
INFO - 16:23:47: 6%|▌ | 3/50 [00:00<00:01, 26.74 it/sec, feas=True, obj=-2.24]
INFO - 16:23:47: 8%|▊ | 4/50 [00:00<00:01, 28.81 it/sec, feas=True, obj=-2.24]
INFO - 16:23:47: Optimization result:
INFO - 16:23:47: Optimizer info:
INFO - 16:23:47: Status: None
INFO - 16:23:47: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:47: Solution:
INFO - 16:23:47: The solution is feasible.
INFO - 16:23:47: Objective: -2.237717395994335
INFO - 16:23:47: Standardized constraints:
INFO - 16:23:47: g_3 = [-0.82126703 -0.17873297 0. -0.18094131]
INFO - 16:23:47: Design space:
INFO - 16:23:47: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:47: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:47: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:47: | x_3 | 0.1 | 0.1587238442156903 | 1 | float |
INFO - 16:23:47: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:47: *** End PropulsionScenario execution (time: 0:00:00.141130) ***
INFO - 16:23:47: *** Start AerodynamicsScenario execution ***
INFO - 16:23:47: AerodynamicsScenario
INFO - 16:23:47: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:47: MDO formulation: MDF
INFO - 16:23:47: Optimization problem:
INFO - 16:23:47: minimize 0.001*-y_4(x_2)
INFO - 16:23:47: with respect to x_2
INFO - 16:23:47: under the inequality constraints
INFO - 16:23:47: g_2(x_2) <= 0
INFO - 16:23:47: over the design space:
INFO - 16:23:47: +------+-------------+-------+-------------+-------+
INFO - 16:23:47: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:47: +------+-------------+-------+-------------+-------+
INFO - 16:23:47: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:47: +------+-------------+-------+-------------+-------+
INFO - 16:23:47: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:47: 2%|▏ | 1/50 [00:00<00:00, 77.69 it/sec, feas=True, obj=-2.24]
INFO - 16:23:47: Optimization result:
INFO - 16:23:47: Optimizer info:
INFO - 16:23:47: Status: 8
INFO - 16:23:47: Message: Positive directional derivative for linesearch
INFO - 16:23:47: Solution:
INFO - 16:23:47: The solution is feasible.
INFO - 16:23:47: Objective: -2.237717395994335
INFO - 16:23:47: Standardized constraints:
INFO - 16:23:47: g_2 = 0.0
INFO - 16:23:47: Design space:
INFO - 16:23:47: +------+-------------+-------+-------------+-------+
INFO - 16:23:47: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:47: +------+-------------+-------+-------------+-------+
INFO - 16:23:47: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:47: +------+-------------+-------+-------------+-------+
INFO - 16:23:47: *** End AerodynamicsScenario execution (time: 0:00:00.014656) ***
INFO - 16:23:47: *** Start StructureScenario execution ***
INFO - 16:23:47: StructureScenario
INFO - 16:23:47: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:47: MDO formulation: MDF
INFO - 16:23:47: Optimization problem:
INFO - 16:23:47: minimize 0.001*-y_4(x_1)
INFO - 16:23:47: with respect to x_1
INFO - 16:23:47: under the inequality constraints
INFO - 16:23:47: g_1(x_1) <= 0
INFO - 16:23:47: over the design space:
INFO - 16:23:47: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:47: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:47: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:47: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:47: | x_1[1] | 0.75 | 0.7806436836756807 | 1.25 | float |
INFO - 16:23:47: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:47: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:47: 2%|▏ | 1/50 [00:00<00:00, 97.49 it/sec, feas=True, obj=-2.24]
INFO - 16:23:47: Optimization result:
INFO - 16:23:47: Optimizer info:
INFO - 16:23:47: Status: 8
INFO - 16:23:47: Message: Positive directional derivative for linesearch
INFO - 16:23:47: Solution:
INFO - 16:23:47: The solution is feasible.
INFO - 16:23:47: Objective: -2.237717395994335
INFO - 16:23:47: Standardized constraints:
INFO - 16:23:47: g_1 = [-1.59589593e-03 -2.02868890e-03 -1.31333010e-02 -2.32802973e-02
INFO - 16:23:47: -3.14967236e-02 -2.40000000e-01 2.65898414e-13]
INFO - 16:23:47: Design space:
INFO - 16:23:47: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:47: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:47: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:47: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:47: | x_1[1] | 0.75 | 0.7806436836756807 | 1.25 | float |
INFO - 16:23:47: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:47: *** End StructureScenario execution (time: 0:00:00.012178) ***
INFO - 16:23:47: *** Start PropulsionScenario execution ***
INFO - 16:23:47: PropulsionScenario
INFO - 16:23:47: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:47: MDO formulation: MDF
INFO - 16:23:47: Optimization problem:
INFO - 16:23:47: minimize 0.001*-y_4(x_3)
INFO - 16:23:47: with respect to x_3
INFO - 16:23:47: under the inequality constraints
INFO - 16:23:47: g_3(x_3) <= 0
INFO - 16:23:47: over the design space:
INFO - 16:23:47: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:47: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:47: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:47: | x_3 | 0.1 | 0.1587238442156903 | 1 | float |
INFO - 16:23:47: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:47: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:47: 2%|▏ | 1/50 [00:00<00:00, 108.30 it/sec, feas=True, obj=-2.24]
INFO - 16:23:47: 4%|▍ | 2/50 [00:00<00:00, 142.02 it/sec, feas=True, obj=-2.24]
INFO - 16:23:47: 6%|▌ | 3/50 [00:00<00:00, 155.84 it/sec, feas=True, obj=-2.24]
INFO - 16:23:47: Optimization result:
INFO - 16:23:47: Optimizer info:
INFO - 16:23:47: Status: None
INFO - 16:23:47: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:47: Solution:
INFO - 16:23:47: The solution is feasible.
INFO - 16:23:47: Objective: -2.2377173959943373
INFO - 16:23:47: Standardized constraints:
INFO - 16:23:47: g_3 = [-8.21267030e-01 -1.78732970e-01 7.54951657e-15 -1.80941307e-01]
INFO - 16:23:47: Design space:
INFO - 16:23:47: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:47: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:47: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:47: | x_3 | 0.1 | 0.1587238442156915 | 1 | float |
INFO - 16:23:47: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:47: *** End PropulsionScenario execution (time: 0:00:00.021424) ***
INFO - 16:23:47: *** Start AerodynamicsScenario execution ***
INFO - 16:23:47: AerodynamicsScenario
INFO - 16:23:47: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:47: MDO formulation: MDF
INFO - 16:23:47: Optimization problem:
INFO - 16:23:47: minimize 0.001*-y_4(x_2)
INFO - 16:23:47: with respect to x_2
INFO - 16:23:47: under the inequality constraints
INFO - 16:23:47: g_2(x_2) <= 0
INFO - 16:23:47: over the design space:
INFO - 16:23:47: +------+-------------+-------+-------------+-------+
INFO - 16:23:47: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:47: +------+-------------+-------+-------------+-------+
INFO - 16:23:47: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:47: +------+-------------+-------+-------------+-------+
INFO - 16:23:47: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:47: 2%|▏ | 1/50 [00:00<00:00, 75.91 it/sec, feas=True, obj=-2.24]
INFO - 16:23:47: Optimization result:
INFO - 16:23:47: Optimizer info:
INFO - 16:23:47: Status: 8
INFO - 16:23:47: Message: Positive directional derivative for linesearch
INFO - 16:23:47: Solution:
INFO - 16:23:47: The solution is feasible.
INFO - 16:23:47: Objective: -2.2377173959943377
INFO - 16:23:47: Standardized constraints:
INFO - 16:23:47: g_2 = 0.0
INFO - 16:23:47: Design space:
INFO - 16:23:47: +------+-------------+-------+-------------+-------+
INFO - 16:23:47: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:47: +------+-------------+-------+-------------+-------+
INFO - 16:23:47: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:47: +------+-------------+-------+-------------+-------+
INFO - 16:23:47: *** End AerodynamicsScenario execution (time: 0:00:00.014912) ***
INFO - 16:23:47: *** Start StructureScenario execution ***
INFO - 16:23:47: StructureScenario
INFO - 16:23:47: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:47: MDO formulation: MDF
INFO - 16:23:47: Optimization problem:
INFO - 16:23:47: minimize 0.001*-y_4(x_1)
INFO - 16:23:47: with respect to x_1
INFO - 16:23:47: under the inequality constraints
INFO - 16:23:47: g_1(x_1) <= 0
INFO - 16:23:47: over the design space:
INFO - 16:23:47: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:47: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:47: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:47: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:47: | x_1[1] | 0.75 | 0.7806436836756807 | 1.25 | float |
INFO - 16:23:47: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:47: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:47: 2%|▏ | 1/50 [00:00<00:00, 80.40 it/sec, feas=True, obj=-2.24]
INFO - 16:23:47: Optimization result:
INFO - 16:23:47: Optimizer info:
INFO - 16:23:47: Status: 8
INFO - 16:23:47: Message: Positive directional derivative for linesearch
INFO - 16:23:47: Solution:
INFO - 16:23:47: The solution is feasible.
INFO - 16:23:47: Objective: -2.2377173959943373
INFO - 16:23:47: Standardized constraints:
INFO - 16:23:47: g_1 = [-1.59589593e-03 -2.02868890e-03 -1.31333010e-02 -2.32802973e-02
INFO - 16:23:47: -3.14967236e-02 -2.40000000e-01 2.65898414e-13]
INFO - 16:23:47: Design space:
INFO - 16:23:47: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:47: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:47: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:47: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:47: | x_1[1] | 0.75 | 0.7806436836756807 | 1.25 | float |
INFO - 16:23:47: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:47: *** End StructureScenario execution (time: 0:00:00.014536) ***
INFO - 16:23:47: 46%|████▌ | 46/100 [00:30<00:36, 1.50 it/sec, feas=True, obj=-2.24]
INFO - 16:23:47: *** Start PropulsionScenario execution ***
INFO - 16:23:47: PropulsionScenario
INFO - 16:23:47: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:47: MDO formulation: MDF
INFO - 16:23:47: Optimization problem:
INFO - 16:23:47: minimize 0.001*-y_4(x_3)
INFO - 16:23:47: with respect to x_3
INFO - 16:23:47: under the inequality constraints
INFO - 16:23:47: g_3(x_3) <= 0
INFO - 16:23:47: over the design space:
INFO - 16:23:47: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:47: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:47: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:47: | x_3 | 0.1 | 0.1587238442156915 | 1 | float |
INFO - 16:23:47: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:47: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:47: 2%|▏ | 1/50 [00:00<00:01, 38.77 it/sec, feas=True, obj=-2.19]
INFO - 16:23:47: 4%|▍ | 2/50 [00:00<00:01, 28.09 it/sec, feas=True, obj=-2.19]
INFO - 16:23:47: 6%|▌ | 3/50 [00:00<00:01, 26.57 it/sec, feas=True, obj=-2.19]
INFO - 16:23:47: 8%|▊ | 4/50 [00:00<00:01, 25.73 it/sec, feas=True, obj=-2.19]
INFO - 16:23:47: Optimization result:
INFO - 16:23:47: Optimizer info:
INFO - 16:23:47: Status: None
INFO - 16:23:47: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:47: Solution:
INFO - 16:23:47: The solution is feasible.
INFO - 16:23:47: Objective: -2.1901342716878958
INFO - 16:23:47: Standardized constraints:
INFO - 16:23:47: g_3 = [-8.23924007e-01 -1.76075993e-01 6.88338275e-15 -1.79803384e-01]
INFO - 16:23:47: Design space:
INFO - 16:23:47: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:47: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:47: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:47: | x_3 | 0.1 | 0.1601786529209688 | 1 | float |
INFO - 16:23:47: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:47: *** End PropulsionScenario execution (time: 0:00:00.158187) ***
INFO - 16:23:47: *** Start AerodynamicsScenario execution ***
INFO - 16:23:47: AerodynamicsScenario
INFO - 16:23:47: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:47: MDO formulation: MDF
INFO - 16:23:47: Optimization problem:
INFO - 16:23:47: minimize 0.001*-y_4(x_2)
INFO - 16:23:47: with respect to x_2
INFO - 16:23:47: under the inequality constraints
INFO - 16:23:47: g_2(x_2) <= 0
INFO - 16:23:47: over the design space:
INFO - 16:23:47: +------+-------------+-------+-------------+-------+
INFO - 16:23:47: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:47: +------+-------------+-------+-------------+-------+
INFO - 16:23:47: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:47: +------+-------------+-------+-------------+-------+
INFO - 16:23:47: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:47: 2%|▏ | 1/50 [00:00<00:00, 77.18 it/sec, feas=True, obj=-2.19]
INFO - 16:23:47: Optimization result:
INFO - 16:23:47: Optimizer info:
INFO - 16:23:47: Status: 8
INFO - 16:23:47: Message: Positive directional derivative for linesearch
INFO - 16:23:47: Solution:
INFO - 16:23:47: The solution is feasible.
INFO - 16:23:47: Objective: -2.190134271687896
INFO - 16:23:47: Standardized constraints:
INFO - 16:23:47: g_2 = -0.0002651658798968892
INFO - 16:23:47: Design space:
INFO - 16:23:47: +------+-------------+-------+-------------+-------+
INFO - 16:23:47: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:47: +------+-------------+-------+-------------+-------+
INFO - 16:23:47: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:47: +------+-------------+-------+-------------+-------+
INFO - 16:23:47: *** End AerodynamicsScenario execution (time: 0:00:00.014702) ***
INFO - 16:23:47: *** Start StructureScenario execution ***
INFO - 16:23:47: StructureScenario
INFO - 16:23:47: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:47: MDO formulation: MDF
INFO - 16:23:47: Optimization problem:
INFO - 16:23:47: minimize 0.001*-y_4(x_1)
INFO - 16:23:47: with respect to x_1
INFO - 16:23:47: under the inequality constraints
INFO - 16:23:47: g_1(x_1) <= 0
INFO - 16:23:47: over the design space:
INFO - 16:23:47: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:47: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:47: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:47: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:47: | x_1[1] | 0.75 | 0.7806436836756807 | 1.25 | float |
INFO - 16:23:47: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:47: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:47: 2%|▏ | 1/50 [00:00<00:00, 82.87 it/sec, feas=False, obj=-2.19]
INFO - 16:23:47: 4%|▍ | 2/50 [00:00<00:01, 36.22 it/sec, feas=True, obj=-2.19]
INFO - 16:23:47: 6%|▌ | 3/50 [00:00<00:01, 31.45 it/sec, feas=True, obj=-2.19]
INFO - 16:23:47: 8%|▊ | 4/50 [00:00<00:01, 29.52 it/sec, feas=True, obj=-2.19]
WARNING - 16:23:47: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 0.0009157477359807847 is still above the tolerance 1e-06.
INFO - 16:23:47: 10%|█ | 5/50 [00:00<00:01, 30.21 it/sec, feas=True, obj=-2.19]
INFO - 16:23:47: Optimization result:
INFO - 16:23:47: Optimizer info:
INFO - 16:23:47: Status: None
INFO - 16:23:47: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:47: Solution:
INFO - 16:23:47: The solution is feasible.
INFO - 16:23:47: Objective: -2.1892329111583266
INFO - 16:23:47: Standardized constraints:
INFO - 16:23:47: g_1 = [ 9.74331726e-13 -1.20354754e-03 -1.26039910e-02 -2.28998313e-02
INFO - 16:23:47: -3.12035475e-02 -2.39801492e-01 -1.98507660e-04]
INFO - 16:23:47: Design space:
INFO - 16:23:47: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:47: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:47: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:47: | x_1[0] | 0.1 | 0.1000000000000056 | 0.4 | float |
INFO - 16:23:47: | x_1[1] | 0.75 | 0.7812743873488447 | 1.25 | float |
INFO - 16:23:47: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:47: *** End StructureScenario execution (time: 0:00:00.168207) ***
INFO - 16:23:47: *** Start PropulsionScenario execution ***
INFO - 16:23:47: PropulsionScenario
INFO - 16:23:47: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:47: MDO formulation: MDF
INFO - 16:23:47: Optimization problem:
INFO - 16:23:47: minimize 0.001*-y_4(x_3)
INFO - 16:23:47: with respect to x_3
INFO - 16:23:47: under the inequality constraints
INFO - 16:23:47: g_3(x_3) <= 0
INFO - 16:23:47: over the design space:
INFO - 16:23:47: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:47: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:47: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:47: | x_3 | 0.1 | 0.1601786529209688 | 1 | float |
INFO - 16:23:47: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:47: Solving optimization problem with algorithm SLSQP:
WARNING - 16:23:47: MDAGaussSeidel has reached its maximum number of unsuccessful iterations, but the normalized residual norm 6.724932466608626e-05 is still above the tolerance 1e-06.
INFO - 16:23:47: 2%|▏ | 1/50 [00:00<00:00, 51.49 it/sec, feas=True, obj=-2.19]
INFO - 16:23:47: Optimization result:
INFO - 16:23:47: Optimizer info:
INFO - 16:23:47: Status: 8
INFO - 16:23:47: Message: Positive directional derivative for linesearch
INFO - 16:23:47: Solution:
INFO - 16:23:47: The solution is feasible.
INFO - 16:23:47: Objective: -2.1892329111583266
INFO - 16:23:47: Standardized constraints:
INFO - 16:23:47: g_3 = [-8.23921916e-01 -1.76078084e-01 6.88338275e-15 -1.79803384e-01]
INFO - 16:23:47: Design space:
INFO - 16:23:47: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:47: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:47: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:47: | x_3 | 0.1 | 0.1601786529209688 | 1 | float |
INFO - 16:23:47: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:47: *** End PropulsionScenario execution (time: 0:00:00.021254) ***
INFO - 16:23:47: *** Start AerodynamicsScenario execution ***
INFO - 16:23:47: AerodynamicsScenario
INFO - 16:23:47: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:47: MDO formulation: MDF
INFO - 16:23:47: Optimization problem:
INFO - 16:23:47: minimize 0.001*-y_4(x_2)
INFO - 16:23:47: with respect to x_2
INFO - 16:23:47: under the inequality constraints
INFO - 16:23:47: g_2(x_2) <= 0
INFO - 16:23:47: over the design space:
INFO - 16:23:47: +------+-------------+-------+-------------+-------+
INFO - 16:23:47: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:47: +------+-------------+-------+-------------+-------+
INFO - 16:23:47: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:47: +------+-------------+-------+-------------+-------+
INFO - 16:23:47: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:47: 2%|▏ | 1/50 [00:00<00:00, 81.97 it/sec, feas=True, obj=-2.19]
INFO - 16:23:47: Optimization result:
INFO - 16:23:47: Optimizer info:
INFO - 16:23:47: Status: 8
INFO - 16:23:47: Message: Positive directional derivative for linesearch
INFO - 16:23:47: Solution:
INFO - 16:23:47: The solution is feasible.
INFO - 16:23:47: Objective: -2.1892329111583266
INFO - 16:23:47: Standardized constraints:
INFO - 16:23:47: g_2 = -0.0002651658798968892
INFO - 16:23:47: Design space:
INFO - 16:23:47: +------+-------------+-------+-------------+-------+
INFO - 16:23:47: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:47: +------+-------------+-------+-------------+-------+
INFO - 16:23:47: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:47: +------+-------------+-------+-------------+-------+
INFO - 16:23:47: *** End AerodynamicsScenario execution (time: 0:00:00.013895) ***
INFO - 16:23:47: *** Start StructureScenario execution ***
INFO - 16:23:47: StructureScenario
INFO - 16:23:47: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:47: MDO formulation: MDF
INFO - 16:23:47: Optimization problem:
INFO - 16:23:47: minimize 0.001*-y_4(x_1)
INFO - 16:23:47: with respect to x_1
INFO - 16:23:47: under the inequality constraints
INFO - 16:23:47: g_1(x_1) <= 0
INFO - 16:23:47: over the design space:
INFO - 16:23:47: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:47: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:47: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:47: | x_1[0] | 0.1 | 0.1000000000000056 | 0.4 | float |
INFO - 16:23:47: | x_1[1] | 0.75 | 0.7812743873488447 | 1.25 | float |
INFO - 16:23:47: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:47: Solving optimization problem with algorithm SLSQP:
WARNING - 16:23:47: MDAGaussSeidel has reached its maximum number of unsuccessful iterations, but the normalized residual norm 0.0009157477359807847 is still above the tolerance 1e-06.
INFO - 16:23:47: 2%|▏ | 1/50 [00:00<00:00, 52.08 it/sec, feas=True, obj=-2.19]
INFO - 16:23:48: 4%|▍ | 2/50 [00:00<00:01, 45.89 it/sec, feas=True, obj=-2.19]
INFO - 16:23:48: 6%|▌ | 3/50 [00:00<00:01, 43.27 it/sec, feas=True, obj=-2.19]
INFO - 16:23:48: Optimization result:
INFO - 16:23:48: Optimizer info:
INFO - 16:23:48: Status: None
INFO - 16:23:48: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:48: Solution:
INFO - 16:23:48: The solution is feasible.
INFO - 16:23:48: Objective: -2.1892329111583266
INFO - 16:23:48: Standardized constraints:
INFO - 16:23:48: g_1 = [ 9.74331726e-13 -1.20354754e-03 -1.26039910e-02 -2.28998313e-02
INFO - 16:23:48: -3.12035475e-02 -2.39801492e-01 -1.98507660e-04]
INFO - 16:23:48: Design space:
INFO - 16:23:48: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:48: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:48: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:48: | x_1[0] | 0.1 | 0.1000000000000056 | 0.4 | float |
INFO - 16:23:48: | x_1[1] | 0.75 | 0.7812743873488447 | 1.25 | float |
INFO - 16:23:48: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:48: *** End StructureScenario execution (time: 0:00:00.072012) ***
WARNING - 16:23:48: MDAGaussSeidel has reached its maximum number of unsuccessful iterations, but the normalized residual norm 0.0009157477359807847 is still above the tolerance 1e-06.
INFO - 16:23:48: 47%|████▋ | 47/100 [00:31<00:35, 1.51 it/sec, feas=True, obj=-2.19]
INFO - 16:23:48: *** Start PropulsionScenario execution ***
INFO - 16:23:48: PropulsionScenario
INFO - 16:23:48: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:48: MDO formulation: MDF
INFO - 16:23:48: Optimization problem:
INFO - 16:23:48: minimize 0.001*-y_4(x_3)
INFO - 16:23:48: with respect to x_3
INFO - 16:23:48: under the inequality constraints
INFO - 16:23:48: g_3(x_3) <= 0
INFO - 16:23:48: over the design space:
INFO - 16:23:48: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:48: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:48: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:48: | x_3 | 0.1 | 0.1601786529209688 | 1 | float |
INFO - 16:23:48: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:48: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:48: 2%|▏ | 1/50 [00:00<00:01, 37.76 it/sec, feas=False, obj=-2.26]
INFO - 16:23:48: 4%|▍ | 2/50 [00:00<00:01, 36.98 it/sec, feas=True, obj=-2.25]
INFO - 16:23:48: 6%|▌ | 3/50 [00:00<00:01, 30.73 it/sec, feas=False, obj=-2.26]
INFO - 16:23:48: 8%|▊ | 4/50 [00:00<00:01, 28.33 it/sec, feas=True, obj=-2.25]
INFO - 16:23:48: 10%|█ | 5/50 [00:00<00:01, 27.31 it/sec, feas=True, obj=-2.25]
INFO - 16:23:48: 12%|█▏ | 6/50 [00:00<00:01, 28.69 it/sec, feas=True, obj=-2.25]
INFO - 16:23:48: Optimization result:
INFO - 16:23:48: Optimizer info:
INFO - 16:23:48: Status: None
INFO - 16:23:48: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:48: Solution:
INFO - 16:23:48: The solution is feasible.
INFO - 16:23:48: Objective: -2.25359412557233
INFO - 16:23:48: Standardized constraints:
INFO - 16:23:48: g_3 = [-8.33328149e-01 -1.66671851e-01 4.88498131e-15 -1.81438268e-01]
INFO - 16:23:48: Design space:
INFO - 16:23:48: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:48: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:48: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:48: | x_3 | 0.1 | 0.1581854271808724 | 1 | float |
INFO - 16:23:48: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:48: *** End PropulsionScenario execution (time: 0:00:00.211582) ***
INFO - 16:23:48: *** Start AerodynamicsScenario execution ***
INFO - 16:23:48: AerodynamicsScenario
INFO - 16:23:48: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:48: MDO formulation: MDF
INFO - 16:23:48: Optimization problem:
INFO - 16:23:48: minimize 0.001*-y_4(x_2)
INFO - 16:23:48: with respect to x_2
INFO - 16:23:48: under the inequality constraints
INFO - 16:23:48: g_2(x_2) <= 0
INFO - 16:23:48: over the design space:
INFO - 16:23:48: +------+-------------+-------+-------------+-------+
INFO - 16:23:48: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:48: +------+-------------+-------+-------------+-------+
INFO - 16:23:48: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:48: +------+-------------+-------+-------------+-------+
INFO - 16:23:48: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:48: 2%|▏ | 1/50 [00:00<00:00, 77.50 it/sec, feas=True, obj=-2.25]
INFO - 16:23:48: Optimization result:
INFO - 16:23:48: Optimizer info:
INFO - 16:23:48: Status: 8
INFO - 16:23:48: Message: Positive directional derivative for linesearch
INFO - 16:23:48: Solution:
INFO - 16:23:48: The solution is feasible.
INFO - 16:23:48: Objective: -2.25359412557233
INFO - 16:23:48: Standardized constraints:
INFO - 16:23:48: g_2 = 0.0
INFO - 16:23:48: Design space:
INFO - 16:23:48: +------+-------------+-------+-------------+-------+
INFO - 16:23:48: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:48: +------+-------------+-------+-------------+-------+
INFO - 16:23:48: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:48: +------+-------------+-------+-------------+-------+
INFO - 16:23:48: *** End AerodynamicsScenario execution (time: 0:00:00.014572) ***
INFO - 16:23:48: *** Start StructureScenario execution ***
INFO - 16:23:48: StructureScenario
INFO - 16:23:48: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:48: MDO formulation: MDF
INFO - 16:23:48: Optimization problem:
INFO - 16:23:48: minimize 0.001*-y_4(x_1)
INFO - 16:23:48: with respect to x_1
INFO - 16:23:48: under the inequality constraints
INFO - 16:23:48: g_1(x_1) <= 0
INFO - 16:23:48: over the design space:
INFO - 16:23:48: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:48: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:48: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:48: | x_1[0] | 0.1 | 0.1000000000000056 | 0.4 | float |
INFO - 16:23:48: | x_1[1] | 0.75 | 0.7812743873488447 | 1.25 | float |
INFO - 16:23:48: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:48: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:48: 2%|▏ | 1/50 [00:00<00:00, 96.10 it/sec, feas=True, obj=-2.25]
INFO - 16:23:48: 4%|▍ | 2/50 [00:00<00:01, 38.40 it/sec, feas=True, obj=-2.25]
INFO - 16:23:48: 6%|▌ | 3/50 [00:00<00:01, 32.65 it/sec, feas=True, obj=-2.25]
WARNING - 16:23:48: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 0.0009157477359807847 is still above the tolerance 1e-06.
INFO - 16:23:48: 8%|▊ | 4/50 [00:00<00:01, 28.85 it/sec, feas=True, obj=-2.25]
INFO - 16:23:48: 10%|█ | 5/50 [00:00<00:01, 28.08 it/sec, feas=True, obj=-2.25]
INFO - 16:23:48: Optimization result:
INFO - 16:23:48: Optimizer info:
INFO - 16:23:48: Status: None
INFO - 16:23:48: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:48: Solution:
INFO - 16:23:48: The solution is feasible.
INFO - 16:23:48: Objective: -2.254531977218995
INFO - 16:23:48: Standardized constraints:
INFO - 16:23:48: g_1 = [-1.59589593e-03 -2.02868890e-03 -1.31333010e-02 -2.32802973e-02
INFO - 16:23:48: -3.14967236e-02 -2.40000000e-01 -2.22044605e-16]
INFO - 16:23:48: Design space:
INFO - 16:23:48: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:48: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:48: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:48: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:48: | x_1[1] | 0.75 | 0.7806436836765267 | 1.25 | float |
INFO - 16:23:48: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:48: *** End StructureScenario execution (time: 0:00:00.180882) ***
INFO - 16:23:48: *** Start PropulsionScenario execution ***
INFO - 16:23:48: PropulsionScenario
INFO - 16:23:48: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:48: MDO formulation: MDF
INFO - 16:23:48: Optimization problem:
INFO - 16:23:48: minimize 0.001*-y_4(x_3)
INFO - 16:23:48: with respect to x_3
INFO - 16:23:48: under the inequality constraints
INFO - 16:23:48: g_3(x_3) <= 0
INFO - 16:23:48: over the design space:
INFO - 16:23:48: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:48: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:48: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:48: | x_3 | 0.1 | 0.1581854271808724 | 1 | float |
INFO - 16:23:48: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:48: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:48: 2%|▏ | 1/50 [00:00<00:00, 109.37 it/sec, feas=True, obj=-2.25]
INFO - 16:23:48: Optimization result:
INFO - 16:23:48: Optimizer info:
INFO - 16:23:48: Status: 8
INFO - 16:23:48: Message: Positive directional derivative for linesearch
INFO - 16:23:48: Solution:
INFO - 16:23:48: The solution is feasible.
INFO - 16:23:48: Objective: -2.254531977218995
INFO - 16:23:48: Standardized constraints:
INFO - 16:23:48: g_3 = [-8.33330205e-01 -1.66669795e-01 4.88498131e-15 -1.81438268e-01]
INFO - 16:23:48: Design space:
INFO - 16:23:48: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:48: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:48: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:48: | x_3 | 0.1 | 0.1581854271808724 | 1 | float |
INFO - 16:23:48: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:48: *** End PropulsionScenario execution (time: 0:00:00.011150) ***
INFO - 16:23:48: *** Start AerodynamicsScenario execution ***
INFO - 16:23:48: AerodynamicsScenario
INFO - 16:23:48: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:48: MDO formulation: MDF
INFO - 16:23:48: Optimization problem:
INFO - 16:23:48: minimize 0.001*-y_4(x_2)
INFO - 16:23:48: with respect to x_2
INFO - 16:23:48: under the inequality constraints
INFO - 16:23:48: g_2(x_2) <= 0
INFO - 16:23:48: over the design space:
INFO - 16:23:48: +------+-------------+-------+-------------+-------+
INFO - 16:23:48: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:48: +------+-------------+-------+-------------+-------+
INFO - 16:23:48: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:48: +------+-------------+-------+-------------+-------+
INFO - 16:23:48: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:48: 2%|▏ | 1/50 [00:00<00:00, 109.01 it/sec, feas=True, obj=-2.25]
INFO - 16:23:48: Optimization result:
INFO - 16:23:48: Optimizer info:
INFO - 16:23:48: Status: 8
INFO - 16:23:48: Message: Positive directional derivative for linesearch
INFO - 16:23:48: Solution:
INFO - 16:23:48: The solution is feasible.
INFO - 16:23:48: Objective: -2.254531977218995
INFO - 16:23:48: Standardized constraints:
INFO - 16:23:48: g_2 = 0.0
INFO - 16:23:48: Design space:
INFO - 16:23:48: +------+-------------+-------+-------------+-------+
INFO - 16:23:48: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:48: +------+-------------+-------+-------------+-------+
INFO - 16:23:48: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:48: +------+-------------+-------+-------------+-------+
INFO - 16:23:48: *** End AerodynamicsScenario execution (time: 0:00:00.010793) ***
INFO - 16:23:48: *** Start StructureScenario execution ***
INFO - 16:23:48: StructureScenario
INFO - 16:23:48: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:48: MDO formulation: MDF
INFO - 16:23:48: Optimization problem:
INFO - 16:23:48: minimize 0.001*-y_4(x_1)
INFO - 16:23:48: with respect to x_1
INFO - 16:23:48: under the inequality constraints
INFO - 16:23:48: g_1(x_1) <= 0
INFO - 16:23:48: over the design space:
INFO - 16:23:48: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:48: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:48: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:48: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:48: | x_1[1] | 0.75 | 0.7806436836765267 | 1.25 | float |
INFO - 16:23:48: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:48: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:48: 2%|▏ | 1/50 [00:00<00:00, 103.27 it/sec, feas=True, obj=-2.25]
INFO - 16:23:48: 4%|▍ | 2/50 [00:00<00:00, 65.66 it/sec, feas=True, obj=-2.25]
INFO - 16:23:48: 6%|▌ | 3/50 [00:00<00:00, 87.52 it/sec, feas=True, obj=-2.25]
INFO - 16:23:48: Optimization result:
INFO - 16:23:48: Optimizer info:
INFO - 16:23:48: Status: None
INFO - 16:23:48: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:48: Solution:
INFO - 16:23:48: The solution is feasible.
INFO - 16:23:48: Objective: -2.254531977218996
INFO - 16:23:48: Standardized constraints:
INFO - 16:23:48: g_1 = [-0.0015959 -0.00202869 -0.0131333 -0.0232803 -0.03149672 -0.24
INFO - 16:23:48: 0. ]
INFO - 16:23:48: Design space:
INFO - 16:23:48: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:48: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:48: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:48: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:48: | x_1[1] | 0.75 | 0.7806436836765261 | 1.25 | float |
INFO - 16:23:48: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:48: *** End StructureScenario execution (time: 0:00:00.036655) ***
INFO - 16:23:48: 48%|████▊ | 48/100 [00:31<00:34, 1.52 it/sec, feas=True, obj=-2.25]
INFO - 16:23:48: *** Start PropulsionScenario execution ***
INFO - 16:23:48: PropulsionScenario
INFO - 16:23:48: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:48: MDO formulation: MDF
INFO - 16:23:48: Optimization problem:
INFO - 16:23:48: minimize 0.001*-y_4(x_3)
INFO - 16:23:48: with respect to x_3
INFO - 16:23:48: under the inequality constraints
INFO - 16:23:48: g_3(x_3) <= 0
INFO - 16:23:48: over the design space:
INFO - 16:23:48: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:48: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:48: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:48: | x_3 | 0.1 | 0.1581854271808724 | 1 | float |
INFO - 16:23:48: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:48: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:48: 2%|▏ | 1/50 [00:00<00:01, 37.48 it/sec, feas=True, obj=-2.17]
INFO - 16:23:48: 4%|▍ | 2/50 [00:00<00:01, 28.35 it/sec, feas=True, obj=-2.17]
INFO - 16:23:48: 6%|▌ | 3/50 [00:00<00:01, 26.38 it/sec, feas=True, obj=-2.17]
INFO - 16:23:48: 8%|▊ | 4/50 [00:00<00:01, 28.31 it/sec, feas=True, obj=-2.17]
INFO - 16:23:48: Optimization result:
INFO - 16:23:48: Optimizer info:
INFO - 16:23:48: Status: None
INFO - 16:23:48: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:48: Solution:
INFO - 16:23:48: The solution is feasible.
INFO - 16:23:48: Objective: -2.173398336780509
INFO - 16:23:48: Standardized constraints:
INFO - 16:23:48: g_3 = [-8.26694979e-01 -1.73305021e-01 1.77635684e-15 -1.79835333e-01]
INFO - 16:23:48: Design space:
INFO - 16:23:48: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:48: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:48: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:48: | x_3 | 0.1 | 0.1611879493003633 | 1 | float |
INFO - 16:23:48: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:48: *** End PropulsionScenario execution (time: 0:00:00.144064) ***
INFO - 16:23:48: *** Start AerodynamicsScenario execution ***
INFO - 16:23:48: AerodynamicsScenario
INFO - 16:23:48: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:48: MDO formulation: MDF
INFO - 16:23:48: Optimization problem:
INFO - 16:23:48: minimize 0.001*-y_4(x_2)
INFO - 16:23:48: with respect to x_2
INFO - 16:23:48: under the inequality constraints
INFO - 16:23:48: g_2(x_2) <= 0
INFO - 16:23:48: over the design space:
INFO - 16:23:48: +------+-------------+-------+-------------+-------+
INFO - 16:23:48: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:48: +------+-------------+-------+-------------+-------+
INFO - 16:23:48: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:48: +------+-------------+-------+-------------+-------+
INFO - 16:23:48: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:48: 2%|▏ | 1/50 [00:00<00:00, 89.14 it/sec, feas=True, obj=-2.17]
INFO - 16:23:48: Optimization result:
INFO - 16:23:48: Optimizer info:
INFO - 16:23:48: Status: 8
INFO - 16:23:48: Message: Positive directional derivative for linesearch
INFO - 16:23:48: Solution:
INFO - 16:23:48: The solution is feasible.
INFO - 16:23:48: Objective: -2.173398336780509
INFO - 16:23:48: Standardized constraints:
INFO - 16:23:48: g_2 = -4.346970141155815e-05
INFO - 16:23:48: Design space:
INFO - 16:23:48: +------+-------------+-------+-------------+-------+
INFO - 16:23:48: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:48: +------+-------------+-------+-------------+-------+
INFO - 16:23:48: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:48: +------+-------------+-------+-------------+-------+
INFO - 16:23:48: *** End AerodynamicsScenario execution (time: 0:00:00.013074) ***
INFO - 16:23:48: *** Start StructureScenario execution ***
INFO - 16:23:48: StructureScenario
INFO - 16:23:48: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:48: MDO formulation: MDF
INFO - 16:23:48: Optimization problem:
INFO - 16:23:48: minimize 0.001*-y_4(x_1)
INFO - 16:23:48: with respect to x_1
INFO - 16:23:48: under the inequality constraints
INFO - 16:23:48: g_1(x_1) <= 0
INFO - 16:23:48: over the design space:
INFO - 16:23:48: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:48: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:48: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:48: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:48: | x_1[1] | 0.75 | 0.7806436836765261 | 1.25 | float |
INFO - 16:23:48: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:48: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:48: 2%|▏ | 1/50 [00:00<00:00, 97.20 it/sec, feas=True, obj=-2.17]
INFO - 16:23:48: Optimization result:
INFO - 16:23:48: Optimizer info:
INFO - 16:23:48: Status: 8
INFO - 16:23:48: Message: Positive directional derivative for linesearch
INFO - 16:23:48: Solution:
INFO - 16:23:48: The solution is feasible.
INFO - 16:23:48: Objective: -2.173398336780509
INFO - 16:23:48: Standardized constraints:
INFO - 16:23:48: g_1 = [-0.0012476 -0.00183766 -0.01300547 -0.02318545 -0.0314218 -0.24
INFO - 16:23:48: 0. ]
INFO - 16:23:48: Design space:
INFO - 16:23:48: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:48: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:48: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:48: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:48: | x_1[1] | 0.75 | 0.7806436836765261 | 1.25 | float |
INFO - 16:23:48: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:48: *** End StructureScenario execution (time: 0:00:00.012357) ***
INFO - 16:23:48: *** Start PropulsionScenario execution ***
INFO - 16:23:48: PropulsionScenario
INFO - 16:23:48: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:48: MDO formulation: MDF
INFO - 16:23:48: Optimization problem:
INFO - 16:23:48: minimize 0.001*-y_4(x_3)
INFO - 16:23:48: with respect to x_3
INFO - 16:23:48: under the inequality constraints
INFO - 16:23:48: g_3(x_3) <= 0
INFO - 16:23:48: over the design space:
INFO - 16:23:48: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:48: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:48: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:48: | x_3 | 0.1 | 0.1611879493003633 | 1 | float |
INFO - 16:23:48: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:48: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:48: 2%|▏ | 1/50 [00:00<00:00, 109.16 it/sec, feas=True, obj=-2.17]
INFO - 16:23:48: 4%|▍ | 2/50 [00:00<00:00, 156.01 it/sec, feas=True, obj=-2.17]
INFO - 16:23:48: 6%|▌ | 3/50 [00:00<00:00, 173.62 it/sec, feas=True, obj=-2.17]
INFO - 16:23:48: Optimization result:
INFO - 16:23:48: Optimizer info:
INFO - 16:23:48: Status: None
INFO - 16:23:48: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:48: Solution:
INFO - 16:23:48: The solution is feasible.
INFO - 16:23:48: Objective: -2.173398336780509
INFO - 16:23:48: Standardized constraints:
INFO - 16:23:48: g_3 = [-8.26694979e-01 -1.73305021e-01 1.77635684e-15 -1.79835333e-01]
INFO - 16:23:48: Design space:
INFO - 16:23:48: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:48: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:48: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:48: | x_3 | 0.1 | 0.1611879493003633 | 1 | float |
INFO - 16:23:48: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:48: *** End PropulsionScenario execution (time: 0:00:00.019531) ***
INFO - 16:23:48: *** Start AerodynamicsScenario execution ***
INFO - 16:23:48: AerodynamicsScenario
INFO - 16:23:48: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:48: MDO formulation: MDF
INFO - 16:23:48: Optimization problem:
INFO - 16:23:48: minimize 0.001*-y_4(x_2)
INFO - 16:23:48: with respect to x_2
INFO - 16:23:48: under the inequality constraints
INFO - 16:23:48: g_2(x_2) <= 0
INFO - 16:23:48: over the design space:
INFO - 16:23:48: +------+-------------+-------+-------------+-------+
INFO - 16:23:48: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:48: +------+-------------+-------+-------------+-------+
INFO - 16:23:48: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:48: +------+-------------+-------+-------------+-------+
INFO - 16:23:48: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:48: 2%|▏ | 1/50 [00:00<00:00, 78.99 it/sec, feas=True, obj=-2.17]
INFO - 16:23:48: Optimization result:
INFO - 16:23:48: Optimizer info:
INFO - 16:23:48: Status: 8
INFO - 16:23:48: Message: Positive directional derivative for linesearch
INFO - 16:23:48: Solution:
INFO - 16:23:48: The solution is feasible.
INFO - 16:23:48: Objective: -2.173398336780509
INFO - 16:23:48: Standardized constraints:
INFO - 16:23:48: g_2 = -4.346970141155815e-05
INFO - 16:23:48: Design space:
INFO - 16:23:48: +------+-------------+-------+-------------+-------+
INFO - 16:23:48: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:48: +------+-------------+-------+-------------+-------+
INFO - 16:23:48: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:48: +------+-------------+-------+-------------+-------+
INFO - 16:23:48: *** End AerodynamicsScenario execution (time: 0:00:00.014285) ***
INFO - 16:23:48: 49%|████▉ | 49/100 [00:31<00:33, 1.54 it/sec, feas=True, obj=-2.17]
INFO - 16:23:48: *** Start PropulsionScenario execution ***
INFO - 16:23:48: PropulsionScenario
INFO - 16:23:48: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:48: MDO formulation: MDF
INFO - 16:23:48: Optimization problem:
INFO - 16:23:48: minimize 0.001*-y_4(x_3)
INFO - 16:23:48: with respect to x_3
INFO - 16:23:48: under the inequality constraints
INFO - 16:23:48: g_3(x_3) <= 0
INFO - 16:23:48: over the design space:
INFO - 16:23:48: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:48: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:48: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:48: | x_3 | 0.1 | 0.1611879493003633 | 1 | float |
INFO - 16:23:48: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:48: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:48: 2%|▏ | 1/50 [00:00<00:01, 38.23 it/sec, feas=False, obj=-2.25]
INFO - 16:23:48: 4%|▍ | 2/50 [00:00<00:01, 36.41 it/sec, feas=True, obj=-2.25]
INFO - 16:23:48: 6%|▌ | 3/50 [00:00<00:01, 30.69 it/sec, feas=False, obj=-2.25]
INFO - 16:23:48: 8%|▊ | 4/50 [00:00<00:01, 28.05 it/sec, feas=True, obj=-2.25]
INFO - 16:23:48: Optimization result:
INFO - 16:23:48: Optimizer info:
INFO - 16:23:48: Status: 8
INFO - 16:23:48: Message: Positive directional derivative for linesearch
INFO - 16:23:48: Solution:
INFO - 16:23:48: The solution is feasible.
INFO - 16:23:48: Objective: -2.2489621548200356
INFO - 16:23:48: Standardized constraints:
INFO - 16:23:48: g_3 = [-8.36394277e-01 -1.63605723e-01 2.22044605e-16 -1.81371504e-01]
INFO - 16:23:48: Design space:
INFO - 16:23:48: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:48: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:48: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:48: | x_3 | 0.1 | 0.1582575749424446 | 1 | float |
INFO - 16:23:48: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:48: *** End PropulsionScenario execution (time: 0:00:00.144837) ***
INFO - 16:23:48: *** Start AerodynamicsScenario execution ***
INFO - 16:23:48: AerodynamicsScenario
INFO - 16:23:48: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:48: MDO formulation: MDF
INFO - 16:23:48: Optimization problem:
INFO - 16:23:48: minimize 0.001*-y_4(x_2)
INFO - 16:23:48: with respect to x_2
INFO - 16:23:48: under the inequality constraints
INFO - 16:23:48: g_2(x_2) <= 0
INFO - 16:23:48: over the design space:
INFO - 16:23:48: +------+-------------+-------+-------------+-------+
INFO - 16:23:48: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:48: +------+-------------+-------+-------------+-------+
INFO - 16:23:48: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:48: +------+-------------+-------+-------------+-------+
INFO - 16:23:48: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:48: 2%|▏ | 1/50 [00:00<00:00, 103.47 it/sec, feas=True, obj=-2.25]
INFO - 16:23:48: Optimization result:
INFO - 16:23:48: Optimizer info:
INFO - 16:23:48: Status: 8
INFO - 16:23:48: Message: Positive directional derivative for linesearch
INFO - 16:23:48: Solution:
INFO - 16:23:48: The solution is feasible.
INFO - 16:23:48: Objective: -2.2489621548200356
INFO - 16:23:48: Standardized constraints:
INFO - 16:23:48: g_2 = 0.0
INFO - 16:23:48: Design space:
INFO - 16:23:48: +------+-------------+-------+-------------+-------+
INFO - 16:23:48: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:48: +------+-------------+-------+-------------+-------+
INFO - 16:23:48: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:48: +------+-------------+-------+-------------+-------+
INFO - 16:23:48: *** End AerodynamicsScenario execution (time: 0:00:00.011236) ***
INFO - 16:23:48: *** Start StructureScenario execution ***
INFO - 16:23:48: StructureScenario
INFO - 16:23:48: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:48: MDO formulation: MDF
INFO - 16:23:48: Optimization problem:
INFO - 16:23:48: minimize 0.001*-y_4(x_1)
INFO - 16:23:48: with respect to x_1
INFO - 16:23:48: under the inequality constraints
INFO - 16:23:48: g_1(x_1) <= 0
INFO - 16:23:48: over the design space:
INFO - 16:23:48: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:48: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:48: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:48: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:48: | x_1[1] | 0.75 | 0.7806436836765261 | 1.25 | float |
INFO - 16:23:48: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:48: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:48: 2%|▏ | 1/50 [00:00<00:00, 98.71 it/sec, feas=True, obj=-2.25]
INFO - 16:23:49: 4%|▍ | 2/50 [00:00<00:00, 145.80 it/sec, feas=True, obj=-2.25]
INFO - 16:23:49: 6%|▌ | 3/50 [00:00<00:00, 168.36 it/sec, feas=True, obj=-2.25]
INFO - 16:23:49: Optimization result:
INFO - 16:23:49: Optimizer info:
INFO - 16:23:49: Status: None
INFO - 16:23:49: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:49: Solution:
INFO - 16:23:49: The solution is feasible.
INFO - 16:23:49: Objective: -2.2489621548200356
INFO - 16:23:49: Standardized constraints:
INFO - 16:23:49: g_1 = [-0.0015959 -0.00202869 -0.0131333 -0.0232803 -0.03149672 -0.24
INFO - 16:23:49: 0. ]
INFO - 16:23:49: Design space:
INFO - 16:23:49: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:49: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:49: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:49: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:49: | x_1[1] | 0.75 | 0.7806436836765261 | 1.25 | float |
INFO - 16:23:49: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:49: *** End StructureScenario execution (time: 0:00:00.020123) ***
INFO - 16:23:49: *** Start PropulsionScenario execution ***
INFO - 16:23:49: PropulsionScenario
INFO - 16:23:49: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:49: MDO formulation: MDF
INFO - 16:23:49: Optimization problem:
INFO - 16:23:49: minimize 0.001*-y_4(x_3)
INFO - 16:23:49: with respect to x_3
INFO - 16:23:49: under the inequality constraints
INFO - 16:23:49: g_3(x_3) <= 0
INFO - 16:23:49: over the design space:
INFO - 16:23:49: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:49: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:49: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:49: | x_3 | 0.1 | 0.1582575749424446 | 1 | float |
INFO - 16:23:49: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:49: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:49: 2%|▏ | 1/50 [00:00<00:00, 78.59 it/sec, feas=True, obj=-2.25]
INFO - 16:23:49: Optimization result:
INFO - 16:23:49: Optimizer info:
INFO - 16:23:49: Status: 8
INFO - 16:23:49: Message: Positive directional derivative for linesearch
INFO - 16:23:49: Solution:
INFO - 16:23:49: The solution is feasible.
INFO - 16:23:49: Objective: -2.2489621548200356
INFO - 16:23:49: Standardized constraints:
INFO - 16:23:49: g_3 = [-8.36394277e-01 -1.63605723e-01 2.22044605e-16 -1.81371504e-01]
INFO - 16:23:49: Design space:
INFO - 16:23:49: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:49: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:49: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:49: | x_3 | 0.1 | 0.1582575749424446 | 1 | float |
INFO - 16:23:49: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:49: *** End PropulsionScenario execution (time: 0:00:00.014540) ***
INFO - 16:23:49: 50%|█████ | 50/100 [00:32<00:32, 1.56 it/sec, feas=True, obj=-2.25]
INFO - 16:23:49: *** Start PropulsionScenario execution ***
INFO - 16:23:49: PropulsionScenario
INFO - 16:23:49: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:49: MDO formulation: MDF
INFO - 16:23:49: Optimization problem:
INFO - 16:23:49: minimize 0.001*-y_4(x_3)
INFO - 16:23:49: with respect to x_3
INFO - 16:23:49: under the inequality constraints
INFO - 16:23:49: g_3(x_3) <= 0
INFO - 16:23:49: over the design space:
INFO - 16:23:49: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:49: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:49: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:49: | x_3 | 0.1 | 0.1582575749424446 | 1 | float |
INFO - 16:23:49: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:49: Solving optimization problem with algorithm SLSQP:
WARNING - 16:23:49: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 6.724932466608626e-05 is still above the tolerance 1e-06.
INFO - 16:23:49: 2%|▏ | 1/50 [00:00<00:01, 33.78 it/sec, feas=False, obj=-2.29]
INFO - 16:23:49: 4%|▍ | 2/50 [00:00<00:01, 36.23 it/sec, feas=True, obj=-2.29]
INFO - 16:23:49: 6%|▌ | 3/50 [00:00<00:01, 30.58 it/sec, feas=False, obj=-2.29]
INFO - 16:23:49: 8%|▊ | 4/50 [00:00<00:01, 28.52 it/sec, feas=True, obj=-2.29]
INFO - 16:23:49: 10%|█ | 5/50 [00:00<00:01, 30.09 it/sec, feas=True, obj=-2.29]
INFO - 16:23:49: 12%|█▏ | 6/50 [00:00<00:01, 31.19 it/sec, feas=True, obj=-2.29]
INFO - 16:23:49: Optimization result:
INFO - 16:23:49: Optimizer info:
INFO - 16:23:49: Status: None
INFO - 16:23:49: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:49: Solution:
INFO - 16:23:49: The solution is feasible.
INFO - 16:23:49: Objective: -2.289811005415896
INFO - 16:23:49: Standardized constraints:
INFO - 16:23:49: g_3 = [-8.45847003e-01 -1.54152997e-01 3.99680289e-15 -1.82815934e-01]
INFO - 16:23:49: Design space:
INFO - 16:23:49: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:49: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:49: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:49: | x_3 | 0.1 | 0.1567097273581975 | 1 | float |
INFO - 16:23:49: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:49: *** End PropulsionScenario execution (time: 0:00:00.194895) ***
INFO - 16:23:49: *** Start AerodynamicsScenario execution ***
INFO - 16:23:49: AerodynamicsScenario
INFO - 16:23:49: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:49: MDO formulation: MDF
INFO - 16:23:49: Optimization problem:
INFO - 16:23:49: minimize 0.001*-y_4(x_2)
INFO - 16:23:49: with respect to x_2
INFO - 16:23:49: under the inequality constraints
INFO - 16:23:49: g_2(x_2) <= 0
INFO - 16:23:49: over the design space:
INFO - 16:23:49: +------+-------------+-------+-------------+-------+
INFO - 16:23:49: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:49: +------+-------------+-------+-------------+-------+
INFO - 16:23:49: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:49: +------+-------------+-------+-------------+-------+
INFO - 16:23:49: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:49: 2%|▏ | 1/50 [00:00<00:00, 77.76 it/sec, feas=True, obj=-2.29]
INFO - 16:23:49: Optimization result:
INFO - 16:23:49: Optimizer info:
INFO - 16:23:49: Status: 8
INFO - 16:23:49: Message: Positive directional derivative for linesearch
INFO - 16:23:49: Solution:
INFO - 16:23:49: The solution is feasible.
INFO - 16:23:49: Objective: -2.289811005415896
INFO - 16:23:49: Standardized constraints:
INFO - 16:23:49: g_2 = 0.0
INFO - 16:23:49: Design space:
INFO - 16:23:49: +------+-------------+-------+-------------+-------+
INFO - 16:23:49: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:49: +------+-------------+-------+-------------+-------+
INFO - 16:23:49: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:49: +------+-------------+-------+-------------+-------+
INFO - 16:23:49: *** End AerodynamicsScenario execution (time: 0:00:00.014592) ***
INFO - 16:23:49: *** Start StructureScenario execution ***
INFO - 16:23:49: StructureScenario
INFO - 16:23:49: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:49: MDO formulation: MDF
INFO - 16:23:49: Optimization problem:
INFO - 16:23:49: minimize 0.001*-y_4(x_1)
INFO - 16:23:49: with respect to x_1
INFO - 16:23:49: under the inequality constraints
INFO - 16:23:49: g_1(x_1) <= 0
INFO - 16:23:49: over the design space:
INFO - 16:23:49: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:49: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:49: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:49: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:49: | x_1[1] | 0.75 | 0.7806436836765261 | 1.25 | float |
INFO - 16:23:49: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:49: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:49: 2%|▏ | 1/50 [00:00<00:00, 97.81 it/sec, feas=True, obj=-2.29]
INFO - 16:23:49: Optimization result:
INFO - 16:23:49: Optimizer info:
INFO - 16:23:49: Status: 8
INFO - 16:23:49: Message: Positive directional derivative for linesearch
INFO - 16:23:49: Solution:
INFO - 16:23:49: The solution is feasible.
INFO - 16:23:49: Objective: -2.289811005415896
INFO - 16:23:49: Standardized constraints:
INFO - 16:23:49: g_1 = [-0.0015959 -0.00202869 -0.0131333 -0.0232803 -0.03149672 -0.24
INFO - 16:23:49: 0. ]
INFO - 16:23:49: Design space:
INFO - 16:23:49: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:49: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:49: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:49: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:49: | x_1[1] | 0.75 | 0.7806436836765261 | 1.25 | float |
INFO - 16:23:49: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:49: *** End StructureScenario execution (time: 0:00:00.012293) ***
INFO - 16:23:49: *** Start PropulsionScenario execution ***
INFO - 16:23:49: PropulsionScenario
INFO - 16:23:49: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:49: MDO formulation: MDF
INFO - 16:23:49: Optimization problem:
INFO - 16:23:49: minimize 0.001*-y_4(x_3)
INFO - 16:23:49: with respect to x_3
INFO - 16:23:49: under the inequality constraints
INFO - 16:23:49: g_3(x_3) <= 0
INFO - 16:23:49: over the design space:
INFO - 16:23:49: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:49: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:49: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:49: | x_3 | 0.1 | 0.1567097273581975 | 1 | float |
INFO - 16:23:49: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:49: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:49: 2%|▏ | 1/50 [00:00<00:00, 110.52 it/sec, feas=True, obj=-2.29]
INFO - 16:23:49: 4%|▍ | 2/50 [00:00<00:00, 67.97 it/sec, feas=True, obj=-2.29]
INFO - 16:23:49: 6%|▌ | 3/50 [00:00<00:00, 89.62 it/sec, feas=True, obj=-2.29]
INFO - 16:23:49: Optimization result:
INFO - 16:23:49: Optimizer info:
INFO - 16:23:49: Status: None
INFO - 16:23:49: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:49: Solution:
INFO - 16:23:49: The solution is feasible.
INFO - 16:23:49: Objective: -2.289811005415897
INFO - 16:23:49: Standardized constraints:
INFO - 16:23:49: g_3 = [-8.45847003e-01 -1.54152997e-01 8.43769499e-15 -1.82815934e-01]
INFO - 16:23:49: Design space:
INFO - 16:23:49: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:49: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:49: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:49: | x_3 | 0.1 | 0.1567097273581982 | 1 | float |
INFO - 16:23:49: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:49: *** End PropulsionScenario execution (time: 0:00:00.035677) ***
INFO - 16:23:49: *** Start AerodynamicsScenario execution ***
INFO - 16:23:49: AerodynamicsScenario
INFO - 16:23:49: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:49: MDO formulation: MDF
INFO - 16:23:49: Optimization problem:
INFO - 16:23:49: minimize 0.001*-y_4(x_2)
INFO - 16:23:49: with respect to x_2
INFO - 16:23:49: under the inequality constraints
INFO - 16:23:49: g_2(x_2) <= 0
INFO - 16:23:49: over the design space:
INFO - 16:23:49: +------+-------------+-------+-------------+-------+
INFO - 16:23:49: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:49: +------+-------------+-------+-------------+-------+
INFO - 16:23:49: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:49: +------+-------------+-------+-------------+-------+
INFO - 16:23:49: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:49: 2%|▏ | 1/50 [00:00<00:00, 91.01 it/sec, feas=True, obj=-2.29]
INFO - 16:23:49: Optimization result:
INFO - 16:23:49: Optimizer info:
INFO - 16:23:49: Status: 8
INFO - 16:23:49: Message: Positive directional derivative for linesearch
INFO - 16:23:49: Solution:
INFO - 16:23:49: The solution is feasible.
INFO - 16:23:49: Objective: -2.289811005415897
INFO - 16:23:49: Standardized constraints:
INFO - 16:23:49: g_2 = 0.0
INFO - 16:23:49: Design space:
INFO - 16:23:49: +------+-------------+-------+-------------+-------+
INFO - 16:23:49: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:49: +------+-------------+-------+-------------+-------+
INFO - 16:23:49: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:49: +------+-------------+-------+-------------+-------+
INFO - 16:23:49: *** End AerodynamicsScenario execution (time: 0:00:00.012580) ***
INFO - 16:23:49: *** Start StructureScenario execution ***
INFO - 16:23:49: StructureScenario
INFO - 16:23:49: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:49: MDO formulation: MDF
INFO - 16:23:49: Optimization problem:
INFO - 16:23:49: minimize 0.001*-y_4(x_1)
INFO - 16:23:49: with respect to x_1
INFO - 16:23:49: under the inequality constraints
INFO - 16:23:49: g_1(x_1) <= 0
INFO - 16:23:49: over the design space:
INFO - 16:23:49: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:49: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:49: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:49: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:49: | x_1[1] | 0.75 | 0.7806436836765261 | 1.25 | float |
INFO - 16:23:49: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:49: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:49: 2%|▏ | 1/50 [00:00<00:00, 103.14 it/sec, feas=True, obj=-2.29]
INFO - 16:23:49: 4%|▍ | 2/50 [00:00<00:00, 65.41 it/sec, feas=True, obj=-2.29]
INFO - 16:23:49: 6%|▌ | 3/50 [00:00<00:00, 86.86 it/sec, feas=True, obj=-2.29]
INFO - 16:23:49: Optimization result:
INFO - 16:23:49: Optimizer info:
INFO - 16:23:49: Status: None
INFO - 16:23:49: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:49: Solution:
INFO - 16:23:49: The solution is feasible.
INFO - 16:23:49: Objective: -2.2898110054158978
INFO - 16:23:49: Standardized constraints:
INFO - 16:23:49: g_1 = [-1.59589593e-03 -2.02868890e-03 -1.31333010e-02 -2.32802973e-02
INFO - 16:23:49: -3.14967236e-02 -2.40000000e-01 1.11022302e-16]
INFO - 16:23:49: Design space:
INFO - 16:23:49: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:49: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:49: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:49: | x_1[0] | 0.1 | 0.1000000000000002 | 0.4 | float |
INFO - 16:23:49: | x_1[1] | 0.75 | 0.780643683676526 | 1.25 | float |
INFO - 16:23:49: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:49: *** End StructureScenario execution (time: 0:00:00.036976) ***
INFO - 16:23:49: 51%|█████ | 51/100 [00:32<00:31, 1.57 it/sec, feas=True, obj=-2.29]
INFO - 16:23:49: *** Start PropulsionScenario execution ***
INFO - 16:23:49: PropulsionScenario
INFO - 16:23:49: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:49: MDO formulation: MDF
INFO - 16:23:49: Optimization problem:
INFO - 16:23:49: minimize 0.001*-y_4(x_3)
INFO - 16:23:49: with respect to x_3
INFO - 16:23:49: under the inequality constraints
INFO - 16:23:49: g_3(x_3) <= 0
INFO - 16:23:49: over the design space:
INFO - 16:23:49: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:49: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:49: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:49: | x_3 | 0.1 | 0.1567097273581982 | 1 | float |
INFO - 16:23:49: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:49: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:49: 2%|▏ | 1/50 [00:00<00:01, 38.16 it/sec, feas=True, obj=-2.24]
INFO - 16:23:49: 4%|▍ | 2/50 [00:00<00:01, 29.15 it/sec, feas=True, obj=-2.25]
INFO - 16:23:49: 6%|▌ | 3/50 [00:00<00:01, 31.31 it/sec, feas=True, obj=-2.25]
INFO - 16:23:49: 8%|▊ | 4/50 [00:00<00:01, 28.72 it/sec, feas=True, obj=-2.25]
INFO - 16:23:49: Optimization result:
INFO - 16:23:49: Optimizer info:
INFO - 16:23:49: Status: None
INFO - 16:23:49: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:49: Solution:
INFO - 16:23:49: The solution is feasible.
INFO - 16:23:49: Objective: -2.2460746089820085
INFO - 16:23:49: Standardized constraints:
INFO - 16:23:49: g_3 = [-8.32794952e-01 -1.67205048e-01 4.88498131e-15 -1.81420616e-01]
INFO - 16:23:49: Design space:
INFO - 16:23:49: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:49: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:49: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:49: | x_3 | 0.1 | 0.1582814603997714 | 1 | float |
INFO - 16:23:49: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:49: *** End PropulsionScenario execution (time: 0:00:00.141756) ***
INFO - 16:23:49: *** Start AerodynamicsScenario execution ***
INFO - 16:23:49: AerodynamicsScenario
INFO - 16:23:49: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:49: MDO formulation: MDF
INFO - 16:23:49: Optimization problem:
INFO - 16:23:49: minimize 0.001*-y_4(x_2)
INFO - 16:23:49: with respect to x_2
INFO - 16:23:49: under the inequality constraints
INFO - 16:23:49: g_2(x_2) <= 0
INFO - 16:23:49: over the design space:
INFO - 16:23:49: +------+-------------+-------+-------------+-------+
INFO - 16:23:49: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:49: +------+-------------+-------+-------------+-------+
INFO - 16:23:49: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:49: +------+-------------+-------+-------------+-------+
INFO - 16:23:49: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:49: 2%|▏ | 1/50 [00:00<00:00, 76.71 it/sec, feas=True, obj=-2.25]
INFO - 16:23:49: Optimization result:
INFO - 16:23:49: Optimizer info:
INFO - 16:23:49: Status: 8
INFO - 16:23:49: Message: Positive directional derivative for linesearch
INFO - 16:23:49: Solution:
INFO - 16:23:49: The solution is feasible.
INFO - 16:23:49: Objective: -2.2460746089820085
INFO - 16:23:49: Standardized constraints:
INFO - 16:23:49: g_2 = 3.488784171801207e-05
INFO - 16:23:49: Design space:
INFO - 16:23:49: +------+-------------+-------+-------------+-------+
INFO - 16:23:49: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:49: +------+-------------+-------+-------------+-------+
INFO - 16:23:49: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:49: +------+-------------+-------+-------------+-------+
INFO - 16:23:49: *** End AerodynamicsScenario execution (time: 0:00:00.014836) ***
INFO - 16:23:49: *** Start StructureScenario execution ***
INFO - 16:23:49: StructureScenario
INFO - 16:23:49: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:49: MDO formulation: MDF
INFO - 16:23:49: Optimization problem:
INFO - 16:23:49: minimize 0.001*-y_4(x_1)
INFO - 16:23:49: with respect to x_1
INFO - 16:23:49: under the inequality constraints
INFO - 16:23:49: g_1(x_1) <= 0
INFO - 16:23:49: over the design space:
INFO - 16:23:49: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:49: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:49: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:49: | x_1[0] | 0.1 | 0.1000000000000002 | 0.4 | float |
INFO - 16:23:49: | x_1[1] | 0.75 | 0.780643683676526 | 1.25 | float |
INFO - 16:23:49: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:49: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:49: 2%|▏ | 1/50 [00:00<00:00, 97.87 it/sec, feas=True, obj=-2.25]
INFO - 16:23:49: 4%|▍ | 2/50 [00:00<00:00, 70.12 it/sec, feas=True, obj=-2.25]
INFO - 16:23:49: 6%|▌ | 3/50 [00:00<00:00, 87.36 it/sec, feas=True, obj=-2.25]
INFO - 16:23:49: Optimization result:
INFO - 16:23:49: Optimizer info:
INFO - 16:23:49: Status: None
INFO - 16:23:49: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:49: Solution:
INFO - 16:23:49: The solution is feasible.
INFO - 16:23:49: Objective: -2.2460746089820542
INFO - 16:23:49: Standardized constraints:
INFO - 16:23:49: g_1 = [-1.87551990e-03 -2.18203942e-03 -1.32359144e-02 -2.33564362e-02
INFO - 16:23:49: -3.15568661e-02 -2.40000000e-01 3.43058915e-14]
INFO - 16:23:49: Design space:
INFO - 16:23:49: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:49: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:49: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:49: | x_1[0] | 0.1 | 0.100000000000082 | 0.4 | float |
INFO - 16:23:49: | x_1[1] | 0.75 | 0.7806436836764953 | 1.25 | float |
INFO - 16:23:49: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:49: *** End StructureScenario execution (time: 0:00:00.036894) ***
INFO - 16:23:49: *** Start PropulsionScenario execution ***
INFO - 16:23:49: PropulsionScenario
INFO - 16:23:49: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:49: MDO formulation: MDF
INFO - 16:23:49: Optimization problem:
INFO - 16:23:49: minimize 0.001*-y_4(x_3)
INFO - 16:23:49: with respect to x_3
INFO - 16:23:49: under the inequality constraints
INFO - 16:23:49: g_3(x_3) <= 0
INFO - 16:23:49: over the design space:
INFO - 16:23:49: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:49: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:49: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:49: | x_3 | 0.1 | 0.1582814603997714 | 1 | float |
INFO - 16:23:49: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:49: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:49: 2%|▏ | 1/50 [00:00<00:00, 92.75 it/sec, feas=True, obj=-2.25]
INFO - 16:23:49: Optimization result:
INFO - 16:23:49: Optimizer info:
INFO - 16:23:49: Status: 8
INFO - 16:23:49: Message: Positive directional derivative for linesearch
INFO - 16:23:49: Solution:
INFO - 16:23:49: The solution is feasible.
INFO - 16:23:49: Objective: -2.2460746089820542
INFO - 16:23:49: Standardized constraints:
INFO - 16:23:49: g_3 = [-8.32794952e-01 -1.67205048e-01 4.88498131e-15 -1.81420616e-01]
INFO - 16:23:49: Design space:
INFO - 16:23:49: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:49: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:49: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:49: | x_3 | 0.1 | 0.1582814603997714 | 1 | float |
INFO - 16:23:49: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:49: *** End PropulsionScenario execution (time: 0:00:00.012825) ***
INFO - 16:23:49: *** Start AerodynamicsScenario execution ***
INFO - 16:23:49: AerodynamicsScenario
INFO - 16:23:49: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:49: MDO formulation: MDF
INFO - 16:23:49: Optimization problem:
INFO - 16:23:49: minimize 0.001*-y_4(x_2)
INFO - 16:23:49: with respect to x_2
INFO - 16:23:49: under the inequality constraints
INFO - 16:23:49: g_2(x_2) <= 0
INFO - 16:23:49: over the design space:
INFO - 16:23:49: +------+-------------+-------+-------------+-------+
INFO - 16:23:49: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:49: +------+-------------+-------+-------------+-------+
INFO - 16:23:49: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:49: +------+-------------+-------+-------------+-------+
INFO - 16:23:49: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:49: 2%|▏ | 1/50 [00:00<00:00, 90.14 it/sec, feas=True, obj=-2.25]
INFO - 16:23:49: Optimization result:
INFO - 16:23:49: Optimizer info:
INFO - 16:23:49: Status: 8
INFO - 16:23:49: Message: Positive directional derivative for linesearch
INFO - 16:23:49: Solution:
INFO - 16:23:49: The solution is feasible.
INFO - 16:23:49: Objective: -2.2460746089820542
INFO - 16:23:49: Standardized constraints:
INFO - 16:23:49: g_2 = 3.488784171801207e-05
INFO - 16:23:49: Design space:
INFO - 16:23:49: +------+-------------+-------+-------------+-------+
INFO - 16:23:49: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:49: +------+-------------+-------+-------------+-------+
INFO - 16:23:49: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:49: +------+-------------+-------+-------------+-------+
INFO - 16:23:49: *** End AerodynamicsScenario execution (time: 0:00:00.012653) ***
INFO - 16:23:49: *** Start StructureScenario execution ***
INFO - 16:23:49: StructureScenario
INFO - 16:23:49: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:49: MDO formulation: MDF
INFO - 16:23:49: Optimization problem:
INFO - 16:23:49: minimize 0.001*-y_4(x_1)
INFO - 16:23:49: with respect to x_1
INFO - 16:23:49: under the inequality constraints
INFO - 16:23:49: g_1(x_1) <= 0
INFO - 16:23:49: over the design space:
INFO - 16:23:49: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:49: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:49: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:49: | x_1[0] | 0.1 | 0.100000000000082 | 0.4 | float |
INFO - 16:23:49: | x_1[1] | 0.75 | 0.7806436836764953 | 1.25 | float |
INFO - 16:23:49: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:49: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:49: 2%|▏ | 1/50 [00:00<00:00, 103.59 it/sec, feas=True, obj=-2.25]
INFO - 16:23:49: 4%|▍ | 2/50 [00:00<00:00, 63.08 it/sec, feas=True, obj=-2.25]
INFO - 16:23:49: 6%|▌ | 3/50 [00:00<00:00, 78.56 it/sec, feas=True, obj=-2.25]
INFO - 16:23:49: Optimization result:
INFO - 16:23:49: Optimizer info:
INFO - 16:23:49: Status: None
INFO - 16:23:49: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:49: Solution:
INFO - 16:23:49: The solution is feasible.
INFO - 16:23:49: Objective: -2.2460746089820542
INFO - 16:23:49: Standardized constraints:
INFO - 16:23:49: g_1 = [-1.87551990e-03 -2.18203942e-03 -1.32359144e-02 -2.33564362e-02
INFO - 16:23:49: -3.15568661e-02 -2.40000000e-01 3.43058915e-14]
INFO - 16:23:49: Design space:
INFO - 16:23:49: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:49: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:49: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:49: | x_1[0] | 0.1 | 0.100000000000082 | 0.4 | float |
INFO - 16:23:49: | x_1[1] | 0.75 | 0.7806436836764953 | 1.25 | float |
INFO - 16:23:49: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:49: *** End StructureScenario execution (time: 0:00:00.040630) ***
INFO - 16:23:49: 52%|█████▏ | 52/100 [00:32<00:30, 1.59 it/sec, feas=True, obj=-2.25]
INFO - 16:23:49: *** Start PropulsionScenario execution ***
INFO - 16:23:49: PropulsionScenario
INFO - 16:23:49: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:49: MDO formulation: MDF
INFO - 16:23:49: Optimization problem:
INFO - 16:23:49: minimize 0.001*-y_4(x_3)
INFO - 16:23:49: with respect to x_3
INFO - 16:23:49: under the inequality constraints
INFO - 16:23:49: g_3(x_3) <= 0
INFO - 16:23:49: over the design space:
INFO - 16:23:49: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:49: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:49: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:49: | x_3 | 0.1 | 0.1582814603997714 | 1 | float |
INFO - 16:23:49: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:49: Solving optimization problem with algorithm SLSQP:
WARNING - 16:23:49: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 0.00013449864933217252 is still above the tolerance 1e-06.
INFO - 16:23:49: 2%|▏ | 1/50 [00:00<00:01, 33.50 it/sec, feas=False, obj=-2.3]
WARNING - 16:23:49: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 6.724932466608626e-05 is still above the tolerance 1e-06.
INFO - 16:23:49: 4%|▍ | 2/50 [00:00<00:01, 33.30 it/sec, feas=True, obj=-2.29]
WARNING - 16:23:49: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 6.724932466608626e-05 is still above the tolerance 1e-06.
INFO - 16:23:49: 6%|▌ | 3/50 [00:00<00:01, 27.69 it/sec, feas=False, obj=-2.3]
INFO - 16:23:49: 8%|▊ | 4/50 [00:00<00:01, 26.39 it/sec, feas=True, obj=-2.29]
INFO - 16:23:49: 10%|█ | 5/50 [00:00<00:01, 27.93 it/sec, feas=True, obj=-2.29]
INFO - 16:23:49: 12%|█▏ | 6/50 [00:00<00:01, 29.02 it/sec, feas=True, obj=-2.29]
INFO - 16:23:49: Optimization result:
INFO - 16:23:49: Optimizer info:
INFO - 16:23:49: Status: None
INFO - 16:23:49: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:49: Solution:
INFO - 16:23:49: The solution is feasible.
INFO - 16:23:49: Objective: -2.2928387135182664
INFO - 16:23:49: Standardized constraints:
INFO - 16:23:49: g_3 = [-8.44997477e-01 -1.55002523e-01 5.10702591e-15 -1.82789836e-01]
INFO - 16:23:49: Design space:
INFO - 16:23:49: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:49: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:49: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:49: | x_3 | 0.1 | 0.1567374485809811 | 1 | float |
INFO - 16:23:49: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:49: *** End PropulsionScenario execution (time: 0:00:00.209629) ***
INFO - 16:23:49: *** Start AerodynamicsScenario execution ***
INFO - 16:23:49: AerodynamicsScenario
INFO - 16:23:49: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:49: MDO formulation: MDF
INFO - 16:23:49: Optimization problem:
INFO - 16:23:49: minimize 0.001*-y_4(x_2)
INFO - 16:23:49: with respect to x_2
INFO - 16:23:49: under the inequality constraints
INFO - 16:23:49: g_2(x_2) <= 0
INFO - 16:23:49: over the design space:
INFO - 16:23:49: +------+-------------+-------+-------------+-------+
INFO - 16:23:49: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:49: +------+-------------+-------+-------------+-------+
INFO - 16:23:49: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:49: +------+-------------+-------+-------------+-------+
INFO - 16:23:49: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:49: 2%|▏ | 1/50 [00:00<00:00, 74.18 it/sec, feas=True, obj=-2.29]
INFO - 16:23:49: Optimization result:
INFO - 16:23:49: Optimizer info:
INFO - 16:23:49: Status: 8
INFO - 16:23:49: Message: Positive directional derivative for linesearch
INFO - 16:23:49: Solution:
INFO - 16:23:49: The solution is feasible.
INFO - 16:23:49: Objective: -2.2928387135182664
INFO - 16:23:49: Standardized constraints:
INFO - 16:23:49: g_2 = 0.0
INFO - 16:23:49: Design space:
INFO - 16:23:49: +------+-------------+-------+-------------+-------+
INFO - 16:23:49: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:49: +------+-------------+-------+-------------+-------+
INFO - 16:23:49: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:49: +------+-------------+-------+-------------+-------+
INFO - 16:23:49: *** End AerodynamicsScenario execution (time: 0:00:00.015221) ***
INFO - 16:23:49: *** Start StructureScenario execution ***
INFO - 16:23:49: StructureScenario
INFO - 16:23:49: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:49: MDO formulation: MDF
INFO - 16:23:49: Optimization problem:
INFO - 16:23:49: minimize 0.001*-y_4(x_1)
INFO - 16:23:49: with respect to x_1
INFO - 16:23:49: under the inequality constraints
INFO - 16:23:49: g_1(x_1) <= 0
INFO - 16:23:49: over the design space:
INFO - 16:23:49: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:49: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:49: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:49: | x_1[0] | 0.1 | 0.100000000000082 | 0.4 | float |
INFO - 16:23:49: | x_1[1] | 0.75 | 0.7806436836764953 | 1.25 | float |
INFO - 16:23:49: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:49: Solving optimization problem with algorithm SLSQP:
WARNING - 16:23:49: MDAGaussSeidel has reached its maximum number of unsuccessful iterations, but the normalized residual norm 0.0009157477359807847 is still above the tolerance 1e-06.
INFO - 16:23:49: 2%|▏ | 1/50 [00:00<00:00, 52.28 it/sec, feas=True, obj=-2.29]
INFO - 16:23:49: 4%|▍ | 2/50 [00:00<00:01, 46.88 it/sec, feas=True, obj=-2.29]
INFO - 16:23:49: 6%|▌ | 3/50 [00:00<00:01, 45.29 it/sec, feas=True, obj=-2.29]
INFO - 16:23:49: Optimization result:
INFO - 16:23:49: Optimizer info:
INFO - 16:23:49: Status: 8
INFO - 16:23:49: Message: Positive directional derivative for linesearch
INFO - 16:23:49: Solution:
INFO - 16:23:49: The solution is feasible.
INFO - 16:23:49: Objective: -2.2928387135182664
INFO - 16:23:49: Standardized constraints:
INFO - 16:23:49: g_1 = [-1.59589593e-03 -2.02868890e-03 -1.31333010e-02 -2.32802973e-02
INFO - 16:23:49: -3.14967236e-02 -2.40000000e-01 3.43058915e-14]
INFO - 16:23:49: Design space:
INFO - 16:23:49: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:49: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:49: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:49: | x_1[0] | 0.1 | 0.100000000000082 | 0.4 | float |
INFO - 16:23:49: | x_1[1] | 0.75 | 0.7806436836764953 | 1.25 | float |
INFO - 16:23:49: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:49: *** End StructureScenario execution (time: 0:00:00.068568) ***
WARNING - 16:23:50: MDAGaussSeidel has reached its maximum number of unsuccessful iterations, but the normalized residual norm 0.0009157477359807847 is still above the tolerance 1e-06.
INFO - 16:23:50: *** Start PropulsionScenario execution ***
INFO - 16:23:50: PropulsionScenario
INFO - 16:23:50: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:50: MDO formulation: MDF
INFO - 16:23:50: Optimization problem:
INFO - 16:23:50: minimize 0.001*-y_4(x_3)
INFO - 16:23:50: with respect to x_3
INFO - 16:23:50: under the inequality constraints
INFO - 16:23:50: g_3(x_3) <= 0
INFO - 16:23:50: over the design space:
INFO - 16:23:50: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:50: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:50: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:50: | x_3 | 0.1 | 0.1567374485809811 | 1 | float |
INFO - 16:23:50: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:50: Solving optimization problem with algorithm SLSQP:
WARNING - 16:23:50: MDAGaussSeidel has reached its maximum number of unsuccessful iterations, but the normalized residual norm 6.724932466608626e-05 is still above the tolerance 1e-06.
INFO - 16:23:50: 2%|▏ | 1/50 [00:00<00:00, 52.20 it/sec, feas=True, obj=-2.29]
INFO - 16:23:50: Optimization result:
INFO - 16:23:50: Optimizer info:
INFO - 16:23:50: Status: 8
INFO - 16:23:50: Message: Positive directional derivative for linesearch
INFO - 16:23:50: Solution:
INFO - 16:23:50: The solution is feasible.
INFO - 16:23:50: Objective: -2.2928387135182664
INFO - 16:23:50: Standardized constraints:
INFO - 16:23:50: g_3 = [-8.44997477e-01 -1.55002523e-01 5.10702591e-15 -1.82789836e-01]
INFO - 16:23:50: Design space:
INFO - 16:23:50: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:50: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:50: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:50: | x_3 | 0.1 | 0.1567374485809811 | 1 | float |
INFO - 16:23:50: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:50: *** End PropulsionScenario execution (time: 0:00:00.021062) ***
INFO - 16:23:50: *** Start AerodynamicsScenario execution ***
INFO - 16:23:50: AerodynamicsScenario
INFO - 16:23:50: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:50: MDO formulation: MDF
INFO - 16:23:50: Optimization problem:
INFO - 16:23:50: minimize 0.001*-y_4(x_2)
INFO - 16:23:50: with respect to x_2
INFO - 16:23:50: under the inequality constraints
INFO - 16:23:50: g_2(x_2) <= 0
INFO - 16:23:50: over the design space:
INFO - 16:23:50: +------+-------------+-------+-------------+-------+
INFO - 16:23:50: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:50: +------+-------------+-------+-------------+-------+
INFO - 16:23:50: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:50: +------+-------------+-------+-------------+-------+
INFO - 16:23:50: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:50: 2%|▏ | 1/50 [00:00<00:00, 83.18 it/sec, feas=True, obj=-2.29]
INFO - 16:23:50: Optimization result:
INFO - 16:23:50: Optimizer info:
INFO - 16:23:50: Status: 8
INFO - 16:23:50: Message: Positive directional derivative for linesearch
INFO - 16:23:50: Solution:
INFO - 16:23:50: The solution is feasible.
INFO - 16:23:50: Objective: -2.2928387135182664
INFO - 16:23:50: Standardized constraints:
INFO - 16:23:50: g_2 = 0.0
INFO - 16:23:50: Design space:
INFO - 16:23:50: +------+-------------+-------+-------------+-------+
INFO - 16:23:50: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:50: +------+-------------+-------+-------------+-------+
INFO - 16:23:50: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:50: +------+-------------+-------+-------------+-------+
INFO - 16:23:50: *** End AerodynamicsScenario execution (time: 0:00:00.013683) ***
INFO - 16:23:50: 53%|█████▎ | 53/100 [00:33<00:29, 1.60 it/sec, feas=True, obj=-2.29]
INFO - 16:23:50: *** Start PropulsionScenario execution ***
INFO - 16:23:50: PropulsionScenario
INFO - 16:23:50: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:50: MDO formulation: MDF
INFO - 16:23:50: Optimization problem:
INFO - 16:23:50: minimize 0.001*-y_4(x_3)
INFO - 16:23:50: with respect to x_3
INFO - 16:23:50: under the inequality constraints
INFO - 16:23:50: g_3(x_3) <= 0
INFO - 16:23:50: over the design space:
INFO - 16:23:50: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:50: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:50: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:50: | x_3 | 0.1 | 0.1567374485809811 | 1 | float |
INFO - 16:23:50: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:50: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:50: 2%|▏ | 1/50 [00:00<00:01, 38.59 it/sec, feas=True, obj=-2.22]
INFO - 16:23:50: 4%|▍ | 2/50 [00:00<00:01, 28.90 it/sec, feas=True, obj=-2.23]
INFO - 16:23:50: Optimization result:
INFO - 16:23:50: Optimizer info:
INFO - 16:23:50: Status: 8
INFO - 16:23:50: Message: Positive directional derivative for linesearch
INFO - 16:23:50: Solution:
INFO - 16:23:50: The solution is feasible.
INFO - 16:23:50: Objective: -2.228804164453142
INFO - 16:23:50: Standardized constraints:
INFO - 16:23:50: g_3 = [-8.30866009e-01 -1.69133991e-01 3.77475828e-15 -1.81430675e-01]
INFO - 16:23:50: Design space:
INFO - 16:23:50: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:50: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:50: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:50: | x_3 | 0.1 | 0.1594158049214066 | 1 | float |
INFO - 16:23:50: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:50: *** End PropulsionScenario execution (time: 0:00:00.071193) ***
INFO - 16:23:50: *** Start AerodynamicsScenario execution ***
INFO - 16:23:50: AerodynamicsScenario
INFO - 16:23:50: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:50: MDO formulation: MDF
INFO - 16:23:50: Optimization problem:
INFO - 16:23:50: minimize 0.001*-y_4(x_2)
INFO - 16:23:50: with respect to x_2
INFO - 16:23:50: under the inequality constraints
INFO - 16:23:50: g_2(x_2) <= 0
INFO - 16:23:50: over the design space:
INFO - 16:23:50: +------+-------------+-------+-------------+-------+
INFO - 16:23:50: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:50: +------+-------------+-------+-------------+-------+
INFO - 16:23:50: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:50: +------+-------------+-------+-------------+-------+
INFO - 16:23:50: Solving optimization problem with algorithm SLSQP:
WARNING - 16:23:50: Optimization found no feasible point; the least infeasible point is selected.
INFO - 16:23:50: 2%|▏ | 1/50 [00:00<00:00, 104.10 it/sec, feas=False, obj=-2.23]
INFO - 16:23:50: Optimization result:
INFO - 16:23:50: Optimizer info:
INFO - 16:23:50: Status: 8
INFO - 16:23:50: Message: Positive directional derivative for linesearch
INFO - 16:23:50: Solution:
WARNING - 16:23:50: The solution is not feasible.
INFO - 16:23:50: Objective: -2.228804164453142
INFO - 16:23:50: Standardized constraints:
INFO - 16:23:50: g_2 = 0.0008286965265367208
INFO - 16:23:50: Design space:
INFO - 16:23:50: +------+-------------+-------+-------------+-------+
INFO - 16:23:50: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:50: +------+-------------+-------+-------------+-------+
INFO - 16:23:50: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:50: +------+-------------+-------+-------------+-------+
INFO - 16:23:50: *** End AerodynamicsScenario execution (time: 0:00:00.011196) ***
INFO - 16:23:50: *** Start StructureScenario execution ***
INFO - 16:23:50: StructureScenario
INFO - 16:23:50: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:50: MDO formulation: MDF
INFO - 16:23:50: Optimization problem:
INFO - 16:23:50: minimize 0.001*-y_4(x_1)
INFO - 16:23:50: with respect to x_1
INFO - 16:23:50: under the inequality constraints
INFO - 16:23:50: g_1(x_1) <= 0
INFO - 16:23:50: over the design space:
INFO - 16:23:50: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:50: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:50: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:50: | x_1[0] | 0.1 | 0.100000000000082 | 0.4 | float |
INFO - 16:23:50: | x_1[1] | 0.75 | 0.7806436836764953 | 1.25 | float |
INFO - 16:23:50: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:50: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:50: 2%|▏ | 1/50 [00:00<00:00, 98.06 it/sec, feas=True, obj=-2.23]
INFO - 16:23:50: 4%|▍ | 2/50 [00:00<00:00, 59.19 it/sec, feas=True, obj=-2.23]
INFO - 16:23:50: 6%|▌ | 3/50 [00:00<00:00, 71.23 it/sec, feas=True, obj=-2.23]
INFO - 16:23:50: Optimization result:
INFO - 16:23:50: Optimizer info:
INFO - 16:23:50: Status: None
INFO - 16:23:50: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:50: Solution:
INFO - 16:23:50: The solution is feasible.
INFO - 16:23:50: Objective: -2.228804164453142
INFO - 16:23:50: Standardized constraints:
INFO - 16:23:50: g_1 = [-8.25840618e-03 -5.68038501e-03 -1.55758316e-02 -2.50921258e-02
INFO - 16:23:50: -3.29275830e-02 -2.40000000e-01 3.43058915e-14]
INFO - 16:23:50: Design space:
INFO - 16:23:50: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:50: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:50: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:50: | x_1[0] | 0.1 | 0.100000000000082 | 0.4 | float |
INFO - 16:23:50: | x_1[1] | 0.75 | 0.7806436836764953 | 1.25 | float |
INFO - 16:23:50: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:50: *** End StructureScenario execution (time: 0:00:00.044610) ***
INFO - 16:23:50: *** Start PropulsionScenario execution ***
INFO - 16:23:50: PropulsionScenario
INFO - 16:23:50: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:50: MDO formulation: MDF
INFO - 16:23:50: Optimization problem:
INFO - 16:23:50: minimize 0.001*-y_4(x_3)
INFO - 16:23:50: with respect to x_3
INFO - 16:23:50: under the inequality constraints
INFO - 16:23:50: g_3(x_3) <= 0
INFO - 16:23:50: over the design space:
INFO - 16:23:50: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:50: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:50: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:50: | x_3 | 0.1 | 0.1594158049214066 | 1 | float |
INFO - 16:23:50: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:50: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:50: 2%|▏ | 1/50 [00:00<00:00, 90.99 it/sec, feas=True, obj=-2.23]
INFO - 16:23:50: Optimization result:
INFO - 16:23:50: Optimizer info:
INFO - 16:23:50: Status: 8
INFO - 16:23:50: Message: Positive directional derivative for linesearch
INFO - 16:23:50: Solution:
INFO - 16:23:50: The solution is feasible.
INFO - 16:23:50: Objective: -2.228804164453142
INFO - 16:23:50: Standardized constraints:
INFO - 16:23:50: g_3 = [-8.30866009e-01 -1.69133991e-01 3.77475828e-15 -1.81430675e-01]
INFO - 16:23:50: Design space:
INFO - 16:23:50: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:50: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:50: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:50: | x_3 | 0.1 | 0.1594158049214066 | 1 | float |
INFO - 16:23:50: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:50: *** End PropulsionScenario execution (time: 0:00:00.012915) ***
INFO - 16:23:50: 54%|█████▍ | 54/100 [00:33<00:28, 1.62 it/sec, feas=False, obj=-2.23]
INFO - 16:23:50: *** Start PropulsionScenario execution ***
INFO - 16:23:50: PropulsionScenario
INFO - 16:23:50: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:50: MDO formulation: MDF
INFO - 16:23:50: Optimization problem:
INFO - 16:23:50: minimize 0.001*-y_4(x_3)
INFO - 16:23:50: with respect to x_3
INFO - 16:23:50: under the inequality constraints
INFO - 16:23:50: g_3(x_3) <= 0
INFO - 16:23:50: over the design space:
INFO - 16:23:50: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:50: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:50: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:50: | x_3 | 0.1 | 0.1594158049214066 | 1 | float |
INFO - 16:23:50: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:50: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:50: 2%|▏ | 1/50 [00:00<00:01, 37.28 it/sec, feas=False, obj=-2.3]
INFO - 16:23:50: 4%|▍ | 2/50 [00:00<00:01, 37.99 it/sec, feas=True, obj=-2.3]
INFO - 16:23:50: 6%|▌ | 3/50 [00:00<00:01, 31.23 it/sec, feas=False, obj=-2.3]
INFO - 16:23:50: 8%|▊ | 4/50 [00:00<00:01, 28.84 it/sec, feas=True, obj=-2.3]
INFO - 16:23:50: 10%|█ | 5/50 [00:00<00:01, 27.60 it/sec, feas=True, obj=-2.3]
INFO - 16:23:50: 12%|█▏ | 6/50 [00:00<00:01, 28.77 it/sec, feas=True, obj=-2.3]
INFO - 16:23:50: Optimization result:
INFO - 16:23:50: Optimizer info:
INFO - 16:23:50: Status: None
INFO - 16:23:50: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:50: Solution:
INFO - 16:23:50: The solution is feasible.
INFO - 16:23:50: Objective: -2.295629627022848
INFO - 16:23:50: Standardized constraints:
INFO - 16:23:50: g_3 = [-8.43889034e-01 -1.56110966e-01 3.99680289e-15 -1.82842945e-01]
INFO - 16:23:50: Design space:
INFO - 16:23:50: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:50: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:50: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:50: | x_3 | 0.1 | 0.1566810472685422 | 1 | float |
INFO - 16:23:50: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:50: *** End PropulsionScenario execution (time: 0:00:00.211028) ***
INFO - 16:23:50: *** Start AerodynamicsScenario execution ***
INFO - 16:23:50: AerodynamicsScenario
INFO - 16:23:50: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:50: MDO formulation: MDF
INFO - 16:23:50: Optimization problem:
INFO - 16:23:50: minimize 0.001*-y_4(x_2)
INFO - 16:23:50: with respect to x_2
INFO - 16:23:50: under the inequality constraints
INFO - 16:23:50: g_2(x_2) <= 0
INFO - 16:23:50: over the design space:
INFO - 16:23:50: +------+-------------+-------+-------------+-------+
INFO - 16:23:50: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:50: +------+-------------+-------+-------------+-------+
INFO - 16:23:50: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:50: +------+-------------+-------+-------------+-------+
INFO - 16:23:50: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:50: 2%|▏ | 1/50 [00:00<00:00, 90.67 it/sec, feas=True, obj=-2.3]
INFO - 16:23:50: Optimization result:
INFO - 16:23:50: Optimizer info:
INFO - 16:23:50: Status: 8
INFO - 16:23:50: Message: Positive directional derivative for linesearch
INFO - 16:23:50: Solution:
INFO - 16:23:50: The solution is feasible.
INFO - 16:23:50: Objective: -2.295629627022848
INFO - 16:23:50: Standardized constraints:
INFO - 16:23:50: g_2 = 0.0
INFO - 16:23:50: Design space:
INFO - 16:23:50: +------+-------------+-------+-------------+-------+
INFO - 16:23:50: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:50: +------+-------------+-------+-------------+-------+
INFO - 16:23:50: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:50: +------+-------------+-------+-------------+-------+
INFO - 16:23:50: *** End AerodynamicsScenario execution (time: 0:00:00.012717) ***
INFO - 16:23:50: *** Start StructureScenario execution ***
INFO - 16:23:50: StructureScenario
INFO - 16:23:50: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:50: MDO formulation: MDF
INFO - 16:23:50: Optimization problem:
INFO - 16:23:50: minimize 0.001*-y_4(x_1)
INFO - 16:23:50: with respect to x_1
INFO - 16:23:50: under the inequality constraints
INFO - 16:23:50: g_1(x_1) <= 0
INFO - 16:23:50: over the design space:
INFO - 16:23:50: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:50: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:50: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:50: | x_1[0] | 0.1 | 0.100000000000082 | 0.4 | float |
INFO - 16:23:50: | x_1[1] | 0.75 | 0.7806436836764953 | 1.25 | float |
INFO - 16:23:50: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:50: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:50: 2%|▏ | 1/50 [00:00<00:00, 96.89 it/sec, feas=True, obj=-2.3]
INFO - 16:23:50: 4%|▍ | 2/50 [00:00<00:00, 59.15 it/sec, feas=True, obj=-2.3]
INFO - 16:23:50: 6%|▌ | 3/50 [00:00<00:00, 75.97 it/sec, feas=True, obj=-2.3]
INFO - 16:23:50: Optimization result:
INFO - 16:23:50: Optimizer info:
INFO - 16:23:50: Status: None
INFO - 16:23:50: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:50: Solution:
INFO - 16:23:50: The solution is feasible.
INFO - 16:23:50: Objective: -2.295629627022848
INFO - 16:23:50: Standardized constraints:
INFO - 16:23:50: g_1 = [-1.59589593e-03 -2.02868890e-03 -1.31333010e-02 -2.32802973e-02
INFO - 16:23:50: -3.14967236e-02 -2.40000000e-01 3.43058915e-14]
INFO - 16:23:50: Design space:
INFO - 16:23:50: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:50: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:50: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:50: | x_1[0] | 0.1 | 0.100000000000082 | 0.4 | float |
INFO - 16:23:50: | x_1[1] | 0.75 | 0.7806436836764953 | 1.25 | float |
INFO - 16:23:50: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:50: *** End StructureScenario execution (time: 0:00:00.041823) ***
INFO - 16:23:50: *** Start PropulsionScenario execution ***
INFO - 16:23:50: PropulsionScenario
INFO - 16:23:50: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:50: MDO formulation: MDF
INFO - 16:23:50: Optimization problem:
INFO - 16:23:50: minimize 0.001*-y_4(x_3)
INFO - 16:23:50: with respect to x_3
INFO - 16:23:50: under the inequality constraints
INFO - 16:23:50: g_3(x_3) <= 0
INFO - 16:23:50: over the design space:
INFO - 16:23:50: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:50: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:50: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:50: | x_3 | 0.1 | 0.1566810472685422 | 1 | float |
INFO - 16:23:50: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:50: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:50: 2%|▏ | 1/50 [00:00<00:00, 92.48 it/sec, feas=True, obj=-2.3]
INFO - 16:23:50: 4%|▍ | 2/50 [00:00<00:00, 64.39 it/sec, feas=True, obj=-2.3]
INFO - 16:23:50: 6%|▌ | 3/50 [00:00<00:00, 85.32 it/sec, feas=True, obj=-2.3]
INFO - 16:23:50: Optimization result:
INFO - 16:23:50: Optimizer info:
INFO - 16:23:50: Status: None
INFO - 16:23:50: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:50: Solution:
INFO - 16:23:50: The solution is feasible.
INFO - 16:23:50: Objective: -2.295629627022848
INFO - 16:23:50: Standardized constraints:
INFO - 16:23:50: g_3 = [-8.43889034e-01 -1.56110966e-01 3.99680289e-15 -1.82842945e-01]
INFO - 16:23:50: Design space:
INFO - 16:23:50: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:50: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:50: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:50: | x_3 | 0.1 | 0.1566810472685422 | 1 | float |
INFO - 16:23:50: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:50: *** End PropulsionScenario execution (time: 0:00:00.037225) ***
INFO - 16:23:50: *** Start AerodynamicsScenario execution ***
INFO - 16:23:50: AerodynamicsScenario
INFO - 16:23:50: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:50: MDO formulation: MDF
INFO - 16:23:50: Optimization problem:
INFO - 16:23:50: minimize 0.001*-y_4(x_2)
INFO - 16:23:50: with respect to x_2
INFO - 16:23:50: under the inequality constraints
INFO - 16:23:50: g_2(x_2) <= 0
INFO - 16:23:50: over the design space:
INFO - 16:23:50: +------+-------------+-------+-------------+-------+
INFO - 16:23:50: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:50: +------+-------------+-------+-------------+-------+
INFO - 16:23:50: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:50: +------+-------------+-------+-------------+-------+
INFO - 16:23:50: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:50: 2%|▏ | 1/50 [00:00<00:00, 80.96 it/sec, feas=True, obj=-2.3]
INFO - 16:23:50: Optimization result:
INFO - 16:23:50: Optimizer info:
INFO - 16:23:50: Status: 8
INFO - 16:23:50: Message: Positive directional derivative for linesearch
INFO - 16:23:50: Solution:
INFO - 16:23:50: The solution is feasible.
INFO - 16:23:50: Objective: -2.295629627022848
INFO - 16:23:50: Standardized constraints:
INFO - 16:23:50: g_2 = 0.0
INFO - 16:23:50: Design space:
INFO - 16:23:50: +------+-------------+-------+-------------+-------+
INFO - 16:23:50: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:50: +------+-------------+-------+-------------+-------+
INFO - 16:23:50: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:50: +------+-------------+-------+-------------+-------+
INFO - 16:23:50: *** End AerodynamicsScenario execution (time: 0:00:00.013806) ***
INFO - 16:23:50: 55%|█████▌ | 55/100 [00:33<00:27, 1.63 it/sec, feas=True, obj=-2.3]
INFO - 16:23:50: *** Start PropulsionScenario execution ***
INFO - 16:23:50: PropulsionScenario
INFO - 16:23:50: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:50: MDO formulation: MDF
INFO - 16:23:50: Optimization problem:
INFO - 16:23:50: minimize 0.001*-y_4(x_3)
INFO - 16:23:50: with respect to x_3
INFO - 16:23:50: under the inequality constraints
INFO - 16:23:50: g_3(x_3) <= 0
INFO - 16:23:50: over the design space:
INFO - 16:23:50: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:50: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:50: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:50: | x_3 | 0.1 | 0.1566810472685422 | 1 | float |
INFO - 16:23:50: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:50: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:50: 2%|▏ | 1/50 [00:00<00:01, 33.79 it/sec, feas=True, obj=-2.18]
INFO - 16:23:50: 4%|▍ | 2/50 [00:00<00:01, 27.56 it/sec, feas=True, obj=-2.19]
INFO - 16:23:50: 6%|▌ | 3/50 [00:00<00:01, 25.93 it/sec, feas=True, obj=-2.19]
INFO - 16:23:50: 8%|▊ | 4/50 [00:00<00:01, 27.95 it/sec, feas=True, obj=-2.19]
INFO - 16:23:50: Optimization result:
INFO - 16:23:50: Optimizer info:
INFO - 16:23:50: Status: None
INFO - 16:23:50: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:50: Solution:
INFO - 16:23:50: The solution is feasible.
INFO - 16:23:50: Objective: -2.1895288906735613
INFO - 16:23:50: Standardized constraints:
INFO - 16:23:50: g_3 = [-8.35729322e-01 -1.64270678e-01 9.32587341e-15 -1.81368883e-01]
INFO - 16:23:50: Design space:
INFO - 16:23:50: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:50: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:50: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:50: | x_3 | 0.1 | 0.1604047542995144 | 1 | float |
INFO - 16:23:50: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:50: *** End PropulsionScenario execution (time: 0:00:00.145701) ***
INFO - 16:23:50: *** Start AerodynamicsScenario execution ***
INFO - 16:23:50: AerodynamicsScenario
INFO - 16:23:50: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:50: MDO formulation: MDF
INFO - 16:23:50: Optimization problem:
INFO - 16:23:50: minimize 0.001*-y_4(x_2)
INFO - 16:23:50: with respect to x_2
INFO - 16:23:50: under the inequality constraints
INFO - 16:23:50: g_2(x_2) <= 0
INFO - 16:23:50: over the design space:
INFO - 16:23:50: +------+-------------+-------+-------------+-------+
INFO - 16:23:50: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:50: +------+-------------+-------+-------------+-------+
INFO - 16:23:50: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:50: +------+-------------+-------+-------------+-------+
INFO - 16:23:50: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:50: 2%|▏ | 1/50 [00:00<00:00, 77.31 it/sec, feas=True, obj=-2.19]
INFO - 16:23:50: Optimization result:
INFO - 16:23:50: Optimizer info:
INFO - 16:23:50: Status: 8
INFO - 16:23:50: Message: Positive directional derivative for linesearch
INFO - 16:23:50: Solution:
INFO - 16:23:50: The solution is feasible.
INFO - 16:23:50: Objective: -2.1895288906735617
INFO - 16:23:50: Standardized constraints:
INFO - 16:23:50: g_2 = -0.0008091653848931735
INFO - 16:23:50: Design space:
INFO - 16:23:50: +------+-------------+-------+-------------+-------+
INFO - 16:23:50: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:50: +------+-------------+-------+-------------+-------+
INFO - 16:23:50: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:50: +------+-------------+-------+-------------+-------+
INFO - 16:23:50: *** End AerodynamicsScenario execution (time: 0:00:00.014664) ***
INFO - 16:23:50: *** Start StructureScenario execution ***
INFO - 16:23:50: StructureScenario
INFO - 16:23:50: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:50: MDO formulation: MDF
INFO - 16:23:50: Optimization problem:
INFO - 16:23:50: minimize 0.001*-y_4(x_1)
INFO - 16:23:50: with respect to x_1
INFO - 16:23:50: under the inequality constraints
INFO - 16:23:50: g_1(x_1) <= 0
INFO - 16:23:50: over the design space:
INFO - 16:23:50: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:50: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:50: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:50: | x_1[0] | 0.1 | 0.100000000000082 | 0.4 | float |
INFO - 16:23:50: | x_1[1] | 0.75 | 0.7806436836764953 | 1.25 | float |
INFO - 16:23:50: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:50: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:50: 2%|▏ | 1/50 [00:00<00:00, 82.82 it/sec, feas=False, obj=-2.19]
INFO - 16:23:50: 4%|▍ | 2/50 [00:00<00:01, 36.84 it/sec, feas=True, obj=-2.18]
INFO - 16:23:50: 6%|▌ | 3/50 [00:00<00:01, 31.35 it/sec, feas=True, obj=-2.18]
WARNING - 16:23:50: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 0.0018314954719615695 is still above the tolerance 1e-06.
INFO - 16:23:50: 8%|▊ | 4/50 [00:00<00:01, 27.66 it/sec, feas=True, obj=-2.18]
INFO - 16:23:50: 10%|█ | 5/50 [00:00<00:01, 29.59 it/sec, feas=True, obj=-2.18]
INFO - 16:23:50: 12%|█▏ | 6/50 [00:00<00:01, 28.60 it/sec, feas=True, obj=-2.18]
INFO - 16:23:50: Optimization result:
INFO - 16:23:50: Optimizer info:
INFO - 16:23:50: Status: None
INFO - 16:23:50: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:50: Solution:
INFO - 16:23:50: The solution is feasible.
INFO - 16:23:50: Objective: -2.1812976229415755
INFO - 16:23:50: Standardized constraints:
INFO - 16:23:50: g_1 = [ 3.48610030e-14 -1.61519666e-03 -1.30670962e-02 -2.33444124e-02
INFO - 16:23:50: -3.16151967e-02 -2.38161984e-01 -1.83801589e-03]
INFO - 16:23:50: Design space:
INFO - 16:23:50: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:50: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:50: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:50: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:50: | x_1[1] | 0.75 | 0.7864642796263814 | 1.25 | float |
INFO - 16:23:50: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:50: *** End StructureScenario execution (time: 0:00:00.212695) ***
INFO - 16:23:50: *** Start PropulsionScenario execution ***
INFO - 16:23:50: PropulsionScenario
INFO - 16:23:50: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:50: MDO formulation: MDF
INFO - 16:23:50: Optimization problem:
INFO - 16:23:50: minimize 0.001*-y_4(x_3)
INFO - 16:23:50: with respect to x_3
INFO - 16:23:50: under the inequality constraints
INFO - 16:23:50: g_3(x_3) <= 0
INFO - 16:23:50: over the design space:
INFO - 16:23:50: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:50: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:50: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:50: | x_3 | 0.1 | 0.1604047542995144 | 1 | float |
INFO - 16:23:50: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:50: Solving optimization problem with algorithm SLSQP:
WARNING - 16:23:50: MDAGaussSeidel has reached its maximum number of unsuccessful iterations, but the normalized residual norm 0.00013449864933217252 is still above the tolerance 1e-06.
INFO - 16:23:51: 2%|▏ | 1/50 [00:00<00:01, 46.49 it/sec, feas=True, obj=-2.18]
INFO - 16:23:51: 4%|▍ | 2/50 [00:00<00:01, 45.40 it/sec, feas=True, obj=-2.18]
INFO - 16:23:51: 6%|▌ | 3/50 [00:00<00:00, 60.74 it/sec, feas=True, obj=-2.18]
INFO - 16:23:51: Optimization result:
INFO - 16:23:51: Optimizer info:
INFO - 16:23:51: Status: None
INFO - 16:23:51: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:51: Solution:
INFO - 16:23:51: The solution is feasible.
INFO - 16:23:51: Objective: -2.181297622941576
INFO - 16:23:51: Standardized constraints:
INFO - 16:23:51: g_3 = [-8.35710653e-01 -1.64289347e-01 9.32587341e-15 -1.81368883e-01]
INFO - 16:23:51: Design space:
INFO - 16:23:51: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:51: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:51: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:51: | x_3 | 0.1 | 0.1604047542995144 | 1 | float |
INFO - 16:23:51: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:51: *** End PropulsionScenario execution (time: 0:00:00.051877) ***
INFO - 16:23:51: *** Start AerodynamicsScenario execution ***
INFO - 16:23:51: AerodynamicsScenario
INFO - 16:23:51: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:51: MDO formulation: MDF
INFO - 16:23:51: Optimization problem:
INFO - 16:23:51: minimize 0.001*-y_4(x_2)
INFO - 16:23:51: with respect to x_2
INFO - 16:23:51: under the inequality constraints
INFO - 16:23:51: g_2(x_2) <= 0
INFO - 16:23:51: over the design space:
INFO - 16:23:51: +------+-------------+-------+-------------+-------+
INFO - 16:23:51: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:51: +------+-------------+-------+-------------+-------+
INFO - 16:23:51: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:51: +------+-------------+-------+-------------+-------+
INFO - 16:23:51: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:51: 2%|▏ | 1/50 [00:00<00:00, 77.33 it/sec, feas=True, obj=-2.18]
INFO - 16:23:51: Optimization result:
INFO - 16:23:51: Optimizer info:
INFO - 16:23:51: Status: 8
INFO - 16:23:51: Message: Positive directional derivative for linesearch
INFO - 16:23:51: Solution:
INFO - 16:23:51: The solution is feasible.
INFO - 16:23:51: Objective: -2.181297622941576
INFO - 16:23:51: Standardized constraints:
INFO - 16:23:51: g_2 = -0.0008091653848931735
INFO - 16:23:51: Design space:
INFO - 16:23:51: +------+-------------+-------+-------------+-------+
INFO - 16:23:51: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:51: +------+-------------+-------+-------------+-------+
INFO - 16:23:51: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:51: +------+-------------+-------+-------------+-------+
INFO - 16:23:51: *** End AerodynamicsScenario execution (time: 0:00:00.014926) ***
INFO - 16:23:51: *** Start StructureScenario execution ***
INFO - 16:23:51: StructureScenario
INFO - 16:23:51: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:51: MDO formulation: MDF
INFO - 16:23:51: Optimization problem:
INFO - 16:23:51: minimize 0.001*-y_4(x_1)
INFO - 16:23:51: with respect to x_1
INFO - 16:23:51: under the inequality constraints
INFO - 16:23:51: g_1(x_1) <= 0
INFO - 16:23:51: over the design space:
INFO - 16:23:51: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:51: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:51: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:51: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:51: | x_1[1] | 0.75 | 0.7864642796263814 | 1.25 | float |
INFO - 16:23:51: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:51: Solving optimization problem with algorithm SLSQP:
WARNING - 16:23:51: MDAGaussSeidel has reached its maximum number of unsuccessful iterations, but the normalized residual norm 0.0018314954719615695 is still above the tolerance 1e-06.
INFO - 16:23:51: 2%|▏ | 1/50 [00:00<00:00, 50.11 it/sec, feas=True, obj=-2.18]
INFO - 16:23:51: Optimization result:
INFO - 16:23:51: Optimizer info:
INFO - 16:23:51: Status: 8
INFO - 16:23:51: Message: Positive directional derivative for linesearch
INFO - 16:23:51: Solution:
INFO - 16:23:51: The solution is feasible.
INFO - 16:23:51: Objective: -2.1812976229415755
INFO - 16:23:51: Standardized constraints:
INFO - 16:23:51: g_1 = [ 3.48610030e-14 -1.61519666e-03 -1.30670962e-02 -2.33444124e-02
INFO - 16:23:51: -3.16151967e-02 -2.38161984e-01 -1.83801589e-03]
INFO - 16:23:51: Design space:
INFO - 16:23:51: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:51: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:51: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:51: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:51: | x_1[1] | 0.75 | 0.7864642796263814 | 1.25 | float |
INFO - 16:23:51: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:51: *** End StructureScenario execution (time: 0:00:00.022236) ***
INFO - 16:23:51: 56%|█████▌ | 56/100 [00:34<00:26, 1.64 it/sec, feas=True, obj=-2.18]
INFO - 16:23:51: *** Start PropulsionScenario execution ***
INFO - 16:23:51: PropulsionScenario
INFO - 16:23:51: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:51: MDO formulation: MDF
INFO - 16:23:51: Optimization problem:
INFO - 16:23:51: minimize 0.001*-y_4(x_3)
INFO - 16:23:51: with respect to x_3
INFO - 16:23:51: under the inequality constraints
INFO - 16:23:51: g_3(x_3) <= 0
INFO - 16:23:51: over the design space:
INFO - 16:23:51: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:51: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:51: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:51: | x_3 | 0.1 | 0.1604047542995144 | 1 | float |
INFO - 16:23:51: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:51: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:51: 2%|▏ | 1/50 [00:00<00:01, 37.61 it/sec, feas=False, obj=-2.3]
INFO - 16:23:51: 4%|▍ | 2/50 [00:00<00:01, 37.84 it/sec, feas=True, obj=-2.3]
INFO - 16:23:51: 6%|▌ | 3/50 [00:00<00:01, 31.28 it/sec, feas=False, obj=-2.3]
INFO - 16:23:51: 8%|▊ | 4/50 [00:00<00:01, 28.73 it/sec, feas=True, obj=-2.3]
INFO - 16:23:51: Optimization result:
INFO - 16:23:51: Optimizer info:
INFO - 16:23:51: Status: 8
INFO - 16:23:51: Message: Positive directional derivative for linesearch
INFO - 16:23:51: Solution:
INFO - 16:23:51: The solution is feasible.
INFO - 16:23:51: Objective: -2.297866047595566
INFO - 16:23:51: Standardized constraints:
INFO - 16:23:51: g_3 = [-8.36171030e-01 -1.63828970e-01 1.33226763e-15 -1.82740552e-01]
INFO - 16:23:51: Design space:
INFO - 16:23:51: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:51: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:51: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:51: | x_3 | 0.1 | 0.1567898210644101 | 1 | float |
INFO - 16:23:51: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:51: *** End PropulsionScenario execution (time: 0:00:00.141763) ***
INFO - 16:23:51: *** Start AerodynamicsScenario execution ***
INFO - 16:23:51: AerodynamicsScenario
INFO - 16:23:51: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:51: MDO formulation: MDF
INFO - 16:23:51: Optimization problem:
INFO - 16:23:51: minimize 0.001*-y_4(x_2)
INFO - 16:23:51: with respect to x_2
INFO - 16:23:51: under the inequality constraints
INFO - 16:23:51: g_2(x_2) <= 0
INFO - 16:23:51: over the design space:
INFO - 16:23:51: +------+-------------+-------+-------------+-------+
INFO - 16:23:51: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:51: +------+-------------+-------+-------------+-------+
INFO - 16:23:51: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:51: +------+-------------+-------+-------------+-------+
INFO - 16:23:51: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:51: 2%|▏ | 1/50 [00:00<00:00, 73.64 it/sec, feas=True, obj=-2.3]
INFO - 16:23:51: Optimization result:
INFO - 16:23:51: Optimizer info:
INFO - 16:23:51: Status: 8
INFO - 16:23:51: Message: Positive directional derivative for linesearch
INFO - 16:23:51: Solution:
INFO - 16:23:51: The solution is feasible.
INFO - 16:23:51: Objective: -2.297866047595566
INFO - 16:23:51: Standardized constraints:
INFO - 16:23:51: g_2 = 0.0
INFO - 16:23:51: Design space:
INFO - 16:23:51: +------+-------------+-------+-------------+-------+
INFO - 16:23:51: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:51: +------+-------------+-------+-------------+-------+
INFO - 16:23:51: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:51: +------+-------------+-------+-------------+-------+
INFO - 16:23:51: *** End AerodynamicsScenario execution (time: 0:00:00.015535) ***
INFO - 16:23:51: *** Start StructureScenario execution ***
INFO - 16:23:51: StructureScenario
INFO - 16:23:51: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:51: MDO formulation: MDF
INFO - 16:23:51: Optimization problem:
INFO - 16:23:51: minimize 0.001*-y_4(x_1)
INFO - 16:23:51: with respect to x_1
INFO - 16:23:51: under the inequality constraints
INFO - 16:23:51: g_1(x_1) <= 0
INFO - 16:23:51: over the design space:
INFO - 16:23:51: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:51: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:51: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:51: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:51: | x_1[1] | 0.75 | 0.7864642796263814 | 1.25 | float |
INFO - 16:23:51: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:51: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:51: 2%|▏ | 1/50 [00:00<00:00, 92.81 it/sec, feas=True, obj=-2.3]
INFO - 16:23:51: 4%|▍ | 2/50 [00:00<00:01, 36.75 it/sec, feas=True, obj=-2.31]
INFO - 16:23:51: 6%|▌ | 3/50 [00:00<00:01, 31.17 it/sec, feas=True, obj=-2.31]
INFO - 16:23:51: 8%|▊ | 4/50 [00:00<00:01, 28.86 it/sec, feas=True, obj=-2.31]
WARNING - 16:23:51: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 0.0009157477359807847 is still above the tolerance 1e-06.
INFO - 16:23:51: 10%|█ | 5/50 [00:00<00:01, 26.57 it/sec, feas=True, obj=-2.31]
INFO - 16:23:51: Optimization result:
INFO - 16:23:51: Optimizer info:
INFO - 16:23:51: Status: 8
INFO - 16:23:51: Message: Positive directional derivative for linesearch
INFO - 16:23:51: Solution:
INFO - 16:23:51: The solution is feasible.
INFO - 16:23:51: Objective: -2.306618792673027
INFO - 16:23:51: Standardized constraints:
INFO - 16:23:51: g_1 = [-1.59589593e-03 -2.02868890e-03 -1.31333010e-02 -2.32802973e-02
INFO - 16:23:51: -3.14967236e-02 -2.40000000e-01 1.36557432e-14]
INFO - 16:23:51: Design space:
INFO - 16:23:51: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:51: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:51: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:51: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:51: | x_1[1] | 0.75 | 0.7806436836764827 | 1.25 | float |
INFO - 16:23:51: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:51: *** End StructureScenario execution (time: 0:00:00.190881) ***
INFO - 16:23:51: *** Start PropulsionScenario execution ***
INFO - 16:23:51: PropulsionScenario
INFO - 16:23:51: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:51: MDO formulation: MDF
INFO - 16:23:51: Optimization problem:
INFO - 16:23:51: minimize 0.001*-y_4(x_3)
INFO - 16:23:51: with respect to x_3
INFO - 16:23:51: under the inequality constraints
INFO - 16:23:51: g_3(x_3) <= 0
INFO - 16:23:51: over the design space:
INFO - 16:23:51: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:51: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:51: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:51: | x_3 | 0.1 | 0.1567898210644101 | 1 | float |
INFO - 16:23:51: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:51: Solving optimization problem with algorithm SLSQP:
WARNING - 16:23:51: MDAGaussSeidel has reached its maximum number of unsuccessful iterations, but the normalized residual norm 6.724932466608626e-05 is still above the tolerance 1e-06.
INFO - 16:23:51: 2%|▏ | 1/50 [00:00<00:00, 50.88 it/sec, feas=True, obj=-2.31]
INFO - 16:23:51: 4%|▍ | 2/50 [00:00<00:00, 80.25 it/sec, feas=True, obj=-2.31]
INFO - 16:23:51: 6%|▌ | 3/50 [00:00<00:00, 62.73 it/sec, feas=True, obj=-2.31]
INFO - 16:23:51: Optimization result:
INFO - 16:23:51: Optimizer info:
INFO - 16:23:51: Status: None
INFO - 16:23:51: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:51: Solution:
INFO - 16:23:51: The solution is feasible.
INFO - 16:23:51: Objective: -2.306618792673029
INFO - 16:23:51: Standardized constraints:
INFO - 16:23:51: g_3 = [-8.36190321e-01 -1.63809679e-01 7.99360578e-15 -1.82740552e-01]
INFO - 16:23:51: Design space:
INFO - 16:23:51: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:51: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:51: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:51: | x_3 | 0.1 | 0.1567898210644111 | 1 | float |
INFO - 16:23:51: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:51: *** End PropulsionScenario execution (time: 0:00:00.050606) ***
INFO - 16:23:51: *** Start AerodynamicsScenario execution ***
INFO - 16:23:51: AerodynamicsScenario
INFO - 16:23:51: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:51: MDO formulation: MDF
INFO - 16:23:51: Optimization problem:
INFO - 16:23:51: minimize 0.001*-y_4(x_2)
INFO - 16:23:51: with respect to x_2
INFO - 16:23:51: under the inequality constraints
INFO - 16:23:51: g_2(x_2) <= 0
INFO - 16:23:51: over the design space:
INFO - 16:23:51: +------+-------------+-------+-------------+-------+
INFO - 16:23:51: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:51: +------+-------------+-------+-------------+-------+
INFO - 16:23:51: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:51: +------+-------------+-------+-------------+-------+
INFO - 16:23:51: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:51: 2%|▏ | 1/50 [00:00<00:00, 75.70 it/sec, feas=True, obj=-2.31]
INFO - 16:23:51: Optimization result:
INFO - 16:23:51: Optimizer info:
INFO - 16:23:51: Status: 8
INFO - 16:23:51: Message: Positive directional derivative for linesearch
INFO - 16:23:51: Solution:
INFO - 16:23:51: The solution is feasible.
INFO - 16:23:51: Objective: -2.306618792673029
INFO - 16:23:51: Standardized constraints:
INFO - 16:23:51: g_2 = 0.0
INFO - 16:23:51: Design space:
INFO - 16:23:51: +------+-------------+-------+-------------+-------+
INFO - 16:23:51: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:51: +------+-------------+-------+-------------+-------+
INFO - 16:23:51: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:51: +------+-------------+-------+-------------+-------+
INFO - 16:23:51: *** End AerodynamicsScenario execution (time: 0:00:00.015112) ***
INFO - 16:23:51: *** Start StructureScenario execution ***
INFO - 16:23:51: StructureScenario
INFO - 16:23:51: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:51: MDO formulation: MDF
INFO - 16:23:51: Optimization problem:
INFO - 16:23:51: minimize 0.001*-y_4(x_1)
INFO - 16:23:51: with respect to x_1
INFO - 16:23:51: under the inequality constraints
INFO - 16:23:51: g_1(x_1) <= 0
INFO - 16:23:51: over the design space:
INFO - 16:23:51: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:51: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:51: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:51: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:51: | x_1[1] | 0.75 | 0.7806436836764827 | 1.25 | float |
INFO - 16:23:51: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:51: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:51: 2%|▏ | 1/50 [00:00<00:00, 95.15 it/sec, feas=True, obj=-2.31]
INFO - 16:23:51: Optimization result:
INFO - 16:23:51: Optimizer info:
INFO - 16:23:51: Status: 8
INFO - 16:23:51: Message: Positive directional derivative for linesearch
INFO - 16:23:51: Solution:
INFO - 16:23:51: The solution is feasible.
INFO - 16:23:51: Objective: -2.306618792673029
INFO - 16:23:51: Standardized constraints:
INFO - 16:23:51: g_1 = [-1.59589593e-03 -2.02868890e-03 -1.31333010e-02 -2.32802973e-02
INFO - 16:23:51: -3.14967236e-02 -2.40000000e-01 1.36557432e-14]
INFO - 16:23:51: Design space:
INFO - 16:23:51: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:51: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:51: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:51: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:51: | x_1[1] | 0.75 | 0.7806436836764827 | 1.25 | float |
INFO - 16:23:51: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:51: *** End StructureScenario execution (time: 0:00:00.012825) ***
INFO - 16:23:51: 57%|█████▋ | 57/100 [00:34<00:26, 1.64 it/sec, feas=True, obj=-2.31]
INFO - 16:23:51: *** Start PropulsionScenario execution ***
INFO - 16:23:51: PropulsionScenario
INFO - 16:23:51: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:51: MDO formulation: MDF
INFO - 16:23:51: Optimization problem:
INFO - 16:23:51: minimize 0.001*-y_4(x_3)
INFO - 16:23:51: with respect to x_3
INFO - 16:23:51: under the inequality constraints
INFO - 16:23:51: g_3(x_3) <= 0
INFO - 16:23:51: over the design space:
INFO - 16:23:51: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:51: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:51: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:51: | x_3 | 0.1 | 0.1567898210644111 | 1 | float |
INFO - 16:23:51: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:51: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:51: 2%|▏ | 1/50 [00:00<00:01, 37.54 it/sec, feas=True, obj=-2.27]
INFO - 16:23:51: 4%|▍ | 2/50 [00:00<00:01, 27.73 it/sec, feas=True, obj=-2.27]
INFO - 16:23:51: 6%|▌ | 3/50 [00:00<00:01, 26.35 it/sec, feas=True, obj=-2.27]
INFO - 16:23:51: 8%|▊ | 4/50 [00:00<00:01, 25.84 it/sec, feas=True, obj=-2.27]
INFO - 16:23:51: Optimization result:
INFO - 16:23:51: Optimizer info:
INFO - 16:23:51: Status: 8
INFO - 16:23:51: Message: Positive directional derivative for linesearch
INFO - 16:23:51: Solution:
INFO - 16:23:51: The solution is feasible.
INFO - 16:23:51: Objective: -2.268142975799454
INFO - 16:23:51: Standardized constraints:
INFO - 16:23:51: g_3 = [-0.84127114 -0.15872886 0. -0.18194472]
INFO - 16:23:51: Design space:
INFO - 16:23:51: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:51: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:51: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:51: | x_3 | 0.1 | 0.1576400211914478 | 1 | float |
INFO - 16:23:51: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:51: *** End PropulsionScenario execution (time: 0:00:00.157293) ***
INFO - 16:23:51: *** Start AerodynamicsScenario execution ***
INFO - 16:23:51: AerodynamicsScenario
INFO - 16:23:51: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:51: MDO formulation: MDF
INFO - 16:23:51: Optimization problem:
INFO - 16:23:51: minimize 0.001*-y_4(x_2)
INFO - 16:23:51: with respect to x_2
INFO - 16:23:51: under the inequality constraints
INFO - 16:23:51: g_2(x_2) <= 0
INFO - 16:23:51: over the design space:
INFO - 16:23:51: +------+-------------+-------+-------------+-------+
INFO - 16:23:51: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:51: +------+-------------+-------+-------------+-------+
INFO - 16:23:51: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:51: +------+-------------+-------+-------------+-------+
INFO - 16:23:51: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:51: 2%|▏ | 1/50 [00:00<00:00, 104.10 it/sec, feas=True, obj=-2.27]
INFO - 16:23:51: Optimization result:
INFO - 16:23:51: Optimizer info:
INFO - 16:23:51: Status: 8
INFO - 16:23:51: Message: Positive directional derivative for linesearch
INFO - 16:23:51: Solution:
INFO - 16:23:51: The solution is feasible.
INFO - 16:23:51: Objective: -2.268142975799454
INFO - 16:23:51: Standardized constraints:
INFO - 16:23:51: g_2 = 0.0
INFO - 16:23:51: Design space:
INFO - 16:23:51: +------+-------------+-------+-------------+-------+
INFO - 16:23:51: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:51: +------+-------------+-------+-------------+-------+
INFO - 16:23:51: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:51: +------+-------------+-------+-------------+-------+
INFO - 16:23:51: *** End AerodynamicsScenario execution (time: 0:00:00.011320) ***
INFO - 16:23:51: *** Start StructureScenario execution ***
INFO - 16:23:51: StructureScenario
INFO - 16:23:51: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:51: MDO formulation: MDF
INFO - 16:23:51: Optimization problem:
INFO - 16:23:51: minimize 0.001*-y_4(x_1)
INFO - 16:23:51: with respect to x_1
INFO - 16:23:51: under the inequality constraints
INFO - 16:23:51: g_1(x_1) <= 0
INFO - 16:23:51: over the design space:
INFO - 16:23:51: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:51: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:51: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:51: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:51: | x_1[1] | 0.75 | 0.7806436836764827 | 1.25 | float |
INFO - 16:23:51: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:51: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:51: 2%|▏ | 1/50 [00:00<00:00, 97.41 it/sec, feas=True, obj=-2.27]
INFO - 16:23:51: Optimization result:
INFO - 16:23:51: Optimizer info:
INFO - 16:23:51: Status: 8
INFO - 16:23:51: Message: Positive directional derivative for linesearch
INFO - 16:23:51: Solution:
INFO - 16:23:51: The solution is feasible.
INFO - 16:23:51: Objective: -2.268142975799454
INFO - 16:23:51: Standardized constraints:
INFO - 16:23:51: g_1 = [-1.59589593e-03 -2.02868890e-03 -1.31333010e-02 -2.32802973e-02
INFO - 16:23:51: -3.14967236e-02 -2.40000000e-01 1.36557432e-14]
INFO - 16:23:51: Design space:
INFO - 16:23:51: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:51: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:51: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:51: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:51: | x_1[1] | 0.75 | 0.7806436836764827 | 1.25 | float |
INFO - 16:23:51: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:51: *** End StructureScenario execution (time: 0:00:00.012409) ***
INFO - 16:23:51: *** Start PropulsionScenario execution ***
INFO - 16:23:51: PropulsionScenario
INFO - 16:23:51: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:51: MDO formulation: MDF
INFO - 16:23:51: Optimization problem:
INFO - 16:23:51: minimize 0.001*-y_4(x_3)
INFO - 16:23:51: with respect to x_3
INFO - 16:23:51: under the inequality constraints
INFO - 16:23:51: g_3(x_3) <= 0
INFO - 16:23:51: over the design space:
INFO - 16:23:51: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:51: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:51: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:51: | x_3 | 0.1 | 0.1576400211914478 | 1 | float |
INFO - 16:23:51: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:51: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:51: 2%|▏ | 1/50 [00:00<00:00, 109.33 it/sec, feas=True, obj=-2.27]
INFO - 16:23:51: Optimization result:
INFO - 16:23:51: Optimizer info:
INFO - 16:23:51: Status: 8
INFO - 16:23:51: Message: Positive directional derivative for linesearch
INFO - 16:23:51: Solution:
INFO - 16:23:51: The solution is feasible.
INFO - 16:23:51: Objective: -2.268142975799454
INFO - 16:23:51: Standardized constraints:
INFO - 16:23:51: g_3 = [-0.84127114 -0.15872886 0. -0.18194472]
INFO - 16:23:51: Design space:
INFO - 16:23:51: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:51: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:51: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:51: | x_3 | 0.1 | 0.1576400211914478 | 1 | float |
INFO - 16:23:51: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:51: *** End PropulsionScenario execution (time: 0:00:00.011054) ***
INFO - 16:23:51: 58%|█████▊ | 58/100 [00:34<00:25, 1.66 it/sec, feas=True, obj=-2.27]
INFO - 16:23:51: *** Start PropulsionScenario execution ***
INFO - 16:23:51: PropulsionScenario
INFO - 16:23:51: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:51: MDO formulation: MDF
INFO - 16:23:51: Optimization problem:
INFO - 16:23:51: minimize 0.001*-y_4(x_3)
INFO - 16:23:51: with respect to x_3
INFO - 16:23:51: under the inequality constraints
INFO - 16:23:51: g_3(x_3) <= 0
INFO - 16:23:51: over the design space:
INFO - 16:23:51: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:51: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:51: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:51: | x_3 | 0.1 | 0.1576400211914478 | 1 | float |
INFO - 16:23:51: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:51: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:51: 2%|▏ | 1/50 [00:00<00:01, 38.42 it/sec, feas=True, obj=-2.24]
INFO - 16:23:51: 4%|▍ | 2/50 [00:00<00:01, 29.64 it/sec, feas=True, obj=-2.24]
INFO - 16:23:51: 6%|▌ | 3/50 [00:00<00:01, 27.35 it/sec, feas=True, obj=-2.24]
INFO - 16:23:51: Optimization result:
INFO - 16:23:51: Optimizer info:
INFO - 16:23:51: Status: 8
INFO - 16:23:51: Message: Positive directional derivative for linesearch
INFO - 16:23:51: Solution:
INFO - 16:23:51: The solution is feasible.
INFO - 16:23:51: Objective: -2.2401866190499358
INFO - 16:23:51: Standardized constraints:
INFO - 16:23:51: g_3 = [-8.34388668e-01 -1.65611332e-01 5.32907052e-15 -1.81384371e-01]
INFO - 16:23:51: Design space:
INFO - 16:23:51: +------+-------------+-------------------+-------------+-------+
INFO - 16:23:51: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:51: +------+-------------+-------------------+-------------+-------+
INFO - 16:23:51: | x_3 | 0.1 | 0.158290059413496 | 1 | float |
INFO - 16:23:51: +------+-------------+-------------------+-------------+-------+
INFO - 16:23:51: *** End PropulsionScenario execution (time: 0:00:00.111838) ***
INFO - 16:23:51: *** Start AerodynamicsScenario execution ***
INFO - 16:23:51: AerodynamicsScenario
INFO - 16:23:51: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:51: MDO formulation: MDF
INFO - 16:23:51: Optimization problem:
INFO - 16:23:51: minimize 0.001*-y_4(x_2)
INFO - 16:23:51: with respect to x_2
INFO - 16:23:51: under the inequality constraints
INFO - 16:23:51: g_2(x_2) <= 0
INFO - 16:23:51: over the design space:
INFO - 16:23:51: +------+-------------+-------+-------------+-------+
INFO - 16:23:51: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:51: +------+-------------+-------+-------------+-------+
INFO - 16:23:51: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:51: +------+-------------+-------+-------------+-------+
INFO - 16:23:51: Solving optimization problem with algorithm SLSQP:
WARNING - 16:23:51: Optimization found no feasible point; the least infeasible point is selected.
INFO - 16:23:51: 2%|▏ | 1/50 [00:00<00:00, 74.23 it/sec, feas=False, obj=-2.24]
INFO - 16:23:51: Optimization result:
INFO - 16:23:51: Optimizer info:
INFO - 16:23:51: Status: 8
INFO - 16:23:51: Message: Positive directional derivative for linesearch
INFO - 16:23:51: Solution:
WARNING - 16:23:51: The solution is not feasible.
INFO - 16:23:51: Objective: -2.2401866190499358
INFO - 16:23:51: Standardized constraints:
INFO - 16:23:51: g_2 = 0.00022173473151521073
INFO - 16:23:51: Design space:
INFO - 16:23:51: +------+-------------+-------+-------------+-------+
INFO - 16:23:51: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:51: +------+-------------+-------+-------------+-------+
INFO - 16:23:51: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:51: +------+-------------+-------+-------------+-------+
INFO - 16:23:51: *** End AerodynamicsScenario execution (time: 0:00:00.015241) ***
INFO - 16:23:51: *** Start StructureScenario execution ***
INFO - 16:23:51: StructureScenario
INFO - 16:23:51: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:51: MDO formulation: MDF
INFO - 16:23:51: Optimization problem:
INFO - 16:23:51: minimize 0.001*-y_4(x_1)
INFO - 16:23:51: with respect to x_1
INFO - 16:23:51: under the inequality constraints
INFO - 16:23:51: g_1(x_1) <= 0
INFO - 16:23:51: over the design space:
INFO - 16:23:51: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:51: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:51: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:51: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:51: | x_1[1] | 0.75 | 0.7806436836764827 | 1.25 | float |
INFO - 16:23:51: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:51: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:51: 2%|▏ | 1/50 [00:00<00:00, 96.38 it/sec, feas=True, obj=-2.24]
INFO - 16:23:51: 4%|▍ | 2/50 [00:00<00:00, 105.38 it/sec, feas=True, obj=-2.24]
INFO - 16:23:51: 6%|▌ | 3/50 [00:00<00:00, 114.81 it/sec, feas=True, obj=-2.24]
INFO - 16:23:51: Optimization result:
INFO - 16:23:51: Optimizer info:
INFO - 16:23:51: Status: None
INFO - 16:23:51: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:51: Solution:
INFO - 16:23:51: The solution is feasible.
INFO - 16:23:51: Objective: -2.2401866190499358
INFO - 16:23:51: Standardized constraints:
INFO - 16:23:51: g_1 = [-3.37438126e-03 -3.00390577e-03 -1.37857987e-02 -2.37644162e-02
INFO - 16:23:51: -3.18791120e-02 -2.40000000e-01 1.36557432e-14]
INFO - 16:23:51: Design space:
INFO - 16:23:51: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:51: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:51: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:51: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:51: | x_1[1] | 0.75 | 0.7806436836764827 | 1.25 | float |
INFO - 16:23:51: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:51: *** End StructureScenario execution (time: 0:00:00.028667) ***
INFO - 16:23:51: *** Start PropulsionScenario execution ***
INFO - 16:23:51: PropulsionScenario
INFO - 16:23:51: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:51: MDO formulation: MDF
INFO - 16:23:51: Optimization problem:
INFO - 16:23:51: minimize 0.001*-y_4(x_3)
INFO - 16:23:51: with respect to x_3
INFO - 16:23:51: under the inequality constraints
INFO - 16:23:51: g_3(x_3) <= 0
INFO - 16:23:51: over the design space:
INFO - 16:23:51: +------+-------------+-------------------+-------------+-------+
INFO - 16:23:51: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:51: +------+-------------+-------------------+-------------+-------+
INFO - 16:23:51: | x_3 | 0.1 | 0.158290059413496 | 1 | float |
INFO - 16:23:51: +------+-------------+-------------------+-------------+-------+
INFO - 16:23:51: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:51: 2%|▏ | 1/50 [00:00<00:00, 90.16 it/sec, feas=True, obj=-2.24]
INFO - 16:23:51: 4%|▍ | 2/50 [00:00<00:00, 63.08 it/sec, feas=True, obj=-2.24]
INFO - 16:23:51: Optimization result:
INFO - 16:23:51: Optimizer info:
INFO - 16:23:51: Status: 8
INFO - 16:23:51: Message: Positive directional derivative for linesearch
INFO - 16:23:51: Solution:
INFO - 16:23:51: The solution is feasible.
INFO - 16:23:51: Objective: -2.2401866190499358
INFO - 16:23:51: Standardized constraints:
INFO - 16:23:51: g_3 = [-8.34388668e-01 -1.65611332e-01 5.32907052e-15 -1.81384371e-01]
INFO - 16:23:51: Design space:
INFO - 16:23:51: +------+-------------+-------------------+-------------+-------+
INFO - 16:23:51: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:51: +------+-------------+-------------------+-------------+-------+
INFO - 16:23:51: | x_3 | 0.1 | 0.158290059413496 | 1 | float |
INFO - 16:23:51: +------+-------------+-------------------+-------------+-------+
INFO - 16:23:51: *** End PropulsionScenario execution (time: 0:00:00.033685) ***
INFO - 16:23:52: 59%|█████▉ | 59/100 [00:35<00:24, 1.68 it/sec, feas=False, obj=-2.24]
INFO - 16:23:52: *** Start PropulsionScenario execution ***
INFO - 16:23:52: PropulsionScenario
INFO - 16:23:52: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:52: MDO formulation: MDF
INFO - 16:23:52: Optimization problem:
INFO - 16:23:52: minimize 0.001*-y_4(x_3)
INFO - 16:23:52: with respect to x_3
INFO - 16:23:52: under the inequality constraints
INFO - 16:23:52: g_3(x_3) <= 0
INFO - 16:23:52: over the design space:
INFO - 16:23:52: +------+-------------+-------------------+-------------+-------+
INFO - 16:23:52: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:52: +------+-------------+-------------------+-------------+-------+
INFO - 16:23:52: | x_3 | 0.1 | 0.158290059413496 | 1 | float |
INFO - 16:23:52: +------+-------------+-------------------+-------------+-------+
INFO - 16:23:52: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:52: 2%|▏ | 1/50 [00:00<00:01, 38.34 it/sec, feas=False, obj=-2.27]
WARNING - 16:23:52: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 6.855020582101965e-05 is still above the tolerance 1e-06.
INFO - 16:23:52: 4%|▍ | 2/50 [00:00<00:01, 34.98 it/sec, feas=True, obj=-2.27]
INFO - 16:23:52: 6%|▌ | 3/50 [00:00<00:01, 30.22 it/sec, feas=False, obj=-2.27]
INFO - 16:23:52: 8%|▊ | 4/50 [00:00<00:01, 27.92 it/sec, feas=True, obj=-2.27]
INFO - 16:23:52: Optimization result:
INFO - 16:23:52: Optimizer info:
INFO - 16:23:52: Status: 8
INFO - 16:23:52: Message: Positive directional derivative for linesearch
INFO - 16:23:52: Solution:
INFO - 16:23:52: The solution is feasible.
INFO - 16:23:52: Objective: -2.269967791039084
INFO - 16:23:52: Standardized constraints:
INFO - 16:23:52: g_3 = [-8.38942877e-01 -1.61057123e-01 2.22044605e-16 -1.81772493e-01]
INFO - 16:23:52: Design space:
INFO - 16:23:52: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:52: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:52: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:52: | x_3 | 0.1 | 0.1578251204827684 | 1 | float |
INFO - 16:23:52: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:52: *** End PropulsionScenario execution (time: 0:00:00.145216) ***
INFO - 16:23:52: *** Start AerodynamicsScenario execution ***
INFO - 16:23:52: AerodynamicsScenario
INFO - 16:23:52: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:52: MDO formulation: MDF
INFO - 16:23:52: Optimization problem:
INFO - 16:23:52: minimize 0.001*-y_4(x_2)
INFO - 16:23:52: with respect to x_2
INFO - 16:23:52: under the inequality constraints
INFO - 16:23:52: g_2(x_2) <= 0
INFO - 16:23:52: over the design space:
INFO - 16:23:52: +------+-------------+-------+-------------+-------+
INFO - 16:23:52: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:52: +------+-------------+-------+-------------+-------+
INFO - 16:23:52: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:52: +------+-------------+-------+-------------+-------+
INFO - 16:23:52: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:52: 2%|▏ | 1/50 [00:00<00:00, 104.75 it/sec, feas=True, obj=-2.27]
INFO - 16:23:52: Optimization result:
INFO - 16:23:52: Optimizer info:
INFO - 16:23:52: Status: 8
INFO - 16:23:52: Message: Positive directional derivative for linesearch
INFO - 16:23:52: Solution:
INFO - 16:23:52: The solution is feasible.
INFO - 16:23:52: Objective: -2.269967791039084
INFO - 16:23:52: Standardized constraints:
INFO - 16:23:52: g_2 = -0.00019914737330339882
INFO - 16:23:52: Design space:
INFO - 16:23:52: +------+-------------+-------+-------------+-------+
INFO - 16:23:52: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:52: +------+-------------+-------+-------------+-------+
INFO - 16:23:52: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:52: +------+-------------+-------+-------------+-------+
INFO - 16:23:52: *** End AerodynamicsScenario execution (time: 0:00:00.011349) ***
INFO - 16:23:52: *** Start StructureScenario execution ***
INFO - 16:23:52: StructureScenario
INFO - 16:23:52: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:52: MDO formulation: MDF
INFO - 16:23:52: Optimization problem:
INFO - 16:23:52: minimize 0.001*-y_4(x_1)
INFO - 16:23:52: with respect to x_1
INFO - 16:23:52: under the inequality constraints
INFO - 16:23:52: g_1(x_1) <= 0
INFO - 16:23:52: over the design space:
INFO - 16:23:52: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:52: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:52: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:52: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:52: | x_1[1] | 0.75 | 0.7806436836764827 | 1.25 | float |
INFO - 16:23:52: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:52: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:52: 2%|▏ | 1/50 [00:00<00:00, 97.18 it/sec, feas=True, obj=-2.27]
INFO - 16:23:52: 4%|▍ | 2/50 [00:00<00:00, 115.84 it/sec, feas=True, obj=-2.27]
INFO - 16:23:52: 6%|▌ | 3/50 [00:00<00:00, 131.13 it/sec, feas=True, obj=-2.27]
INFO - 16:23:52: Optimization result:
INFO - 16:23:52: Optimizer info:
INFO - 16:23:52: Status: None
INFO - 16:23:52: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:52: Solution:
INFO - 16:23:52: The solution is feasible.
INFO - 16:23:52: Objective: -2.269967791039084
INFO - 16:23:52: Standardized constraints:
INFO - 16:23:52: g_1 = [-1.19810507e-06 -1.15397817e-03 -1.25479259e-02 -2.28459130e-02
INFO - 16:23:52: -3.11535788e-02 -2.40000000e-01 1.36557432e-14]
INFO - 16:23:52: Design space:
INFO - 16:23:52: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:52: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:52: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:52: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:52: | x_1[1] | 0.75 | 0.7806436836764827 | 1.25 | float |
INFO - 16:23:52: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:52: *** End StructureScenario execution (time: 0:00:00.025346) ***
INFO - 16:23:52: *** Start PropulsionScenario execution ***
INFO - 16:23:52: PropulsionScenario
INFO - 16:23:52: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:52: MDO formulation: MDF
INFO - 16:23:52: Optimization problem:
INFO - 16:23:52: minimize 0.001*-y_4(x_3)
INFO - 16:23:52: with respect to x_3
INFO - 16:23:52: under the inequality constraints
INFO - 16:23:52: g_3(x_3) <= 0
INFO - 16:23:52: over the design space:
INFO - 16:23:52: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:52: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:52: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:52: | x_3 | 0.1 | 0.1578251204827684 | 1 | float |
INFO - 16:23:52: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:52: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:52: 2%|▏ | 1/50 [00:00<00:00, 62.19 it/sec, feas=True, obj=-2.27]
INFO - 16:23:52: Optimization result:
INFO - 16:23:52: Optimizer info:
INFO - 16:23:52: Status: 8
INFO - 16:23:52: Message: Positive directional derivative for linesearch
INFO - 16:23:52: Solution:
INFO - 16:23:52: The solution is feasible.
INFO - 16:23:52: Objective: -2.269967791039084
INFO - 16:23:52: Standardized constraints:
INFO - 16:23:52: g_3 = [-8.38942877e-01 -1.61057123e-01 2.22044605e-16 -1.81772493e-01]
INFO - 16:23:52: Design space:
INFO - 16:23:52: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:52: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:52: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:52: | x_3 | 0.1 | 0.1578251204827684 | 1 | float |
INFO - 16:23:52: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:52: *** End PropulsionScenario execution (time: 0:00:00.017935) ***
INFO - 16:23:52: 60%|██████ | 60/100 [00:35<00:23, 1.70 it/sec, feas=True, obj=-2.27]
INFO - 16:23:52: *** Start PropulsionScenario execution ***
INFO - 16:23:52: PropulsionScenario
INFO - 16:23:52: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:52: MDO formulation: MDF
INFO - 16:23:52: Optimization problem:
INFO - 16:23:52: minimize 0.001*-y_4(x_3)
INFO - 16:23:52: with respect to x_3
INFO - 16:23:52: under the inequality constraints
INFO - 16:23:52: g_3(x_3) <= 0
INFO - 16:23:52: over the design space:
INFO - 16:23:52: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:52: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:52: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:52: | x_3 | 0.1 | 0.1578251204827684 | 1 | float |
INFO - 16:23:52: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:52: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:52: 2%|▏ | 1/50 [00:00<00:01, 38.79 it/sec, feas=True, obj=-2.25]
INFO - 16:23:52: 4%|▍ | 2/50 [00:00<00:01, 29.53 it/sec, feas=True, obj=-2.25]
INFO - 16:23:52: 6%|▌ | 3/50 [00:00<00:01, 31.55 it/sec, feas=True, obj=-2.25]
INFO - 16:23:52: 8%|▊ | 4/50 [00:00<00:01, 32.88 it/sec, feas=True, obj=-2.25]
INFO - 16:23:52: Optimization result:
INFO - 16:23:52: Optimizer info:
INFO - 16:23:52: Status: None
INFO - 16:23:52: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:52: Solution:
INFO - 16:23:52: The solution is feasible.
INFO - 16:23:52: Objective: -2.253375612107262
INFO - 16:23:52: Standardized constraints:
INFO - 16:23:52: g_3 = [-8.34884797e-01 -1.65115203e-01 -1.99840144e-15 -1.81426541e-01]
INFO - 16:23:52: Design space:
INFO - 16:23:52: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:52: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:52: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:52: | x_3 | 0.1 | 0.1582037082879361 | 1 | float |
INFO - 16:23:52: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:52: *** End PropulsionScenario execution (time: 0:00:00.124128) ***
INFO - 16:23:52: *** Start AerodynamicsScenario execution ***
INFO - 16:23:52: AerodynamicsScenario
INFO - 16:23:52: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:52: MDO formulation: MDF
INFO - 16:23:52: Optimization problem:
INFO - 16:23:52: minimize 0.001*-y_4(x_2)
INFO - 16:23:52: with respect to x_2
INFO - 16:23:52: under the inequality constraints
INFO - 16:23:52: g_2(x_2) <= 0
INFO - 16:23:52: over the design space:
INFO - 16:23:52: +------+-------------+-------+-------------+-------+
INFO - 16:23:52: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:52: +------+-------------+-------+-------------+-------+
INFO - 16:23:52: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:52: +------+-------------+-------+-------------+-------+
INFO - 16:23:52: Solving optimization problem with algorithm SLSQP:
WARNING - 16:23:52: Optimization found no feasible point; the least infeasible point is selected.
INFO - 16:23:52: 2%|▏ | 1/50 [00:00<00:00, 78.49 it/sec, feas=False, obj=-2.25]
INFO - 16:23:52: Optimization result:
INFO - 16:23:52: Optimizer info:
INFO - 16:23:52: Status: 8
INFO - 16:23:52: Message: Positive directional derivative for linesearch
INFO - 16:23:52: Solution:
WARNING - 16:23:52: The solution is not feasible.
INFO - 16:23:52: Objective: -2.253375612107262
INFO - 16:23:52: Standardized constraints:
INFO - 16:23:52: g_2 = 0.0015281661390051937
INFO - 16:23:52: Design space:
INFO - 16:23:52: +------+-------------+-------+-------------+-------+
INFO - 16:23:52: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:52: +------+-------------+-------+-------------+-------+
INFO - 16:23:52: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:52: +------+-------------+-------+-------------+-------+
INFO - 16:23:52: *** End AerodynamicsScenario execution (time: 0:00:00.014651) ***
INFO - 16:23:52: *** Start StructureScenario execution ***
INFO - 16:23:52: StructureScenario
INFO - 16:23:52: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:52: MDO formulation: MDF
INFO - 16:23:52: Optimization problem:
INFO - 16:23:52: minimize 0.001*-y_4(x_1)
INFO - 16:23:52: with respect to x_1
INFO - 16:23:52: under the inequality constraints
INFO - 16:23:52: g_1(x_1) <= 0
INFO - 16:23:52: over the design space:
INFO - 16:23:52: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:52: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:52: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:52: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:52: | x_1[1] | 0.75 | 0.7806436836764827 | 1.25 | float |
INFO - 16:23:52: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:52: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:52: 2%|▏ | 1/50 [00:00<00:00, 93.49 it/sec, feas=True, obj=-2.25]
INFO - 16:23:52: Optimization result:
INFO - 16:23:52: Optimizer info:
INFO - 16:23:52: Status: 8
INFO - 16:23:52: Message: Positive directional derivative for linesearch
INFO - 16:23:52: Solution:
INFO - 16:23:52: The solution is feasible.
INFO - 16:23:52: Objective: -2.253375612107262
INFO - 16:23:52: Standardized constraints:
INFO - 16:23:52: g_1 = [-1.39153681e-02 -8.77748164e-03 -1.76458248e-02 -2.66267624e-02
INFO - 16:23:52: -3.41390256e-02 -2.40000000e-01 1.36557432e-14]
INFO - 16:23:52: Design space:
INFO - 16:23:52: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:52: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:52: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:52: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:52: | x_1[1] | 0.75 | 0.7806436836764827 | 1.25 | float |
INFO - 16:23:52: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:52: *** End StructureScenario execution (time: 0:00:00.012946) ***
INFO - 16:23:52: *** Start PropulsionScenario execution ***
INFO - 16:23:52: PropulsionScenario
INFO - 16:23:52: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:52: MDO formulation: MDF
INFO - 16:23:52: Optimization problem:
INFO - 16:23:52: minimize 0.001*-y_4(x_3)
INFO - 16:23:52: with respect to x_3
INFO - 16:23:52: under the inequality constraints
INFO - 16:23:52: g_3(x_3) <= 0
INFO - 16:23:52: over the design space:
INFO - 16:23:52: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:52: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:52: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:52: | x_3 | 0.1 | 0.1582037082879361 | 1 | float |
INFO - 16:23:52: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:52: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:52: 2%|▏ | 1/50 [00:00<00:00, 105.15 it/sec, feas=True, obj=-2.25]
INFO - 16:23:52: 4%|▍ | 2/50 [00:00<00:00, 149.01 it/sec, feas=True, obj=-2.25]
INFO - 16:23:52: 6%|▌ | 3/50 [00:00<00:00, 182.08 it/sec, feas=True, obj=-2.25]
INFO - 16:23:52: Optimization result:
INFO - 16:23:52: Optimizer info:
INFO - 16:23:52: Status: None
INFO - 16:23:52: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:52: Solution:
INFO - 16:23:52: The solution is feasible.
INFO - 16:23:52: Objective: -2.253375612107262
INFO - 16:23:52: Standardized constraints:
INFO - 16:23:52: g_3 = [-8.34884797e-01 -1.65115203e-01 -1.99840144e-15 -1.81426541e-01]
INFO - 16:23:52: Design space:
INFO - 16:23:52: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:52: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:52: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:52: | x_3 | 0.1 | 0.1582037082879361 | 1 | float |
INFO - 16:23:52: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:52: *** End PropulsionScenario execution (time: 0:00:00.018796) ***
INFO - 16:23:52: 61%|██████ | 61/100 [00:35<00:22, 1.72 it/sec, feas=False, obj=-2.25]
INFO - 16:23:52: *** Start PropulsionScenario execution ***
INFO - 16:23:52: PropulsionScenario
INFO - 16:23:52: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:52: MDO formulation: MDF
INFO - 16:23:52: Optimization problem:
INFO - 16:23:52: minimize 0.001*-y_4(x_3)
INFO - 16:23:52: with respect to x_3
INFO - 16:23:52: under the inequality constraints
INFO - 16:23:52: g_3(x_3) <= 0
INFO - 16:23:52: over the design space:
INFO - 16:23:52: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:52: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:52: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:52: | x_3 | 0.1 | 0.1582037082879361 | 1 | float |
INFO - 16:23:52: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:52: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:52: 2%|▏ | 1/50 [00:00<00:01, 37.54 it/sec, feas=False, obj=-2.27]
INFO - 16:23:52: 4%|▍ | 2/50 [00:00<00:01, 37.73 it/sec, feas=True, obj=-2.27]
INFO - 16:23:52: 6%|▌ | 3/50 [00:00<00:01, 31.30 it/sec, feas=False, obj=-2.27]
INFO - 16:23:52: 8%|▊ | 4/50 [00:00<00:01, 28.81 it/sec, feas=True, obj=-2.27]
INFO - 16:23:52: 10%|█ | 5/50 [00:00<00:01, 27.09 it/sec, feas=True, obj=-2.27]
INFO - 16:23:52: Optimization result:
INFO - 16:23:52: Optimizer info:
INFO - 16:23:52: Status: 8
INFO - 16:23:52: Message: Positive directional derivative for linesearch
INFO - 16:23:52: Solution:
INFO - 16:23:52: The solution is feasible.
INFO - 16:23:52: Objective: -2.2710108828562805
INFO - 16:23:52: Standardized constraints:
INFO - 16:23:52: g_3 = [-8.38706171e-01 -1.61293829e-01 4.21884749e-15 -1.81790715e-01]
INFO - 16:23:52: Design space:
INFO - 16:23:52: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:52: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:52: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:52: | x_3 | 0.1 | 0.1578055186129909 | 1 | float |
INFO - 16:23:52: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:52: *** End PropulsionScenario execution (time: 0:00:00.187194) ***
INFO - 16:23:52: *** Start AerodynamicsScenario execution ***
INFO - 16:23:52: AerodynamicsScenario
INFO - 16:23:52: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:52: MDO formulation: MDF
INFO - 16:23:52: Optimization problem:
INFO - 16:23:52: minimize 0.001*-y_4(x_2)
INFO - 16:23:52: with respect to x_2
INFO - 16:23:52: under the inequality constraints
INFO - 16:23:52: g_2(x_2) <= 0
INFO - 16:23:52: over the design space:
INFO - 16:23:52: +------+-------------+-------+-------------+-------+
INFO - 16:23:52: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:52: +------+-------------+-------+-------------+-------+
INFO - 16:23:52: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:52: +------+-------------+-------+-------------+-------+
INFO - 16:23:52: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:52: 2%|▏ | 1/50 [00:00<00:00, 72.09 it/sec, feas=True, obj=-2.27]
INFO - 16:23:52: Optimization result:
INFO - 16:23:52: Optimizer info:
INFO - 16:23:52: Status: 8
INFO - 16:23:52: Message: Positive directional derivative for linesearch
INFO - 16:23:52: Solution:
INFO - 16:23:52: The solution is feasible.
INFO - 16:23:52: Objective: -2.27101088285628
INFO - 16:23:52: Standardized constraints:
INFO - 16:23:52: g_2 = 0.0
INFO - 16:23:52: Design space:
INFO - 16:23:52: +------+-------------+-------+-------------+-------+
INFO - 16:23:52: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:52: +------+-------------+-------+-------------+-------+
INFO - 16:23:52: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:52: +------+-------------+-------+-------------+-------+
INFO - 16:23:52: *** End AerodynamicsScenario execution (time: 0:00:00.015889) ***
INFO - 16:23:52: *** Start StructureScenario execution ***
INFO - 16:23:52: StructureScenario
INFO - 16:23:52: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:52: MDO formulation: MDF
INFO - 16:23:52: Optimization problem:
INFO - 16:23:52: minimize 0.001*-y_4(x_1)
INFO - 16:23:52: with respect to x_1
INFO - 16:23:52: under the inequality constraints
INFO - 16:23:52: g_1(x_1) <= 0
INFO - 16:23:52: over the design space:
INFO - 16:23:52: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:52: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:52: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:52: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:52: | x_1[1] | 0.75 | 0.7806436836764827 | 1.25 | float |
INFO - 16:23:52: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:52: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:52: 2%|▏ | 1/50 [00:00<00:00, 76.86 it/sec, feas=True, obj=-2.27]
INFO - 16:23:52: Optimization result:
INFO - 16:23:52: Optimizer info:
INFO - 16:23:52: Status: 8
INFO - 16:23:52: Message: Positive directional derivative for linesearch
INFO - 16:23:52: Solution:
INFO - 16:23:52: The solution is feasible.
INFO - 16:23:52: Objective: -2.2710108828562805
INFO - 16:23:52: Standardized constraints:
INFO - 16:23:52: g_1 = [-1.59589593e-03 -2.02868890e-03 -1.31333010e-02 -2.32802973e-02
INFO - 16:23:52: -3.14967236e-02 -2.40000000e-01 1.36557432e-14]
INFO - 16:23:52: Design space:
INFO - 16:23:52: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:52: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:52: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:52: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:52: | x_1[1] | 0.75 | 0.7806436836764827 | 1.25 | float |
INFO - 16:23:52: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:52: *** End StructureScenario execution (time: 0:00:00.015337) ***
INFO - 16:23:52: *** Start PropulsionScenario execution ***
INFO - 16:23:52: PropulsionScenario
INFO - 16:23:52: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:52: MDO formulation: MDF
INFO - 16:23:52: Optimization problem:
INFO - 16:23:52: minimize 0.001*-y_4(x_3)
INFO - 16:23:52: with respect to x_3
INFO - 16:23:52: under the inequality constraints
INFO - 16:23:52: g_3(x_3) <= 0
INFO - 16:23:52: over the design space:
INFO - 16:23:52: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:52: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:52: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:52: | x_3 | 0.1 | 0.1578055186129909 | 1 | float |
INFO - 16:23:52: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:52: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:52: 2%|▏ | 1/50 [00:00<00:00, 103.64 it/sec, feas=True, obj=-2.27]
INFO - 16:23:52: 4%|▍ | 2/50 [00:00<00:00, 146.59 it/sec, feas=True, obj=-2.27]
INFO - 16:23:52: 6%|▌ | 3/50 [00:00<00:00, 180.31 it/sec, feas=True, obj=-2.27]
INFO - 16:23:52: Optimization result:
INFO - 16:23:52: Optimizer info:
INFO - 16:23:52: Status: None
INFO - 16:23:52: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:52: Solution:
INFO - 16:23:52: The solution is feasible.
INFO - 16:23:52: Objective: -2.2710108828562805
INFO - 16:23:52: Standardized constraints:
INFO - 16:23:52: g_3 = [-8.38706171e-01 -1.61293829e-01 4.21884749e-15 -1.81790715e-01]
INFO - 16:23:52: Design space:
INFO - 16:23:52: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:52: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:52: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:52: | x_3 | 0.1 | 0.1578055186129909 | 1 | float |
INFO - 16:23:52: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:52: *** End PropulsionScenario execution (time: 0:00:00.019135) ***
INFO - 16:23:52: *** Start AerodynamicsScenario execution ***
INFO - 16:23:52: AerodynamicsScenario
INFO - 16:23:52: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:52: MDO formulation: MDF
INFO - 16:23:52: Optimization problem:
INFO - 16:23:52: minimize 0.001*-y_4(x_2)
INFO - 16:23:52: with respect to x_2
INFO - 16:23:52: under the inequality constraints
INFO - 16:23:52: g_2(x_2) <= 0
INFO - 16:23:52: over the design space:
INFO - 16:23:52: +------+-------------+-------+-------------+-------+
INFO - 16:23:52: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:52: +------+-------------+-------+-------------+-------+
INFO - 16:23:52: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:52: +------+-------------+-------+-------------+-------+
INFO - 16:23:52: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:52: 2%|▏ | 1/50 [00:00<00:00, 81.26 it/sec, feas=True, obj=-2.27]
INFO - 16:23:52: Optimization result:
INFO - 16:23:52: Optimizer info:
INFO - 16:23:52: Status: 8
INFO - 16:23:52: Message: Positive directional derivative for linesearch
INFO - 16:23:52: Solution:
INFO - 16:23:52: The solution is feasible.
INFO - 16:23:52: Objective: -2.2710108828562805
INFO - 16:23:52: Standardized constraints:
INFO - 16:23:52: g_2 = 0.0
INFO - 16:23:52: Design space:
INFO - 16:23:52: +------+-------------+-------+-------------+-------+
INFO - 16:23:52: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:52: +------+-------------+-------+-------------+-------+
INFO - 16:23:52: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:52: +------+-------------+-------+-------------+-------+
INFO - 16:23:52: *** End AerodynamicsScenario execution (time: 0:00:00.014111) ***
INFO - 16:23:52: *** Start StructureScenario execution ***
INFO - 16:23:52: StructureScenario
INFO - 16:23:52: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:52: MDO formulation: MDF
INFO - 16:23:52: Optimization problem:
INFO - 16:23:52: minimize 0.001*-y_4(x_1)
INFO - 16:23:52: with respect to x_1
INFO - 16:23:52: under the inequality constraints
INFO - 16:23:52: g_1(x_1) <= 0
INFO - 16:23:52: over the design space:
INFO - 16:23:52: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:52: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:52: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:52: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:52: | x_1[1] | 0.75 | 0.7806436836764827 | 1.25 | float |
INFO - 16:23:52: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:52: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:52: 2%|▏ | 1/50 [00:00<00:00, 97.16 it/sec, feas=True, obj=-2.27]
INFO - 16:23:52: Optimization result:
INFO - 16:23:52: Optimizer info:
INFO - 16:23:52: Status: 8
INFO - 16:23:52: Message: Positive directional derivative for linesearch
INFO - 16:23:52: Solution:
INFO - 16:23:52: The solution is feasible.
INFO - 16:23:52: Objective: -2.2710108828562805
INFO - 16:23:52: Standardized constraints:
INFO - 16:23:52: g_1 = [-1.59589593e-03 -2.02868890e-03 -1.31333010e-02 -2.32802973e-02
INFO - 16:23:52: -3.14967236e-02 -2.40000000e-01 1.36557432e-14]
INFO - 16:23:52: Design space:
INFO - 16:23:52: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:52: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:52: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:52: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:52: | x_1[1] | 0.75 | 0.7806436836764827 | 1.25 | float |
INFO - 16:23:52: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:52: *** End StructureScenario execution (time: 0:00:00.012649) ***
INFO - 16:23:52: 62%|██████▏ | 62/100 [00:35<00:21, 1.73 it/sec, feas=True, obj=-2.27]
INFO - 16:23:52: *** Start PropulsionScenario execution ***
INFO - 16:23:52: PropulsionScenario
INFO - 16:23:52: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:52: MDO formulation: MDF
INFO - 16:23:52: Optimization problem:
INFO - 16:23:52: minimize 0.001*-y_4(x_3)
INFO - 16:23:52: with respect to x_3
INFO - 16:23:52: under the inequality constraints
INFO - 16:23:52: g_3(x_3) <= 0
INFO - 16:23:52: over the design space:
INFO - 16:23:52: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:52: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:52: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:52: | x_3 | 0.1 | 0.1578055186129909 | 1 | float |
INFO - 16:23:52: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:52: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:52: 2%|▏ | 1/50 [00:00<00:01, 34.08 it/sec, feas=True, obj=-2.24]
INFO - 16:23:52: 4%|▍ | 2/50 [00:00<00:01, 27.96 it/sec, feas=True, obj=-2.24]
INFO - 16:23:52: 6%|▌ | 3/50 [00:00<00:01, 26.17 it/sec, feas=True, obj=-2.24]
INFO - 16:23:52: 8%|▊ | 4/50 [00:00<00:01, 28.48 it/sec, feas=True, obj=-2.24]
INFO - 16:23:52: Optimization result:
INFO - 16:23:52: Optimizer info:
INFO - 16:23:52: Status: None
INFO - 16:23:52: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:52: Solution:
INFO - 16:23:52: The solution is feasible.
INFO - 16:23:52: Objective: -2.2376454194431123
INFO - 16:23:52: Standardized constraints:
INFO - 16:23:52: g_3 = [-8.34032481e-01 -1.65967519e-01 4.88498131e-15 -1.81388705e-01]
INFO - 16:23:52: Design space:
INFO - 16:23:52: +------+-------------+-------------------+-------------+-------+
INFO - 16:23:52: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:52: +------+-------------+-------------------+-------------+-------+
INFO - 16:23:52: | x_3 | 0.1 | 0.158323895563523 | 1 | float |
INFO - 16:23:52: +------+-------------+-------------------+-------------+-------+
INFO - 16:23:52: *** End PropulsionScenario execution (time: 0:00:00.143012) ***
INFO - 16:23:52: *** Start AerodynamicsScenario execution ***
INFO - 16:23:52: AerodynamicsScenario
INFO - 16:23:52: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:52: MDO formulation: MDF
INFO - 16:23:52: Optimization problem:
INFO - 16:23:52: minimize 0.001*-y_4(x_2)
INFO - 16:23:52: with respect to x_2
INFO - 16:23:52: under the inequality constraints
INFO - 16:23:52: g_2(x_2) <= 0
INFO - 16:23:52: over the design space:
INFO - 16:23:52: +------+-------------+-------+-------------+-------+
INFO - 16:23:52: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:52: +------+-------------+-------+-------------+-------+
INFO - 16:23:52: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:52: +------+-------------+-------+-------------+-------+
INFO - 16:23:52: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:52: 2%|▏ | 1/50 [00:00<00:00, 89.78 it/sec, feas=True, obj=-2.24]
INFO - 16:23:52: Optimization result:
INFO - 16:23:52: Optimizer info:
INFO - 16:23:52: Status: 8
INFO - 16:23:52: Message: Positive directional derivative for linesearch
INFO - 16:23:52: Solution:
INFO - 16:23:52: The solution is feasible.
INFO - 16:23:52: Objective: -2.2376454194431123
INFO - 16:23:52: Standardized constraints:
INFO - 16:23:52: g_2 = -1.986074026683049e-05
INFO - 16:23:52: Design space:
INFO - 16:23:52: +------+-------------+-------+-------------+-------+
INFO - 16:23:52: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:52: +------+-------------+-------+-------------+-------+
INFO - 16:23:52: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:52: +------+-------------+-------+-------------+-------+
INFO - 16:23:52: *** End AerodynamicsScenario execution (time: 0:00:00.012861) ***
INFO - 16:23:52: *** Start StructureScenario execution ***
INFO - 16:23:52: StructureScenario
INFO - 16:23:52: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:52: MDO formulation: MDF
INFO - 16:23:52: Optimization problem:
INFO - 16:23:52: minimize 0.001*-y_4(x_1)
INFO - 16:23:52: with respect to x_1
INFO - 16:23:52: under the inequality constraints
INFO - 16:23:52: g_1(x_1) <= 0
INFO - 16:23:52: over the design space:
INFO - 16:23:52: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:52: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:52: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:52: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:52: | x_1[1] | 0.75 | 0.7806436836764827 | 1.25 | float |
INFO - 16:23:52: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:52: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:52: 2%|▏ | 1/50 [00:00<00:00, 96.90 it/sec, feas=True, obj=-2.24]
INFO - 16:23:52: 4%|▍ | 2/50 [00:00<00:00, 126.86 it/sec, feas=True, obj=-2.24]
INFO - 16:23:52: 6%|▌ | 3/50 [00:00<00:00, 79.84 it/sec, feas=True, obj=-2.24]
INFO - 16:23:52: Optimization result:
INFO - 16:23:52: Optimizer info:
INFO - 16:23:52: Status: None
INFO - 16:23:52: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:52: Solution:
INFO - 16:23:52: The solution is feasible.
INFO - 16:23:52: Objective: -2.2376454194431123
INFO - 16:23:52: Standardized constraints:
INFO - 16:23:52: g_1 = [-1.43674726e-03 -1.94140555e-03 -1.30748944e-02 -2.32369589e-02
INFO - 16:23:52: -3.14624898e-02 -2.40000000e-01 1.36557432e-14]
INFO - 16:23:52: Design space:
INFO - 16:23:52: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:52: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:52: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:52: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:52: | x_1[1] | 0.75 | 0.7806436836764827 | 1.25 | float |
INFO - 16:23:52: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:52: *** End StructureScenario execution (time: 0:00:00.040008) ***
INFO - 16:23:52: *** Start PropulsionScenario execution ***
INFO - 16:23:52: PropulsionScenario
INFO - 16:23:52: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:52: MDO formulation: MDF
INFO - 16:23:52: Optimization problem:
INFO - 16:23:52: minimize 0.001*-y_4(x_3)
INFO - 16:23:52: with respect to x_3
INFO - 16:23:52: under the inequality constraints
INFO - 16:23:52: g_3(x_3) <= 0
INFO - 16:23:52: over the design space:
INFO - 16:23:52: +------+-------------+-------------------+-------------+-------+
INFO - 16:23:52: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:52: +------+-------------+-------------------+-------------+-------+
INFO - 16:23:52: | x_3 | 0.1 | 0.158323895563523 | 1 | float |
INFO - 16:23:52: +------+-------------+-------------------+-------------+-------+
INFO - 16:23:52: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:52: 2%|▏ | 1/50 [00:00<00:00, 72.60 it/sec, feas=True, obj=-2.24]
INFO - 16:23:52: Optimization result:
INFO - 16:23:52: Optimizer info:
INFO - 16:23:52: Status: 8
INFO - 16:23:52: Message: Positive directional derivative for linesearch
INFO - 16:23:52: Solution:
INFO - 16:23:52: The solution is feasible.
INFO - 16:23:52: Objective: -2.2376454194431123
INFO - 16:23:52: Standardized constraints:
INFO - 16:23:52: g_3 = [-8.34032481e-01 -1.65967519e-01 4.88498131e-15 -1.81388705e-01]
INFO - 16:23:52: Design space:
INFO - 16:23:52: +------+-------------+-------------------+-------------+-------+
INFO - 16:23:52: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:52: +------+-------------+-------------------+-------------+-------+
INFO - 16:23:52: | x_3 | 0.1 | 0.158323895563523 | 1 | float |
INFO - 16:23:52: +------+-------------+-------------------+-------------+-------+
INFO - 16:23:52: *** End PropulsionScenario execution (time: 0:00:00.015541) ***
INFO - 16:23:53: 63%|██████▎ | 63/100 [00:36<00:21, 1.74 it/sec, feas=True, obj=-2.24]
INFO - 16:23:53: *** Start PropulsionScenario execution ***
INFO - 16:23:53: PropulsionScenario
INFO - 16:23:53: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:53: MDO formulation: MDF
INFO - 16:23:53: Optimization problem:
INFO - 16:23:53: minimize 0.001*-y_4(x_3)
INFO - 16:23:53: with respect to x_3
INFO - 16:23:53: under the inequality constraints
INFO - 16:23:53: g_3(x_3) <= 0
INFO - 16:23:53: over the design space:
INFO - 16:23:53: +------+-------------+-------------------+-------------+-------+
INFO - 16:23:53: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:53: +------+-------------+-------------------+-------------+-------+
INFO - 16:23:53: | x_3 | 0.1 | 0.158323895563523 | 1 | float |
INFO - 16:23:53: +------+-------------+-------------------+-------------+-------+
INFO - 16:23:53: Solving optimization problem with algorithm SLSQP:
WARNING - 16:23:53: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 6.724932466608626e-05 is still above the tolerance 1e-06.
INFO - 16:23:53: 2%|▏ | 1/50 [00:00<00:01, 33.77 it/sec, feas=False, obj=-2.27]
INFO - 16:23:53: 4%|▍ | 2/50 [00:00<00:01, 36.24 it/sec, feas=True, obj=-2.27]
INFO - 16:23:53: 6%|▌ | 3/50 [00:00<00:01, 30.83 it/sec, feas=False, obj=-2.27]
INFO - 16:23:53: 8%|▊ | 4/50 [00:00<00:01, 28.37 it/sec, feas=True, obj=-2.27]
INFO - 16:23:53: 10%|█ | 5/50 [00:00<00:01, 29.60 it/sec, feas=True, obj=-2.27]
INFO - 16:23:53: 12%|█▏ | 6/50 [00:00<00:01, 28.25 it/sec, feas=True, obj=-2.27]
INFO - 16:23:53: Optimization result:
INFO - 16:23:53: Optimizer info:
INFO - 16:23:53: Status: None
INFO - 16:23:53: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:53: Solution:
INFO - 16:23:53: The solution is feasible.
INFO - 16:23:53: Objective: -2.2709535426176632
INFO - 16:23:53: Standardized constraints:
INFO - 16:23:53: g_3 = [-8.38719254e-01 -1.61280746e-01 1.33226763e-15 -1.81789082e-01]
INFO - 16:23:53: Design space:
INFO - 16:23:53: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:53: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:53: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:53: | x_3 | 0.1 | 0.1578072749470809 | 1 | float |
INFO - 16:23:53: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:53: *** End PropulsionScenario execution (time: 0:00:00.214996) ***
INFO - 16:23:53: *** Start AerodynamicsScenario execution ***
INFO - 16:23:53: AerodynamicsScenario
INFO - 16:23:53: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:53: MDO formulation: MDF
INFO - 16:23:53: Optimization problem:
INFO - 16:23:53: minimize 0.001*-y_4(x_2)
INFO - 16:23:53: with respect to x_2
INFO - 16:23:53: under the inequality constraints
INFO - 16:23:53: g_2(x_2) <= 0
INFO - 16:23:53: over the design space:
INFO - 16:23:53: +------+-------------+-------+-------------+-------+
INFO - 16:23:53: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:53: +------+-------------+-------+-------------+-------+
INFO - 16:23:53: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:53: +------+-------------+-------+-------------+-------+
INFO - 16:23:53: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:53: 2%|▏ | 1/50 [00:00<00:00, 99.43 it/sec, feas=True, obj=-2.27]
INFO - 16:23:53: Optimization result:
INFO - 16:23:53: Optimizer info:
INFO - 16:23:53: Status: 8
INFO - 16:23:53: Message: Positive directional derivative for linesearch
INFO - 16:23:53: Solution:
INFO - 16:23:53: The solution is feasible.
INFO - 16:23:53: Objective: -2.2709535426176632
INFO - 16:23:53: Standardized constraints:
INFO - 16:23:53: g_2 = 0.0
INFO - 16:23:53: Design space:
INFO - 16:23:53: +------+-------------+-------+-------------+-------+
INFO - 16:23:53: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:53: +------+-------------+-------+-------------+-------+
INFO - 16:23:53: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:53: +------+-------------+-------+-------------+-------+
INFO - 16:23:53: *** End AerodynamicsScenario execution (time: 0:00:00.011929) ***
INFO - 16:23:53: *** Start StructureScenario execution ***
INFO - 16:23:53: StructureScenario
INFO - 16:23:53: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:53: MDO formulation: MDF
INFO - 16:23:53: Optimization problem:
INFO - 16:23:53: minimize 0.001*-y_4(x_1)
INFO - 16:23:53: with respect to x_1
INFO - 16:23:53: under the inequality constraints
INFO - 16:23:53: g_1(x_1) <= 0
INFO - 16:23:53: over the design space:
INFO - 16:23:53: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:53: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:53: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:53: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:53: | x_1[1] | 0.75 | 0.7806436836764827 | 1.25 | float |
INFO - 16:23:53: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:53: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:53: 2%|▏ | 1/50 [00:00<00:00, 94.43 it/sec, feas=True, obj=-2.27]
INFO - 16:23:53: 4%|▍ | 2/50 [00:00<00:00, 58.27 it/sec, feas=True, obj=-2.27]
INFO - 16:23:53: 6%|▌ | 3/50 [00:00<00:00, 72.79 it/sec, feas=True, obj=-2.27]
INFO - 16:23:53: Optimization result:
INFO - 16:23:53: Optimizer info:
INFO - 16:23:53: Status: None
INFO - 16:23:53: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:53: Solution:
INFO - 16:23:53: The solution is feasible.
INFO - 16:23:53: Objective: -2.2709535426176632
INFO - 16:23:53: Standardized constraints:
INFO - 16:23:53: g_1 = [-1.59589593e-03 -2.02868890e-03 -1.31333010e-02 -2.32802973e-02
INFO - 16:23:53: -3.14967236e-02 -2.40000000e-01 1.36557432e-14]
INFO - 16:23:53: Design space:
INFO - 16:23:53: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:53: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:53: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:53: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:53: | x_1[1] | 0.75 | 0.7806436836764827 | 1.25 | float |
INFO - 16:23:53: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:53: *** End StructureScenario execution (time: 0:00:00.043765) ***
INFO - 16:23:53: *** Start PropulsionScenario execution ***
INFO - 16:23:53: PropulsionScenario
INFO - 16:23:53: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:53: MDO formulation: MDF
INFO - 16:23:53: Optimization problem:
INFO - 16:23:53: minimize 0.001*-y_4(x_3)
INFO - 16:23:53: with respect to x_3
INFO - 16:23:53: under the inequality constraints
INFO - 16:23:53: g_3(x_3) <= 0
INFO - 16:23:53: over the design space:
INFO - 16:23:53: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:53: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:53: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:53: | x_3 | 0.1 | 0.1578072749470809 | 1 | float |
INFO - 16:23:53: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:53: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:53: 2%|▏ | 1/50 [00:00<00:00, 92.55 it/sec, feas=True, obj=-2.27]
INFO - 16:23:53: Optimization result:
INFO - 16:23:53: Optimizer info:
INFO - 16:23:53: Status: 8
INFO - 16:23:53: Message: Positive directional derivative for linesearch
INFO - 16:23:53: Solution:
INFO - 16:23:53: The solution is feasible.
INFO - 16:23:53: Objective: -2.2709535426176632
INFO - 16:23:53: Standardized constraints:
INFO - 16:23:53: g_3 = [-8.38719254e-01 -1.61280746e-01 1.33226763e-15 -1.81789082e-01]
INFO - 16:23:53: Design space:
INFO - 16:23:53: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:53: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:53: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:53: | x_3 | 0.1 | 0.1578072749470809 | 1 | float |
INFO - 16:23:53: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:53: *** End PropulsionScenario execution (time: 0:00:00.012761) ***
INFO - 16:23:53: 64%|██████▍ | 64/100 [00:36<00:20, 1.76 it/sec, feas=True, obj=-2.27]
INFO - 16:23:53: *** Start PropulsionScenario execution ***
INFO - 16:23:53: PropulsionScenario
INFO - 16:23:53: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:53: MDO formulation: MDF
INFO - 16:23:53: Optimization problem:
INFO - 16:23:53: minimize 0.001*-y_4(x_3)
INFO - 16:23:53: with respect to x_3
INFO - 16:23:53: under the inequality constraints
INFO - 16:23:53: g_3(x_3) <= 0
INFO - 16:23:53: over the design space:
INFO - 16:23:53: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:53: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:53: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:53: | x_3 | 0.1 | 0.1578072749470809 | 1 | float |
INFO - 16:23:53: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:53: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:53: 2%|▏ | 1/50 [00:00<00:01, 38.59 it/sec, feas=True, obj=-2.26]
INFO - 16:23:53: 4%|▍ | 2/50 [00:00<00:01, 29.56 it/sec, feas=True, obj=-2.26]
INFO - 16:23:53: 6%|▌ | 3/50 [00:00<00:01, 27.73 it/sec, feas=True, obj=-2.26]
INFO - 16:23:53: Optimization result:
INFO - 16:23:53: Optimizer info:
INFO - 16:23:53: Status: 8
INFO - 16:23:53: Message: Positive directional derivative for linesearch
INFO - 16:23:53: Solution:
INFO - 16:23:53: The solution is feasible.
INFO - 16:23:53: Objective: -2.2596008096630142
INFO - 16:23:53: Standardized constraints:
INFO - 16:23:53: g_3 = [-8.37609366e-01 -1.62390634e-01 7.77156117e-15 -1.81570707e-01]
INFO - 16:23:53: Design space:
INFO - 16:23:53: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:53: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:53: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:53: | x_3 | 0.1 | 0.1580424790111169 | 1 | float |
INFO - 16:23:53: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:53: *** End PropulsionScenario execution (time: 0:00:00.110480) ***
INFO - 16:23:53: *** Start AerodynamicsScenario execution ***
INFO - 16:23:53: AerodynamicsScenario
INFO - 16:23:53: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:53: MDO formulation: MDF
INFO - 16:23:53: Optimization problem:
INFO - 16:23:53: minimize 0.001*-y_4(x_2)
INFO - 16:23:53: with respect to x_2
INFO - 16:23:53: under the inequality constraints
INFO - 16:23:53: g_2(x_2) <= 0
INFO - 16:23:53: over the design space:
INFO - 16:23:53: +------+-------------+-------+-------------+-------+
INFO - 16:23:53: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:53: +------+-------------+-------+-------------+-------+
INFO - 16:23:53: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:53: +------+-------------+-------+-------------+-------+
INFO - 16:23:53: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:53: 2%|▏ | 1/50 [00:00<00:00, 76.45 it/sec, feas=True, obj=-2.26]
INFO - 16:23:53: Optimization result:
INFO - 16:23:53: Optimizer info:
INFO - 16:23:53: Status: 8
INFO - 16:23:53: Message: Positive directional derivative for linesearch
INFO - 16:23:53: Solution:
INFO - 16:23:53: The solution is feasible.
INFO - 16:23:53: Objective: -2.259600809663015
INFO - 16:23:53: Standardized constraints:
INFO - 16:23:53: g_2 = 0.0
INFO - 16:23:53: Design space:
INFO - 16:23:53: +------+-------------+-------+-------------+-------+
INFO - 16:23:53: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:53: +------+-------------+-------+-------------+-------+
INFO - 16:23:53: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:53: +------+-------------+-------+-------------+-------+
INFO - 16:23:53: *** End AerodynamicsScenario execution (time: 0:00:00.014805) ***
INFO - 16:23:53: *** Start StructureScenario execution ***
INFO - 16:23:53: StructureScenario
INFO - 16:23:53: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:53: MDO formulation: MDF
INFO - 16:23:53: Optimization problem:
INFO - 16:23:53: minimize 0.001*-y_4(x_1)
INFO - 16:23:53: with respect to x_1
INFO - 16:23:53: under the inequality constraints
INFO - 16:23:53: g_1(x_1) <= 0
INFO - 16:23:53: over the design space:
INFO - 16:23:53: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:53: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:53: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:53: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:53: | x_1[1] | 0.75 | 0.7806436836764827 | 1.25 | float |
INFO - 16:23:53: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:53: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:53: 2%|▏ | 1/50 [00:00<00:00, 82.32 it/sec, feas=True, obj=-2.26]
INFO - 16:23:53: 4%|▍ | 2/50 [00:00<00:00, 55.82 it/sec, feas=True, obj=-2.26]
INFO - 16:23:53: 6%|▌ | 3/50 [00:00<00:00, 49.23 it/sec, feas=True, obj=-2.26]
INFO - 16:23:53: Optimization result:
INFO - 16:23:53: Optimizer info:
INFO - 16:23:53: Status: 8
INFO - 16:23:53: Message: Positive directional derivative for linesearch
INFO - 16:23:53: Solution:
INFO - 16:23:53: The solution is feasible.
INFO - 16:23:53: Objective: -2.2596008096630142
INFO - 16:23:53: Standardized constraints:
INFO - 16:23:53: g_1 = [-1.59589593e-03 -2.02868890e-03 -1.31333010e-02 -2.32802973e-02
INFO - 16:23:53: -3.14967236e-02 -2.40000000e-01 1.36557432e-14]
INFO - 16:23:53: Design space:
INFO - 16:23:53: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:53: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:53: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:53: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:53: | x_1[1] | 0.75 | 0.7806436836764827 | 1.25 | float |
INFO - 16:23:53: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:53: *** End StructureScenario execution (time: 0:00:00.063376) ***
INFO - 16:23:53: *** Start PropulsionScenario execution ***
INFO - 16:23:53: PropulsionScenario
INFO - 16:23:53: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:53: MDO formulation: MDF
INFO - 16:23:53: Optimization problem:
INFO - 16:23:53: minimize 0.001*-y_4(x_3)
INFO - 16:23:53: with respect to x_3
INFO - 16:23:53: under the inequality constraints
INFO - 16:23:53: g_3(x_3) <= 0
INFO - 16:23:53: over the design space:
INFO - 16:23:53: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:53: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:53: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:53: | x_3 | 0.1 | 0.1580424790111169 | 1 | float |
INFO - 16:23:53: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:53: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:53: 2%|▏ | 1/50 [00:00<00:00, 90.90 it/sec, feas=True, obj=-2.26]
INFO - 16:23:53: Optimization result:
INFO - 16:23:53: Optimizer info:
INFO - 16:23:53: Status: 8
INFO - 16:23:53: Message: Positive directional derivative for linesearch
INFO - 16:23:53: Solution:
INFO - 16:23:53: The solution is feasible.
INFO - 16:23:53: Objective: -2.2596008096630142
INFO - 16:23:53: Standardized constraints:
INFO - 16:23:53: g_3 = [-8.37609366e-01 -1.62390634e-01 7.77156117e-15 -1.81570707e-01]
INFO - 16:23:53: Design space:
INFO - 16:23:53: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:53: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:53: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:53: | x_3 | 0.1 | 0.1580424790111169 | 1 | float |
INFO - 16:23:53: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:53: *** End PropulsionScenario execution (time: 0:00:00.012774) ***
INFO - 16:23:53: *** Start AerodynamicsScenario execution ***
INFO - 16:23:53: AerodynamicsScenario
INFO - 16:23:53: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:53: MDO formulation: MDF
INFO - 16:23:53: Optimization problem:
INFO - 16:23:53: minimize 0.001*-y_4(x_2)
INFO - 16:23:53: with respect to x_2
INFO - 16:23:53: under the inequality constraints
INFO - 16:23:53: g_2(x_2) <= 0
INFO - 16:23:53: over the design space:
INFO - 16:23:53: +------+-------------+-------+-------------+-------+
INFO - 16:23:53: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:53: +------+-------------+-------+-------------+-------+
INFO - 16:23:53: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:53: +------+-------------+-------+-------------+-------+
INFO - 16:23:53: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:53: 2%|▏ | 1/50 [00:00<00:00, 108.13 it/sec, feas=True, obj=-2.26]
INFO - 16:23:53: Optimization result:
INFO - 16:23:53: Optimizer info:
INFO - 16:23:53: Status: 8
INFO - 16:23:53: Message: Positive directional derivative for linesearch
INFO - 16:23:53: Solution:
INFO - 16:23:53: The solution is feasible.
INFO - 16:23:53: Objective: -2.2596008096630142
INFO - 16:23:53: Standardized constraints:
INFO - 16:23:53: g_2 = 0.0
INFO - 16:23:53: Design space:
INFO - 16:23:53: +------+-------------+-------+-------------+-------+
INFO - 16:23:53: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:53: +------+-------------+-------+-------------+-------+
INFO - 16:23:53: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:53: +------+-------------+-------+-------------+-------+
INFO - 16:23:53: *** End AerodynamicsScenario execution (time: 0:00:00.010808) ***
INFO - 16:23:53: *** Start StructureScenario execution ***
INFO - 16:23:53: StructureScenario
INFO - 16:23:53: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:53: MDO formulation: MDF
INFO - 16:23:53: Optimization problem:
INFO - 16:23:53: minimize 0.001*-y_4(x_1)
INFO - 16:23:53: with respect to x_1
INFO - 16:23:53: under the inequality constraints
INFO - 16:23:53: g_1(x_1) <= 0
INFO - 16:23:53: over the design space:
INFO - 16:23:53: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:53: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:53: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:53: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:53: | x_1[1] | 0.75 | 0.7806436836764827 | 1.25 | float |
INFO - 16:23:53: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:53: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:53: 2%|▏ | 1/50 [00:00<00:00, 102.36 it/sec, feas=True, obj=-2.26]
INFO - 16:23:53: 4%|▍ | 2/50 [00:00<00:00, 60.43 it/sec, feas=True, obj=-2.26]
INFO - 16:23:53: 6%|▌ | 3/50 [00:00<00:00, 50.28 it/sec, feas=True, obj=-2.26]
INFO - 16:23:53: Optimization result:
INFO - 16:23:53: Optimizer info:
INFO - 16:23:53: Status: 8
INFO - 16:23:53: Message: Positive directional derivative for linesearch
INFO - 16:23:53: Solution:
INFO - 16:23:53: The solution is feasible.
INFO - 16:23:53: Objective: -2.2596008096630142
INFO - 16:23:53: Standardized constraints:
INFO - 16:23:53: g_1 = [-1.59589593e-03 -2.02868890e-03 -1.31333010e-02 -2.32802973e-02
INFO - 16:23:53: -3.14967236e-02 -2.40000000e-01 1.36557432e-14]
INFO - 16:23:53: Design space:
INFO - 16:23:53: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:53: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:53: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:53: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:53: | x_1[1] | 0.75 | 0.7806436836764827 | 1.25 | float |
INFO - 16:23:53: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:53: *** End StructureScenario execution (time: 0:00:00.061942) ***
INFO - 16:23:53: 65%|██████▌ | 65/100 [00:36<00:19, 1.77 it/sec, feas=True, obj=-2.26]
INFO - 16:23:53: *** Start PropulsionScenario execution ***
INFO - 16:23:53: PropulsionScenario
INFO - 16:23:53: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:53: MDO formulation: MDF
INFO - 16:23:53: Optimization problem:
INFO - 16:23:53: minimize 0.001*-y_4(x_3)
INFO - 16:23:53: with respect to x_3
INFO - 16:23:53: under the inequality constraints
INFO - 16:23:53: g_3(x_3) <= 0
INFO - 16:23:53: over the design space:
INFO - 16:23:53: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:53: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:53: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:53: | x_3 | 0.1 | 0.1580424790111169 | 1 | float |
INFO - 16:23:53: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:53: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:53: 2%|▏ | 1/50 [00:00<00:01, 38.63 it/sec, feas=True, obj=-2.24]
INFO - 16:23:53: 4%|▍ | 2/50 [00:00<00:01, 29.54 it/sec, feas=True, obj=-2.24]
INFO - 16:23:53: 6%|▌ | 3/50 [00:00<00:01, 32.59 it/sec, feas=True, obj=-2.24]
INFO - 16:23:53: 8%|▊ | 4/50 [00:00<00:01, 34.01 it/sec, feas=True, obj=-2.24]
INFO - 16:23:53: Optimization result:
INFO - 16:23:53: Optimizer info:
INFO - 16:23:53: Status: None
INFO - 16:23:53: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:53: Solution:
INFO - 16:23:53: The solution is feasible.
INFO - 16:23:53: Objective: -2.244139152383384
INFO - 16:23:53: Standardized constraints:
INFO - 16:23:53: g_3 = [-8.36369678e-01 -1.63630322e-01 1.55431223e-15 -1.81296306e-01]
INFO - 16:23:53: Design space:
INFO - 16:23:53: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:53: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:53: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:53: | x_3 | 0.1 | 0.1584581367441573 | 1 | float |
INFO - 16:23:53: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:53: *** End PropulsionScenario execution (time: 0:00:00.120073) ***
INFO - 16:23:53: *** Start AerodynamicsScenario execution ***
INFO - 16:23:53: AerodynamicsScenario
INFO - 16:23:53: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:53: MDO formulation: MDF
INFO - 16:23:53: Optimization problem:
INFO - 16:23:53: minimize 0.001*-y_4(x_2)
INFO - 16:23:53: with respect to x_2
INFO - 16:23:53: under the inequality constraints
INFO - 16:23:53: g_2(x_2) <= 0
INFO - 16:23:53: over the design space:
INFO - 16:23:53: +------+-------------+-------+-------------+-------+
INFO - 16:23:53: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:53: +------+-------------+-------+-------------+-------+
INFO - 16:23:53: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:53: +------+-------------+-------+-------------+-------+
INFO - 16:23:53: Solving optimization problem with algorithm SLSQP:
WARNING - 16:23:53: Optimization found no feasible point; the least infeasible point is selected.
INFO - 16:23:53: 2%|▏ | 1/50 [00:00<00:00, 66.81 it/sec, feas=False, obj=-2.24]
INFO - 16:23:53: Optimization result:
INFO - 16:23:53: Optimizer info:
INFO - 16:23:53: Status: 8
INFO - 16:23:53: Message: Positive directional derivative for linesearch
INFO - 16:23:53: Solution:
WARNING - 16:23:53: The solution is not feasible.
INFO - 16:23:53: Objective: -2.2441391523833834
INFO - 16:23:53: Standardized constraints:
INFO - 16:23:53: g_2 = 0.00010407937007195223
INFO - 16:23:53: Design space:
INFO - 16:23:53: +------+-------------+-------+-------------+-------+
INFO - 16:23:53: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:53: +------+-------------+-------+-------------+-------+
INFO - 16:23:53: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:53: +------+-------------+-------+-------------+-------+
INFO - 16:23:53: *** End AerodynamicsScenario execution (time: 0:00:00.016613) ***
INFO - 16:23:53: *** Start StructureScenario execution ***
INFO - 16:23:53: StructureScenario
INFO - 16:23:53: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:53: MDO formulation: MDF
INFO - 16:23:53: Optimization problem:
INFO - 16:23:53: minimize 0.001*-y_4(x_1)
INFO - 16:23:53: with respect to x_1
INFO - 16:23:53: under the inequality constraints
INFO - 16:23:53: g_1(x_1) <= 0
INFO - 16:23:53: over the design space:
INFO - 16:23:53: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:53: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:53: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:53: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:53: | x_1[1] | 0.75 | 0.7806436836764827 | 1.25 | float |
INFO - 16:23:53: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:53: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:53: 2%|▏ | 1/50 [00:00<00:00, 80.93 it/sec, feas=True, obj=-2.24]
INFO - 16:23:53: Optimization result:
INFO - 16:23:53: Optimizer info:
INFO - 16:23:53: Status: 8
INFO - 16:23:53: Message: Positive directional derivative for linesearch
INFO - 16:23:53: Solution:
INFO - 16:23:53: The solution is feasible.
INFO - 16:23:53: Objective: -2.244139152383384
INFO - 16:23:53: Standardized constraints:
INFO - 16:23:53: g_1 = [-2.43031091e-03 -2.48627281e-03 -1.34394792e-02 -2.35074751e-02
INFO - 16:23:53: -3.16761692e-02 -2.40000000e-01 1.36557432e-14]
INFO - 16:23:53: Design space:
INFO - 16:23:53: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:53: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:53: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:53: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:53: | x_1[1] | 0.75 | 0.7806436836764827 | 1.25 | float |
INFO - 16:23:53: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:53: *** End StructureScenario execution (time: 0:00:00.014571) ***
INFO - 16:23:53: *** Start PropulsionScenario execution ***
INFO - 16:23:53: PropulsionScenario
INFO - 16:23:53: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:53: MDO formulation: MDF
INFO - 16:23:53: Optimization problem:
INFO - 16:23:53: minimize 0.001*-y_4(x_3)
INFO - 16:23:53: with respect to x_3
INFO - 16:23:53: under the inequality constraints
INFO - 16:23:53: g_3(x_3) <= 0
INFO - 16:23:53: over the design space:
INFO - 16:23:53: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:53: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:53: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:53: | x_3 | 0.1 | 0.1584581367441573 | 1 | float |
INFO - 16:23:53: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:53: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:53: 2%|▏ | 1/50 [00:00<00:00, 87.98 it/sec, feas=True, obj=-2.24]
INFO - 16:23:53: Optimization result:
INFO - 16:23:53: Optimizer info:
INFO - 16:23:53: Status: 8
INFO - 16:23:53: Message: Positive directional derivative for linesearch
INFO - 16:23:53: Solution:
INFO - 16:23:53: The solution is feasible.
INFO - 16:23:53: Objective: -2.244139152383384
INFO - 16:23:53: Standardized constraints:
INFO - 16:23:53: g_3 = [-8.36369678e-01 -1.63630322e-01 1.55431223e-15 -1.81296306e-01]
INFO - 16:23:53: Design space:
INFO - 16:23:53: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:53: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:53: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:53: | x_3 | 0.1 | 0.1584581367441573 | 1 | float |
INFO - 16:23:53: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:53: *** End PropulsionScenario execution (time: 0:00:00.013351) ***
INFO - 16:23:53: *** Start AerodynamicsScenario execution ***
INFO - 16:23:53: AerodynamicsScenario
INFO - 16:23:53: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:53: MDO formulation: MDF
INFO - 16:23:53: Optimization problem:
INFO - 16:23:53: minimize 0.001*-y_4(x_2)
INFO - 16:23:53: with respect to x_2
INFO - 16:23:53: under the inequality constraints
INFO - 16:23:53: g_2(x_2) <= 0
INFO - 16:23:53: over the design space:
INFO - 16:23:53: +------+-------------+-------+-------------+-------+
INFO - 16:23:53: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:53: +------+-------------+-------+-------------+-------+
INFO - 16:23:53: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:53: +------+-------------+-------+-------------+-------+
INFO - 16:23:53: Solving optimization problem with algorithm SLSQP:
WARNING - 16:23:53: Optimization found no feasible point; the least infeasible point is selected.
INFO - 16:23:53: 2%|▏ | 1/50 [00:00<00:00, 106.73 it/sec, feas=False, obj=-2.24]
INFO - 16:23:53: Optimization result:
INFO - 16:23:53: Optimizer info:
INFO - 16:23:53: Status: 8
INFO - 16:23:53: Message: Positive directional derivative for linesearch
INFO - 16:23:53: Solution:
WARNING - 16:23:53: The solution is not feasible.
INFO - 16:23:53: Objective: -2.244139152383384
INFO - 16:23:53: Standardized constraints:
INFO - 16:23:53: g_2 = 0.00010407937007195223
INFO - 16:23:53: Design space:
INFO - 16:23:53: +------+-------------+-------+-------------+-------+
INFO - 16:23:53: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:53: +------+-------------+-------+-------------+-------+
INFO - 16:23:53: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:53: +------+-------------+-------+-------------+-------+
INFO - 16:23:53: *** End AerodynamicsScenario execution (time: 0:00:00.011038) ***
INFO - 16:23:53: *** Start StructureScenario execution ***
INFO - 16:23:53: StructureScenario
INFO - 16:23:53: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:53: MDO formulation: MDF
INFO - 16:23:53: Optimization problem:
INFO - 16:23:53: minimize 0.001*-y_4(x_1)
INFO - 16:23:53: with respect to x_1
INFO - 16:23:53: under the inequality constraints
INFO - 16:23:53: g_1(x_1) <= 0
INFO - 16:23:53: over the design space:
INFO - 16:23:53: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:53: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:53: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:53: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:53: | x_1[1] | 0.75 | 0.7806436836764827 | 1.25 | float |
INFO - 16:23:53: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:53: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:53: 2%|▏ | 1/50 [00:00<00:00, 101.23 it/sec, feas=True, obj=-2.24]
INFO - 16:23:53: Optimization result:
INFO - 16:23:53: Optimizer info:
INFO - 16:23:53: Status: 8
INFO - 16:23:53: Message: Positive directional derivative for linesearch
INFO - 16:23:53: Solution:
INFO - 16:23:53: The solution is feasible.
INFO - 16:23:53: Objective: -2.244139152383384
INFO - 16:23:53: Standardized constraints:
INFO - 16:23:53: g_1 = [-2.43031091e-03 -2.48627281e-03 -1.34394792e-02 -2.35074751e-02
INFO - 16:23:53: -3.16761692e-02 -2.40000000e-01 1.36557432e-14]
INFO - 16:23:53: Design space:
INFO - 16:23:53: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:53: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:53: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:53: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:53: | x_1[1] | 0.75 | 0.7806436836764827 | 1.25 | float |
INFO - 16:23:53: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:53: *** End StructureScenario execution (time: 0:00:00.011759) ***
INFO - 16:23:53: 66%|██████▌ | 66/100 [00:36<00:19, 1.79 it/sec, feas=False, obj=-2.24]
INFO - 16:23:53: *** Start PropulsionScenario execution ***
INFO - 16:23:53: PropulsionScenario
INFO - 16:23:53: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:53: MDO formulation: MDF
INFO - 16:23:53: Optimization problem:
INFO - 16:23:53: minimize 0.001*-y_4(x_3)
INFO - 16:23:53: with respect to x_3
INFO - 16:23:53: under the inequality constraints
INFO - 16:23:53: g_3(x_3) <= 0
INFO - 16:23:53: over the design space:
INFO - 16:23:53: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:53: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:53: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:53: | x_3 | 0.1 | 0.1584581367441573 | 1 | float |
INFO - 16:23:53: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:53: Solving optimization problem with algorithm SLSQP:
WARNING - 16:23:53: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 6.724932466608626e-05 is still above the tolerance 1e-06.
INFO - 16:23:53: 2%|▏ | 1/50 [00:00<00:01, 33.45 it/sec, feas=False, obj=-2.26]
INFO - 16:23:53: 4%|▍ | 2/50 [00:00<00:01, 35.87 it/sec, feas=True, obj=-2.26]
INFO - 16:23:53: 6%|▌ | 3/50 [00:00<00:01, 31.08 it/sec, feas=False, obj=-2.26]
INFO - 16:23:54: 8%|▊ | 4/50 [00:00<00:01, 28.89 it/sec, feas=True, obj=-2.26]
INFO - 16:23:54: 10%|█ | 5/50 [00:00<00:01, 27.86 it/sec, feas=True, obj=-2.26]
WARNING - 16:23:54: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 6.724932466608626e-05 is still above the tolerance 1e-06.
INFO - 16:23:54: 12%|█▏ | 6/50 [00:00<00:01, 28.63 it/sec, feas=True, obj=-2.26]
INFO - 16:23:54: Optimization result:
INFO - 16:23:54: Optimizer info:
INFO - 16:23:54: Status: None
INFO - 16:23:54: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:54: Solution:
INFO - 16:23:54: The solution is feasible.
INFO - 16:23:54: Objective: -2.2629808707273313
INFO - 16:23:54: Standardized constraints:
INFO - 16:23:54: g_3 = [-8.35396332e-01 -1.64603668e-01 4.21884749e-15 -1.81703256e-01]
INFO - 16:23:54: Design space:
INFO - 16:23:54: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:54: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:54: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:54: | x_3 | 0.1 | 0.1578996407261434 | 1 | float |
INFO - 16:23:54: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:54: *** End PropulsionScenario execution (time: 0:00:00.211936) ***
INFO - 16:23:54: *** Start AerodynamicsScenario execution ***
INFO - 16:23:54: AerodynamicsScenario
INFO - 16:23:54: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:54: MDO formulation: MDF
INFO - 16:23:54: Optimization problem:
INFO - 16:23:54: minimize 0.001*-y_4(x_2)
INFO - 16:23:54: with respect to x_2
INFO - 16:23:54: under the inequality constraints
INFO - 16:23:54: g_2(x_2) <= 0
INFO - 16:23:54: over the design space:
INFO - 16:23:54: +------+-------------+-------+-------------+-------+
INFO - 16:23:54: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:54: +------+-------------+-------+-------------+-------+
INFO - 16:23:54: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:54: +------+-------------+-------+-------------+-------+
INFO - 16:23:54: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:54: 2%|▏ | 1/50 [00:00<00:00, 71.13 it/sec, feas=True, obj=-2.26]
INFO - 16:23:54: Optimization result:
INFO - 16:23:54: Optimizer info:
INFO - 16:23:54: Status: 8
INFO - 16:23:54: Message: Positive directional derivative for linesearch
INFO - 16:23:54: Solution:
INFO - 16:23:54: The solution is feasible.
INFO - 16:23:54: Objective: -2.2629808707273313
INFO - 16:23:54: Standardized constraints:
INFO - 16:23:54: g_2 = 2.220446049250313e-16
INFO - 16:23:54: Design space:
INFO - 16:23:54: +------+-------------+-------+-------------+-------+
INFO - 16:23:54: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:54: +------+-------------+-------+-------------+-------+
INFO - 16:23:54: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:54: +------+-------------+-------+-------------+-------+
INFO - 16:23:54: *** End AerodynamicsScenario execution (time: 0:00:00.015592) ***
INFO - 16:23:54: *** Start StructureScenario execution ***
INFO - 16:23:54: StructureScenario
INFO - 16:23:54: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:54: MDO formulation: MDF
INFO - 16:23:54: Optimization problem:
INFO - 16:23:54: minimize 0.001*-y_4(x_1)
INFO - 16:23:54: with respect to x_1
INFO - 16:23:54: under the inequality constraints
INFO - 16:23:54: g_1(x_1) <= 0
INFO - 16:23:54: over the design space:
INFO - 16:23:54: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:54: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:54: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:54: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:54: | x_1[1] | 0.75 | 0.7806436836764827 | 1.25 | float |
INFO - 16:23:54: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:54: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:54: 2%|▏ | 1/50 [00:00<00:00, 97.58 it/sec, feas=True, obj=-2.26]
INFO - 16:23:54: Optimization result:
INFO - 16:23:54: Optimizer info:
INFO - 16:23:54: Status: 8
INFO - 16:23:54: Message: Positive directional derivative for linesearch
INFO - 16:23:54: Solution:
INFO - 16:23:54: The solution is feasible.
INFO - 16:23:54: Objective: -2.2629808707273313
INFO - 16:23:54: Standardized constraints:
INFO - 16:23:54: g_1 = [-1.59589593e-03 -2.02868890e-03 -1.31333010e-02 -2.32802973e-02
INFO - 16:23:54: -3.14967236e-02 -2.40000000e-01 1.36557432e-14]
INFO - 16:23:54: Design space:
INFO - 16:23:54: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:54: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:54: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:54: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:54: | x_1[1] | 0.75 | 0.7806436836764827 | 1.25 | float |
INFO - 16:23:54: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:54: *** End StructureScenario execution (time: 0:00:00.012176) ***
INFO - 16:23:54: *** Start PropulsionScenario execution ***
INFO - 16:23:54: PropulsionScenario
INFO - 16:23:54: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:54: MDO formulation: MDF
INFO - 16:23:54: Optimization problem:
INFO - 16:23:54: minimize 0.001*-y_4(x_3)
INFO - 16:23:54: with respect to x_3
INFO - 16:23:54: under the inequality constraints
INFO - 16:23:54: g_3(x_3) <= 0
INFO - 16:23:54: over the design space:
INFO - 16:23:54: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:54: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:54: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:54: | x_3 | 0.1 | 0.1578996407261434 | 1 | float |
INFO - 16:23:54: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:54: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:54: 2%|▏ | 1/50 [00:00<00:00, 109.20 it/sec, feas=True, obj=-2.26]
INFO - 16:23:54: 4%|▍ | 2/50 [00:00<00:00, 143.96 it/sec, feas=True, obj=-2.26]
INFO - 16:23:54: 6%|▌ | 3/50 [00:00<00:00, 168.49 it/sec, feas=True, obj=-2.26]
INFO - 16:23:54: Optimization result:
INFO - 16:23:54: Optimizer info:
INFO - 16:23:54: Status: None
INFO - 16:23:54: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:54: Solution:
INFO - 16:23:54: The solution is feasible.
INFO - 16:23:54: Objective: -2.2629808707273313
INFO - 16:23:54: Standardized constraints:
INFO - 16:23:54: g_3 = [-8.35396332e-01 -1.64603668e-01 4.21884749e-15 -1.81703256e-01]
INFO - 16:23:54: Design space:
INFO - 16:23:54: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:54: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:54: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:54: | x_3 | 0.1 | 0.1578996407261434 | 1 | float |
INFO - 16:23:54: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:54: *** End PropulsionScenario execution (time: 0:00:00.019814) ***
INFO - 16:23:54: *** Start AerodynamicsScenario execution ***
INFO - 16:23:54: AerodynamicsScenario
INFO - 16:23:54: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:54: MDO formulation: MDF
INFO - 16:23:54: Optimization problem:
INFO - 16:23:54: minimize 0.001*-y_4(x_2)
INFO - 16:23:54: with respect to x_2
INFO - 16:23:54: under the inequality constraints
INFO - 16:23:54: g_2(x_2) <= 0
INFO - 16:23:54: over the design space:
INFO - 16:23:54: +------+-------------+-------+-------------+-------+
INFO - 16:23:54: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:54: +------+-------------+-------+-------------+-------+
INFO - 16:23:54: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:54: +------+-------------+-------+-------------+-------+
INFO - 16:23:54: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:54: 2%|▏ | 1/50 [00:00<00:00, 80.68 it/sec, feas=True, obj=-2.26]
INFO - 16:23:54: Optimization result:
INFO - 16:23:54: Optimizer info:
INFO - 16:23:54: Status: 8
INFO - 16:23:54: Message: Positive directional derivative for linesearch
INFO - 16:23:54: Solution:
INFO - 16:23:54: The solution is feasible.
INFO - 16:23:54: Objective: -2.2629808707273313
INFO - 16:23:54: Standardized constraints:
INFO - 16:23:54: g_2 = 2.220446049250313e-16
INFO - 16:23:54: Design space:
INFO - 16:23:54: +------+-------------+-------+-------------+-------+
INFO - 16:23:54: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:54: +------+-------------+-------+-------------+-------+
INFO - 16:23:54: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:54: +------+-------------+-------+-------------+-------+
INFO - 16:23:54: *** End AerodynamicsScenario execution (time: 0:00:00.014028) ***
INFO - 16:23:54: 67%|██████▋ | 67/100 [00:37<00:18, 1.80 it/sec, feas=True, obj=-2.26]
INFO - 16:23:54: *** Start PropulsionScenario execution ***
INFO - 16:23:54: PropulsionScenario
INFO - 16:23:54: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:54: MDO formulation: MDF
INFO - 16:23:54: Optimization problem:
INFO - 16:23:54: minimize 0.001*-y_4(x_3)
INFO - 16:23:54: with respect to x_3
INFO - 16:23:54: under the inequality constraints
INFO - 16:23:54: g_3(x_3) <= 0
INFO - 16:23:54: over the design space:
INFO - 16:23:54: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:54: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:54: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:54: | x_3 | 0.1 | 0.1578996407261434 | 1 | float |
INFO - 16:23:54: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:54: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:54: 2%|▏ | 1/50 [00:00<00:01, 39.90 it/sec, feas=True, obj=-2.24]
INFO - 16:23:54: 4%|▍ | 2/50 [00:00<00:01, 30.00 it/sec, feas=True, obj=-2.25]
INFO - 16:23:54: 6%|▌ | 3/50 [00:00<00:01, 32.95 it/sec, feas=True, obj=-2.25]
INFO - 16:23:54: 8%|▊ | 4/50 [00:00<00:01, 34.48 it/sec, feas=True, obj=-2.25]
INFO - 16:23:54: Optimization result:
INFO - 16:23:54: Optimizer info:
INFO - 16:23:54: Status: None
INFO - 16:23:54: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:54: Solution:
INFO - 16:23:54: The solution is feasible.
INFO - 16:23:54: Objective: -2.2458889825908797
INFO - 16:23:54: Standardized constraints:
INFO - 16:23:54: g_3 = [-8.35353332e-01 -1.64646668e-01 -1.44328993e-15 -1.81277458e-01]
INFO - 16:23:54: Design space:
INFO - 16:23:54: +------+-------------+-------------------+-------------+-------+
INFO - 16:23:54: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:54: +------+-------------+-------------------+-------------+-------+
INFO - 16:23:54: | x_3 | 0.1 | 0.158445273669383 | 1 | float |
INFO - 16:23:54: +------+-------------+-------------------+-------------+-------+
INFO - 16:23:54: *** End PropulsionScenario execution (time: 0:00:00.119315) ***
INFO - 16:23:54: *** Start AerodynamicsScenario execution ***
INFO - 16:23:54: AerodynamicsScenario
INFO - 16:23:54: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:54: MDO formulation: MDF
INFO - 16:23:54: Optimization problem:
INFO - 16:23:54: minimize 0.001*-y_4(x_2)
INFO - 16:23:54: with respect to x_2
INFO - 16:23:54: under the inequality constraints
INFO - 16:23:54: g_2(x_2) <= 0
INFO - 16:23:54: over the design space:
INFO - 16:23:54: +------+-------------+-------+-------------+-------+
INFO - 16:23:54: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:54: +------+-------------+-------+-------------+-------+
INFO - 16:23:54: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:54: +------+-------------+-------+-------------+-------+
INFO - 16:23:54: Solving optimization problem with algorithm SLSQP:
WARNING - 16:23:54: Optimization found no feasible point; the least infeasible point is selected.
INFO - 16:23:54: 2%|▏ | 1/50 [00:00<00:00, 74.45 it/sec, feas=False, obj=-2.25]
INFO - 16:23:54: Optimization result:
INFO - 16:23:54: Optimizer info:
INFO - 16:23:54: Status: 8
INFO - 16:23:54: Message: Positive directional derivative for linesearch
INFO - 16:23:54: Solution:
WARNING - 16:23:54: The solution is not feasible.
INFO - 16:23:54: Objective: -2.2458889825908797
INFO - 16:23:54: Standardized constraints:
INFO - 16:23:54: g_2 = 0.00044541176325818554
INFO - 16:23:54: Design space:
INFO - 16:23:54: +------+-------------+-------+-------------+-------+
INFO - 16:23:54: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:54: +------+-------------+-------+-------------+-------+
INFO - 16:23:54: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:54: +------+-------------+-------+-------------+-------+
INFO - 16:23:54: *** End AerodynamicsScenario execution (time: 0:00:00.015347) ***
INFO - 16:23:54: *** Start StructureScenario execution ***
INFO - 16:23:54: StructureScenario
INFO - 16:23:54: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:54: MDO formulation: MDF
INFO - 16:23:54: Optimization problem:
INFO - 16:23:54: minimize 0.001*-y_4(x_1)
INFO - 16:23:54: with respect to x_1
INFO - 16:23:54: under the inequality constraints
INFO - 16:23:54: g_1(x_1) <= 0
INFO - 16:23:54: over the design space:
INFO - 16:23:54: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:54: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:54: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:54: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:54: | x_1[1] | 0.75 | 0.7806436836764827 | 1.25 | float |
INFO - 16:23:54: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:54: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:54: 2%|▏ | 1/50 [00:00<00:00, 95.63 it/sec, feas=True, obj=-2.25]
INFO - 16:23:54: Optimization result:
INFO - 16:23:54: Optimizer info:
INFO - 16:23:54: Status: 8
INFO - 16:23:54: Message: Positive directional derivative for linesearch
INFO - 16:23:54: Solution:
INFO - 16:23:54: The solution is feasible.
INFO - 16:23:54: Objective: -2.2458889825908797
INFO - 16:23:54: Standardized constraints:
INFO - 16:23:54: g_1 = [-5.17155874e-03 -3.98904885e-03 -1.44447903e-02 -2.42532740e-02
INFO - 16:23:54: -3.22651959e-02 -2.40000000e-01 1.36557432e-14]
INFO - 16:23:54: Design space:
INFO - 16:23:54: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:54: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:54: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:54: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:54: | x_1[1] | 0.75 | 0.7806436836764827 | 1.25 | float |
INFO - 16:23:54: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:54: *** End StructureScenario execution (time: 0:00:00.012661) ***
INFO - 16:23:54: *** Start PropulsionScenario execution ***
INFO - 16:23:54: PropulsionScenario
INFO - 16:23:54: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:54: MDO formulation: MDF
INFO - 16:23:54: Optimization problem:
INFO - 16:23:54: minimize 0.001*-y_4(x_3)
INFO - 16:23:54: with respect to x_3
INFO - 16:23:54: under the inequality constraints
INFO - 16:23:54: g_3(x_3) <= 0
INFO - 16:23:54: over the design space:
INFO - 16:23:54: +------+-------------+-------------------+-------------+-------+
INFO - 16:23:54: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:54: +------+-------------+-------------------+-------------+-------+
INFO - 16:23:54: | x_3 | 0.1 | 0.158445273669383 | 1 | float |
INFO - 16:23:54: +------+-------------+-------------------+-------------+-------+
INFO - 16:23:54: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:54: 2%|▏ | 1/50 [00:00<00:00, 107.44 it/sec, feas=True, obj=-2.25]
INFO - 16:23:54: 4%|▍ | 2/50 [00:00<00:00, 141.74 it/sec, feas=True, obj=-2.25]
INFO - 16:23:54: 6%|▌ | 3/50 [00:00<00:00, 157.13 it/sec, feas=True, obj=-2.25]
INFO - 16:23:54: Optimization result:
INFO - 16:23:54: Optimizer info:
INFO - 16:23:54: Status: None
INFO - 16:23:54: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:54: Solution:
INFO - 16:23:54: The solution is feasible.
INFO - 16:23:54: Objective: -2.245888982590882
INFO - 16:23:54: Standardized constraints:
INFO - 16:23:54: g_3 = [-8.35353332e-01 -1.64646668e-01 8.65973959e-15 -1.81277458e-01]
INFO - 16:23:54: Design space:
INFO - 16:23:54: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:54: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:54: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:54: | x_3 | 0.1 | 0.1584452736693846 | 1 | float |
INFO - 16:23:54: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:54: *** End PropulsionScenario execution (time: 0:00:00.021419) ***
INFO - 16:23:54: *** Start AerodynamicsScenario execution ***
INFO - 16:23:54: AerodynamicsScenario
INFO - 16:23:54: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:54: MDO formulation: MDF
INFO - 16:23:54: Optimization problem:
INFO - 16:23:54: minimize 0.001*-y_4(x_2)
INFO - 16:23:54: with respect to x_2
INFO - 16:23:54: under the inequality constraints
INFO - 16:23:54: g_2(x_2) <= 0
INFO - 16:23:54: over the design space:
INFO - 16:23:54: +------+-------------+-------+-------------+-------+
INFO - 16:23:54: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:54: +------+-------------+-------+-------------+-------+
INFO - 16:23:54: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:54: +------+-------------+-------+-------------+-------+
INFO - 16:23:54: Solving optimization problem with algorithm SLSQP:
WARNING - 16:23:54: Optimization found no feasible point; the least infeasible point is selected.
INFO - 16:23:54: 2%|▏ | 1/50 [00:00<00:00, 77.79 it/sec, feas=False, obj=-2.25]
INFO - 16:23:54: Optimization result:
INFO - 16:23:54: Optimizer info:
INFO - 16:23:54: Status: 8
INFO - 16:23:54: Message: Positive directional derivative for linesearch
INFO - 16:23:54: Solution:
WARNING - 16:23:54: The solution is not feasible.
INFO - 16:23:54: Objective: -2.245888982590882
INFO - 16:23:54: Standardized constraints:
INFO - 16:23:54: g_2 = 0.00044541176325818554
INFO - 16:23:54: Design space:
INFO - 16:23:54: +------+-------------+-------+-------------+-------+
INFO - 16:23:54: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:54: +------+-------------+-------+-------------+-------+
INFO - 16:23:54: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:54: +------+-------------+-------+-------------+-------+
INFO - 16:23:54: *** End AerodynamicsScenario execution (time: 0:00:00.014335) ***
INFO - 16:23:54: *** Start StructureScenario execution ***
INFO - 16:23:54: StructureScenario
INFO - 16:23:54: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:54: MDO formulation: MDF
INFO - 16:23:54: Optimization problem:
INFO - 16:23:54: minimize 0.001*-y_4(x_1)
INFO - 16:23:54: with respect to x_1
INFO - 16:23:54: under the inequality constraints
INFO - 16:23:54: g_1(x_1) <= 0
INFO - 16:23:54: over the design space:
INFO - 16:23:54: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:54: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:54: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:54: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:54: | x_1[1] | 0.75 | 0.7806436836764827 | 1.25 | float |
INFO - 16:23:54: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:54: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:54: 2%|▏ | 1/50 [00:00<00:00, 101.26 it/sec, feas=True, obj=-2.25]
INFO - 16:23:54: Optimization result:
INFO - 16:23:54: Optimizer info:
INFO - 16:23:54: Status: 8
INFO - 16:23:54: Message: Positive directional derivative for linesearch
INFO - 16:23:54: Solution:
INFO - 16:23:54: The solution is feasible.
INFO - 16:23:54: Objective: -2.245888982590882
INFO - 16:23:54: Standardized constraints:
INFO - 16:23:54: g_1 = [-5.17155874e-03 -3.98904885e-03 -1.44447903e-02 -2.42532740e-02
INFO - 16:23:54: -3.22651959e-02 -2.40000000e-01 1.36557432e-14]
INFO - 16:23:54: Design space:
INFO - 16:23:54: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:54: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:54: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:54: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:54: | x_1[1] | 0.75 | 0.7806436836764827 | 1.25 | float |
INFO - 16:23:54: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:54: *** End StructureScenario execution (time: 0:00:00.011832) ***
INFO - 16:23:54: 68%|██████▊ | 68/100 [00:37<00:17, 1.81 it/sec, feas=False, obj=-2.25]
INFO - 16:23:54: *** Start PropulsionScenario execution ***
INFO - 16:23:54: PropulsionScenario
INFO - 16:23:54: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:54: MDO formulation: MDF
INFO - 16:23:54: Optimization problem:
INFO - 16:23:54: minimize 0.001*-y_4(x_3)
INFO - 16:23:54: with respect to x_3
INFO - 16:23:54: under the inequality constraints
INFO - 16:23:54: g_3(x_3) <= 0
INFO - 16:23:54: over the design space:
INFO - 16:23:54: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:54: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:54: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:54: | x_3 | 0.1 | 0.1584452736693846 | 1 | float |
INFO - 16:23:54: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:54: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:54: 2%|▏ | 1/50 [00:00<00:01, 37.25 it/sec, feas=False, obj=-2.26]
INFO - 16:23:54: 4%|▍ | 2/50 [00:00<00:01, 37.99 it/sec, feas=True, obj=-2.26]
INFO - 16:23:54: 6%|▌ | 3/50 [00:00<00:01, 32.19 it/sec, feas=False, obj=-2.26]
INFO - 16:23:54: 8%|▊ | 4/50 [00:00<00:01, 29.68 it/sec, feas=True, obj=-2.26]
INFO - 16:23:54: 10%|█ | 5/50 [00:00<00:01, 31.36 it/sec, feas=True, obj=-2.26]
INFO - 16:23:54: 12%|█▏ | 6/50 [00:00<00:01, 32.39 it/sec, feas=True, obj=-2.26]
INFO - 16:23:54: Optimization result:
INFO - 16:23:54: Optimizer info:
INFO - 16:23:54: Status: None
INFO - 16:23:54: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:54: Solution:
INFO - 16:23:54: The solution is feasible.
INFO - 16:23:54: Objective: -2.2630941349492284
INFO - 16:23:54: Standardized constraints:
INFO - 16:23:54: g_3 = [-8.36212497e-01 -1.63787503e-01 1.88737914e-14 -1.81729821e-01]
INFO - 16:23:54: Design space:
INFO - 16:23:54: +------+-------------+-------------------+-------------+-------+
INFO - 16:23:54: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:54: +------+-------------+-------------------+-------------+-------+
INFO - 16:23:54: | x_3 | 0.1 | 0.157871041997244 | 1 | float |
INFO - 16:23:54: +------+-------------+-------------------+-------------+-------+
INFO - 16:23:54: *** End PropulsionScenario execution (time: 0:00:00.187597) ***
INFO - 16:23:54: *** Start AerodynamicsScenario execution ***
INFO - 16:23:54: AerodynamicsScenario
INFO - 16:23:54: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:54: MDO formulation: MDF
INFO - 16:23:54: Optimization problem:
INFO - 16:23:54: minimize 0.001*-y_4(x_2)
INFO - 16:23:54: with respect to x_2
INFO - 16:23:54: under the inequality constraints
INFO - 16:23:54: g_2(x_2) <= 0
INFO - 16:23:54: over the design space:
INFO - 16:23:54: +------+-------------+-------+-------------+-------+
INFO - 16:23:54: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:54: +------+-------------+-------+-------------+-------+
INFO - 16:23:54: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:54: +------+-------------+-------+-------------+-------+
INFO - 16:23:54: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:54: 2%|▏ | 1/50 [00:00<00:00, 67.15 it/sec, feas=True, obj=-2.26]
INFO - 16:23:54: Optimization result:
INFO - 16:23:54: Optimizer info:
INFO - 16:23:54: Status: 8
INFO - 16:23:54: Message: Positive directional derivative for linesearch
INFO - 16:23:54: Solution:
INFO - 16:23:54: The solution is feasible.
INFO - 16:23:54: Objective: -2.2630941349492284
INFO - 16:23:54: Standardized constraints:
INFO - 16:23:54: g_2 = 0.0
INFO - 16:23:54: Design space:
INFO - 16:23:54: +------+-------------+-------+-------------+-------+
INFO - 16:23:54: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:54: +------+-------------+-------+-------------+-------+
INFO - 16:23:54: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:54: +------+-------------+-------+-------------+-------+
INFO - 16:23:54: *** End AerodynamicsScenario execution (time: 0:00:00.016555) ***
INFO - 16:23:54: *** Start StructureScenario execution ***
INFO - 16:23:54: StructureScenario
INFO - 16:23:54: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:54: MDO formulation: MDF
INFO - 16:23:54: Optimization problem:
INFO - 16:23:54: minimize 0.001*-y_4(x_1)
INFO - 16:23:54: with respect to x_1
INFO - 16:23:54: under the inequality constraints
INFO - 16:23:54: g_1(x_1) <= 0
INFO - 16:23:54: over the design space:
INFO - 16:23:54: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:54: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:54: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:54: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:54: | x_1[1] | 0.75 | 0.7806436836764827 | 1.25 | float |
INFO - 16:23:54: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:54: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:54: 2%|▏ | 1/50 [00:00<00:00, 82.37 it/sec, feas=True, obj=-2.26]
INFO - 16:23:54: Optimization result:
INFO - 16:23:54: Optimizer info:
INFO - 16:23:54: Status: 8
INFO - 16:23:54: Message: Positive directional derivative for linesearch
INFO - 16:23:54: Solution:
INFO - 16:23:54: The solution is feasible.
INFO - 16:23:54: Objective: -2.2630941349492284
INFO - 16:23:54: Standardized constraints:
INFO - 16:23:54: g_1 = [-1.59589593e-03 -2.02868890e-03 -1.31333010e-02 -2.32802973e-02
INFO - 16:23:54: -3.14967236e-02 -2.40000000e-01 1.36557432e-14]
INFO - 16:23:54: Design space:
INFO - 16:23:54: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:54: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:54: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:54: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:54: | x_1[1] | 0.75 | 0.7806436836764827 | 1.25 | float |
INFO - 16:23:54: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:54: *** End StructureScenario execution (time: 0:00:00.014410) ***
INFO - 16:23:54: *** Start PropulsionScenario execution ***
INFO - 16:23:54: PropulsionScenario
INFO - 16:23:54: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:54: MDO formulation: MDF
INFO - 16:23:54: Optimization problem:
INFO - 16:23:54: minimize 0.001*-y_4(x_3)
INFO - 16:23:54: with respect to x_3
INFO - 16:23:54: under the inequality constraints
INFO - 16:23:54: g_3(x_3) <= 0
INFO - 16:23:54: over the design space:
INFO - 16:23:54: +------+-------------+-------------------+-------------+-------+
INFO - 16:23:54: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:54: +------+-------------+-------------------+-------------+-------+
INFO - 16:23:54: | x_3 | 0.1 | 0.157871041997244 | 1 | float |
INFO - 16:23:54: +------+-------------+-------------------+-------------+-------+
INFO - 16:23:54: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:54: 2%|▏ | 1/50 [00:00<00:00, 110.66 it/sec, feas=True, obj=-2.26]
INFO - 16:23:54: 4%|▍ | 2/50 [00:00<00:00, 146.15 it/sec, feas=True, obj=-2.26]
INFO - 16:23:54: 6%|▌ | 3/50 [00:00<00:00, 170.97 it/sec, feas=True, obj=-2.26]
INFO - 16:23:54: Optimization result:
INFO - 16:23:54: Optimizer info:
INFO - 16:23:54: Status: None
INFO - 16:23:54: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:54: Solution:
INFO - 16:23:54: The solution is feasible.
INFO - 16:23:54: Objective: -2.2630941349492284
INFO - 16:23:54: Standardized constraints:
INFO - 16:23:54: g_3 = [-8.36212497e-01 -1.63787503e-01 1.88737914e-14 -1.81729821e-01]
INFO - 16:23:54: Design space:
INFO - 16:23:54: +------+-------------+-------------------+-------------+-------+
INFO - 16:23:54: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:54: +------+-------------+-------------------+-------------+-------+
INFO - 16:23:54: | x_3 | 0.1 | 0.157871041997244 | 1 | float |
INFO - 16:23:54: +------+-------------+-------------------+-------------+-------+
INFO - 16:23:54: *** End PropulsionScenario execution (time: 0:00:00.019832) ***
INFO - 16:23:54: *** Start AerodynamicsScenario execution ***
INFO - 16:23:54: AerodynamicsScenario
INFO - 16:23:54: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:54: MDO formulation: MDF
INFO - 16:23:54: Optimization problem:
INFO - 16:23:54: minimize 0.001*-y_4(x_2)
INFO - 16:23:54: with respect to x_2
INFO - 16:23:54: under the inequality constraints
INFO - 16:23:54: g_2(x_2) <= 0
INFO - 16:23:54: over the design space:
INFO - 16:23:54: +------+-------------+-------+-------------+-------+
INFO - 16:23:54: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:54: +------+-------------+-------+-------------+-------+
INFO - 16:23:54: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:54: +------+-------------+-------+-------------+-------+
INFO - 16:23:54: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:54: 2%|▏ | 1/50 [00:00<00:00, 80.82 it/sec, feas=True, obj=-2.26]
INFO - 16:23:54: Optimization result:
INFO - 16:23:54: Optimizer info:
INFO - 16:23:54: Status: 8
INFO - 16:23:54: Message: Positive directional derivative for linesearch
INFO - 16:23:54: Solution:
INFO - 16:23:54: The solution is feasible.
INFO - 16:23:54: Objective: -2.2630941349492284
INFO - 16:23:54: Standardized constraints:
INFO - 16:23:54: g_2 = 0.0
INFO - 16:23:54: Design space:
INFO - 16:23:54: +------+-------------+-------+-------------+-------+
INFO - 16:23:54: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:54: +------+-------------+-------+-------------+-------+
INFO - 16:23:54: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:54: +------+-------------+-------+-------------+-------+
INFO - 16:23:54: *** End AerodynamicsScenario execution (time: 0:00:00.014079) ***
INFO - 16:23:54: *** Start StructureScenario execution ***
INFO - 16:23:54: StructureScenario
INFO - 16:23:54: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:54: MDO formulation: MDF
INFO - 16:23:54: Optimization problem:
INFO - 16:23:54: minimize 0.001*-y_4(x_1)
INFO - 16:23:54: with respect to x_1
INFO - 16:23:54: under the inequality constraints
INFO - 16:23:54: g_1(x_1) <= 0
INFO - 16:23:54: over the design space:
INFO - 16:23:54: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:54: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:54: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:54: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:54: | x_1[1] | 0.75 | 0.7806436836764827 | 1.25 | float |
INFO - 16:23:54: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:54: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:54: 2%|▏ | 1/50 [00:00<00:00, 102.38 it/sec, feas=True, obj=-2.26]
INFO - 16:23:54: Optimization result:
INFO - 16:23:54: Optimizer info:
INFO - 16:23:54: Status: 8
INFO - 16:23:54: Message: Positive directional derivative for linesearch
INFO - 16:23:54: Solution:
INFO - 16:23:54: The solution is feasible.
INFO - 16:23:54: Objective: -2.2630941349492284
INFO - 16:23:54: Standardized constraints:
INFO - 16:23:54: g_1 = [-1.59589593e-03 -2.02868890e-03 -1.31333010e-02 -2.32802973e-02
INFO - 16:23:54: -3.14967236e-02 -2.40000000e-01 1.36557432e-14]
INFO - 16:23:54: Design space:
INFO - 16:23:54: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:54: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:54: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:54: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:54: | x_1[1] | 0.75 | 0.7806436836764827 | 1.25 | float |
INFO - 16:23:54: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:54: *** End StructureScenario execution (time: 0:00:00.011803) ***
INFO - 16:23:54: 69%|██████▉ | 69/100 [00:37<00:16, 1.82 it/sec, feas=True, obj=-2.26]
INFO - 16:23:54: *** Start PropulsionScenario execution ***
INFO - 16:23:54: PropulsionScenario
INFO - 16:23:54: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:54: MDO formulation: MDF
INFO - 16:23:54: Optimization problem:
INFO - 16:23:54: minimize 0.001*-y_4(x_3)
INFO - 16:23:54: with respect to x_3
INFO - 16:23:54: under the inequality constraints
INFO - 16:23:54: g_3(x_3) <= 0
INFO - 16:23:54: over the design space:
INFO - 16:23:54: +------+-------------+-------------------+-------------+-------+
INFO - 16:23:54: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:54: +------+-------------+-------------------+-------------+-------+
INFO - 16:23:54: | x_3 | 0.1 | 0.157871041997244 | 1 | float |
INFO - 16:23:54: +------+-------------+-------------------+-------------+-------+
INFO - 16:23:54: Solving optimization problem with algorithm SLSQP:
WARNING - 16:23:54: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 6.724932466608626e-05 is still above the tolerance 1e-06.
INFO - 16:23:54: 2%|▏ | 1/50 [00:00<00:01, 34.17 it/sec, feas=True, obj=-2.25]
INFO - 16:23:54: 4%|▍ | 2/50 [00:00<00:01, 27.62 it/sec, feas=True, obj=-2.25]
INFO - 16:23:54: 6%|▌ | 3/50 [00:00<00:01, 31.00 it/sec, feas=True, obj=-2.25]
INFO - 16:23:54: 8%|▊ | 4/50 [00:00<00:01, 32.55 it/sec, feas=True, obj=-2.25]
INFO - 16:23:54: Optimization result:
INFO - 16:23:54: Optimizer info:
INFO - 16:23:54: Status: None
INFO - 16:23:54: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:54: Solution:
INFO - 16:23:54: The solution is feasible.
INFO - 16:23:54: Objective: -2.2462437877714003
INFO - 16:23:54: Standardized constraints:
INFO - 16:23:54: g_3 = [-8.35432907e-01 -1.64567093e-01 6.43929354e-15 -1.81314272e-01]
INFO - 16:23:54: Design space:
INFO - 16:23:54: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:54: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:54: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:54: | x_3 | 0.1 | 0.1584472365631759 | 1 | float |
INFO - 16:23:54: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:54: *** End PropulsionScenario execution (time: 0:00:00.125257) ***
INFO - 16:23:54: *** Start AerodynamicsScenario execution ***
INFO - 16:23:54: AerodynamicsScenario
INFO - 16:23:54: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:54: MDO formulation: MDF
INFO - 16:23:54: Optimization problem:
INFO - 16:23:54: minimize 0.001*-y_4(x_2)
INFO - 16:23:54: with respect to x_2
INFO - 16:23:54: under the inequality constraints
INFO - 16:23:54: g_2(x_2) <= 0
INFO - 16:23:54: over the design space:
INFO - 16:23:54: +------+-------------+-------+-------------+-------+
INFO - 16:23:54: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:54: +------+-------------+-------+-------------+-------+
INFO - 16:23:54: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:54: +------+-------------+-------+-------------+-------+
INFO - 16:23:54: Solving optimization problem with algorithm SLSQP:
WARNING - 16:23:54: Optimization found no feasible point; the least infeasible point is selected.
INFO - 16:23:54: 2%|▏ | 1/50 [00:00<00:00, 65.60 it/sec, feas=False, obj=-2.25]
INFO - 16:23:54: Optimization result:
INFO - 16:23:54: Optimizer info:
INFO - 16:23:54: Status: 8
INFO - 16:23:54: Message: Positive directional derivative for linesearch
INFO - 16:23:54: Solution:
WARNING - 16:23:54: The solution is not feasible.
INFO - 16:23:54: Objective: -2.2462437877714003
INFO - 16:23:54: Standardized constraints:
INFO - 16:23:54: g_2 = 0.00015747453962910996
INFO - 16:23:54: Design space:
INFO - 16:23:54: +------+-------------+-------+-------------+-------+
INFO - 16:23:54: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:54: +------+-------------+-------+-------------+-------+
INFO - 16:23:54: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:54: +------+-------------+-------+-------------+-------+
INFO - 16:23:54: *** End AerodynamicsScenario execution (time: 0:00:00.016928) ***
INFO - 16:23:54: *** Start StructureScenario execution ***
INFO - 16:23:54: StructureScenario
INFO - 16:23:54: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:54: MDO formulation: MDF
INFO - 16:23:54: Optimization problem:
INFO - 16:23:54: minimize 0.001*-y_4(x_1)
INFO - 16:23:54: with respect to x_1
INFO - 16:23:54: under the inequality constraints
INFO - 16:23:54: g_1(x_1) <= 0
INFO - 16:23:54: over the design space:
INFO - 16:23:54: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:54: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:54: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:54: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:54: | x_1[1] | 0.75 | 0.7806436836764827 | 1.25 | float |
INFO - 16:23:54: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:54: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:54: 2%|▏ | 1/50 [00:00<00:00, 97.43 it/sec, feas=True, obj=-2.25]
INFO - 16:23:54: Optimization result:
INFO - 16:23:54: Optimizer info:
INFO - 16:23:54: Status: 8
INFO - 16:23:54: Message: Positive directional derivative for linesearch
INFO - 16:23:54: Solution:
INFO - 16:23:54: The solution is feasible.
INFO - 16:23:54: Objective: -2.2462437877714003
INFO - 16:23:54: Standardized constraints:
INFO - 16:23:54: g_1 = [-2.85864822e-03 -2.72114093e-03 -1.35966215e-02 -2.36240648e-02
INFO - 16:23:54: -3.17682582e-02 -2.40000000e-01 1.36557432e-14]
INFO - 16:23:54: Design space:
INFO - 16:23:54: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:54: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:54: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:54: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:54: | x_1[1] | 0.75 | 0.7806436836764827 | 1.25 | float |
INFO - 16:23:54: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:54: *** End StructureScenario execution (time: 0:00:00.012353) ***
INFO - 16:23:54: *** Start PropulsionScenario execution ***
INFO - 16:23:54: PropulsionScenario
INFO - 16:23:54: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:54: MDO formulation: MDF
INFO - 16:23:54: Optimization problem:
INFO - 16:23:54: minimize 0.001*-y_4(x_3)
INFO - 16:23:54: with respect to x_3
INFO - 16:23:54: under the inequality constraints
INFO - 16:23:54: g_3(x_3) <= 0
INFO - 16:23:54: over the design space:
INFO - 16:23:54: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:54: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:54: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:54: | x_3 | 0.1 | 0.1584472365631759 | 1 | float |
INFO - 16:23:54: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:54: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:54: 2%|▏ | 1/50 [00:00<00:00, 108.72 it/sec, feas=True, obj=-2.25]
INFO - 16:23:54: Optimization result:
INFO - 16:23:54: Optimizer info:
INFO - 16:23:54: Status: 8
INFO - 16:23:54: Message: Positive directional derivative for linesearch
INFO - 16:23:54: Solution:
INFO - 16:23:54: The solution is feasible.
INFO - 16:23:54: Objective: -2.2462437877714003
INFO - 16:23:54: Standardized constraints:
INFO - 16:23:54: g_3 = [-8.35432907e-01 -1.64567093e-01 6.43929354e-15 -1.81314272e-01]
INFO - 16:23:54: Design space:
INFO - 16:23:54: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:54: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:54: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:54: | x_3 | 0.1 | 0.1584472365631759 | 1 | float |
INFO - 16:23:54: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:54: *** End PropulsionScenario execution (time: 0:00:00.011033) ***
INFO - 16:23:54: *** Start AerodynamicsScenario execution ***
INFO - 16:23:54: AerodynamicsScenario
INFO - 16:23:54: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:54: MDO formulation: MDF
INFO - 16:23:54: Optimization problem:
INFO - 16:23:54: minimize 0.001*-y_4(x_2)
INFO - 16:23:54: with respect to x_2
INFO - 16:23:54: under the inequality constraints
INFO - 16:23:54: g_2(x_2) <= 0
INFO - 16:23:54: over the design space:
INFO - 16:23:54: +------+-------------+-------+-------------+-------+
INFO - 16:23:54: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:54: +------+-------------+-------+-------------+-------+
INFO - 16:23:54: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:54: +------+-------------+-------+-------------+-------+
INFO - 16:23:54: Solving optimization problem with algorithm SLSQP:
WARNING - 16:23:54: Optimization found no feasible point; the least infeasible point is selected.
INFO - 16:23:54: 2%|▏ | 1/50 [00:00<00:00, 87.60 it/sec, feas=False, obj=-2.25]
INFO - 16:23:54: Optimization result:
INFO - 16:23:54: Optimizer info:
INFO - 16:23:54: Status: 8
INFO - 16:23:54: Message: Positive directional derivative for linesearch
INFO - 16:23:54: Solution:
WARNING - 16:23:54: The solution is not feasible.
INFO - 16:23:54: Objective: -2.2462437877714003
INFO - 16:23:54: Standardized constraints:
INFO - 16:23:54: g_2 = 0.00015747453962910996
INFO - 16:23:54: Design space:
INFO - 16:23:54: +------+-------------+-------+-------------+-------+
INFO - 16:23:54: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:54: +------+-------------+-------+-------------+-------+
INFO - 16:23:54: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:54: +------+-------------+-------+-------------+-------+
INFO - 16:23:54: *** End AerodynamicsScenario execution (time: 0:00:00.013033) ***
INFO - 16:23:54: 70%|███████ | 70/100 [00:38<00:16, 1.84 it/sec, feas=False, obj=-2.25]
INFO - 16:23:54: *** Start PropulsionScenario execution ***
INFO - 16:23:54: PropulsionScenario
INFO - 16:23:54: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:54: MDO formulation: MDF
INFO - 16:23:54: Optimization problem:
INFO - 16:23:54: minimize 0.001*-y_4(x_3)
INFO - 16:23:54: with respect to x_3
INFO - 16:23:54: under the inequality constraints
INFO - 16:23:54: g_3(x_3) <= 0
INFO - 16:23:54: over the design space:
INFO - 16:23:54: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:54: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:54: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:54: | x_3 | 0.1 | 0.1584472365631759 | 1 | float |
INFO - 16:23:54: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:54: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:54: 2%|▏ | 1/50 [00:00<00:01, 38.60 it/sec, feas=False, obj=-2.26]
INFO - 16:23:54: 4%|▍ | 2/50 [00:00<00:01, 39.82 it/sec, feas=True, obj=-2.26]
INFO - 16:23:55: 6%|▌ | 3/50 [00:00<00:01, 32.61 it/sec, feas=False, obj=-2.26]
INFO - 16:23:55: 8%|▊ | 4/50 [00:00<00:01, 29.87 it/sec, feas=True, obj=-2.26]
INFO - 16:23:55: 10%|█ | 5/50 [00:00<00:01, 28.42 it/sec, feas=True, obj=-2.26]
INFO - 16:23:55: 12%|█▏ | 6/50 [00:00<00:01, 29.89 it/sec, feas=True, obj=-2.26]
INFO - 16:23:55: Optimization result:
INFO - 16:23:55: Optimizer info:
INFO - 16:23:55: Status: None
INFO - 16:23:55: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:55: Solution:
INFO - 16:23:55: The solution is feasible.
INFO - 16:23:55: Objective: -2.2627440472782765
INFO - 16:23:55: Standardized constraints:
INFO - 16:23:55: g_3 = [-8.36367623e-01 -1.63632377e-01 5.10702591e-15 -1.81750381e-01]
INFO - 16:23:55: Design space:
INFO - 16:23:55: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:55: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:55: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:55: | x_3 | 0.1 | 0.1578489130007868 | 1 | float |
INFO - 16:23:55: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:55: *** End PropulsionScenario execution (time: 0:00:00.203332) ***
INFO - 16:23:55: *** Start AerodynamicsScenario execution ***
INFO - 16:23:55: AerodynamicsScenario
INFO - 16:23:55: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:55: MDO formulation: MDF
INFO - 16:23:55: Optimization problem:
INFO - 16:23:55: minimize 0.001*-y_4(x_2)
INFO - 16:23:55: with respect to x_2
INFO - 16:23:55: under the inequality constraints
INFO - 16:23:55: g_2(x_2) <= 0
INFO - 16:23:55: over the design space:
INFO - 16:23:55: +------+-------------+-------+-------------+-------+
INFO - 16:23:55: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:55: +------+-------------+-------+-------------+-------+
INFO - 16:23:55: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:55: +------+-------------+-------+-------------+-------+
INFO - 16:23:55: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:55: 2%|▏ | 1/50 [00:00<00:00, 90.31 it/sec, feas=True, obj=-2.26]
INFO - 16:23:55: Optimization result:
INFO - 16:23:55: Optimizer info:
INFO - 16:23:55: Status: 8
INFO - 16:23:55: Message: Positive directional derivative for linesearch
INFO - 16:23:55: Solution:
INFO - 16:23:55: The solution is feasible.
INFO - 16:23:55: Objective: -2.2627440472782765
INFO - 16:23:55: Standardized constraints:
INFO - 16:23:55: g_2 = -2.220446049250313e-16
INFO - 16:23:55: Design space:
INFO - 16:23:55: +------+-------------+-------+-------------+-------+
INFO - 16:23:55: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:55: +------+-------------+-------+-------------+-------+
INFO - 16:23:55: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:55: +------+-------------+-------+-------------+-------+
INFO - 16:23:55: *** End AerodynamicsScenario execution (time: 0:00:00.012691) ***
INFO - 16:23:55: *** Start StructureScenario execution ***
INFO - 16:23:55: StructureScenario
INFO - 16:23:55: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:55: MDO formulation: MDF
INFO - 16:23:55: Optimization problem:
INFO - 16:23:55: minimize 0.001*-y_4(x_1)
INFO - 16:23:55: with respect to x_1
INFO - 16:23:55: under the inequality constraints
INFO - 16:23:55: g_1(x_1) <= 0
INFO - 16:23:55: over the design space:
INFO - 16:23:55: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:55: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:55: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:55: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:55: | x_1[1] | 0.75 | 0.7806436836764827 | 1.25 | float |
INFO - 16:23:55: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:55: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:55: 2%|▏ | 1/50 [00:00<00:00, 97.40 it/sec, feas=True, obj=-2.26]
INFO - 16:23:55: Optimization result:
INFO - 16:23:55: Optimizer info:
INFO - 16:23:55: Status: 8
INFO - 16:23:55: Message: Positive directional derivative for linesearch
INFO - 16:23:55: Solution:
INFO - 16:23:55: The solution is feasible.
INFO - 16:23:55: Objective: -2.2627440472782765
INFO - 16:23:55: Standardized constraints:
INFO - 16:23:55: g_1 = [-1.59589593e-03 -2.02868890e-03 -1.31333010e-02 -2.32802973e-02
INFO - 16:23:55: -3.14967236e-02 -2.40000000e-01 1.36557432e-14]
INFO - 16:23:55: Design space:
INFO - 16:23:55: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:55: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:55: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:55: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:55: | x_1[1] | 0.75 | 0.7806436836764827 | 1.25 | float |
INFO - 16:23:55: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:55: *** End StructureScenario execution (time: 0:00:00.012343) ***
INFO - 16:23:55: *** Start PropulsionScenario execution ***
INFO - 16:23:55: PropulsionScenario
INFO - 16:23:55: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:55: MDO formulation: MDF
INFO - 16:23:55: Optimization problem:
INFO - 16:23:55: minimize 0.001*-y_4(x_3)
INFO - 16:23:55: with respect to x_3
INFO - 16:23:55: under the inequality constraints
INFO - 16:23:55: g_3(x_3) <= 0
INFO - 16:23:55: over the design space:
INFO - 16:23:55: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:55: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:55: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:55: | x_3 | 0.1 | 0.1578489130007868 | 1 | float |
INFO - 16:23:55: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:55: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:55: 2%|▏ | 1/50 [00:00<00:00, 109.44 it/sec, feas=True, obj=-2.26]
INFO - 16:23:55: Optimization result:
INFO - 16:23:55: Optimizer info:
INFO - 16:23:55: Status: 8
INFO - 16:23:55: Message: Positive directional derivative for linesearch
INFO - 16:23:55: Solution:
INFO - 16:23:55: The solution is feasible.
INFO - 16:23:55: Objective: -2.2627440472782765
INFO - 16:23:55: Standardized constraints:
INFO - 16:23:55: g_3 = [-8.36367623e-01 -1.63632377e-01 5.10702591e-15 -1.81750381e-01]
INFO - 16:23:55: Design space:
INFO - 16:23:55: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:55: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:55: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:55: | x_3 | 0.1 | 0.1578489130007868 | 1 | float |
INFO - 16:23:55: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:55: *** End PropulsionScenario execution (time: 0:00:00.010815) ***
INFO - 16:23:55: 71%|███████ | 71/100 [00:38<00:15, 1.85 it/sec, feas=True, obj=-2.26]
INFO - 16:23:55: *** Start PropulsionScenario execution ***
INFO - 16:23:55: PropulsionScenario
INFO - 16:23:55: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:55: MDO formulation: MDF
INFO - 16:23:55: Optimization problem:
INFO - 16:23:55: minimize 0.001*-y_4(x_3)
INFO - 16:23:55: with respect to x_3
INFO - 16:23:55: under the inequality constraints
INFO - 16:23:55: g_3(x_3) <= 0
INFO - 16:23:55: over the design space:
INFO - 16:23:55: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:55: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:55: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:55: | x_3 | 0.1 | 0.1578489130007868 | 1 | float |
INFO - 16:23:55: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:55: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:55: 2%|▏ | 1/50 [00:00<00:01, 38.59 it/sec, feas=True, obj=-2.24]
INFO - 16:23:55: 4%|▍ | 2/50 [00:00<00:01, 29.69 it/sec, feas=True, obj=-2.25]
INFO - 16:23:55: 6%|▌ | 3/50 [00:00<00:01, 27.49 it/sec, feas=True, obj=-2.25]
INFO - 16:23:55: 8%|▊ | 4/50 [00:00<00:01, 29.38 it/sec, feas=True, obj=-2.25]
INFO - 16:23:55: Optimization result:
INFO - 16:23:55: Optimizer info:
INFO - 16:23:55: Status: None
INFO - 16:23:55: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:55: Solution:
INFO - 16:23:55: The solution is feasible.
INFO - 16:23:55: Objective: -2.2456645030762257
INFO - 16:23:55: Standardized constraints:
INFO - 16:23:55: g_3 = [-8.35563399e-01 -1.64436601e-01 8.88178420e-16 -1.81271168e-01]
INFO - 16:23:55: Design space:
INFO - 16:23:55: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:55: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:55: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:55: | x_3 | 0.1 | 0.1584554058636569 | 1 | float |
INFO - 16:23:55: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:55: *** End PropulsionScenario execution (time: 0:00:00.138383) ***
INFO - 16:23:55: *** Start AerodynamicsScenario execution ***
INFO - 16:23:55: AerodynamicsScenario
INFO - 16:23:55: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:55: MDO formulation: MDF
INFO - 16:23:55: Optimization problem:
INFO - 16:23:55: minimize 0.001*-y_4(x_2)
INFO - 16:23:55: with respect to x_2
INFO - 16:23:55: under the inequality constraints
INFO - 16:23:55: g_2(x_2) <= 0
INFO - 16:23:55: over the design space:
INFO - 16:23:55: +------+-------------+-------+-------------+-------+
INFO - 16:23:55: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:55: +------+-------------+-------+-------------+-------+
INFO - 16:23:55: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:55: +------+-------------+-------+-------------+-------+
INFO - 16:23:55: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:55: 2%|▏ | 1/50 [00:00<00:00, 92.03 it/sec, feas=True, obj=-2.25]
INFO - 16:23:55: Optimization result:
INFO - 16:23:55: Optimizer info:
INFO - 16:23:55: Status: 8
INFO - 16:23:55: Message: Positive directional derivative for linesearch
INFO - 16:23:55: Solution:
INFO - 16:23:55: The solution is feasible.
INFO - 16:23:55: Objective: -2.2456645030762257
INFO - 16:23:55: Standardized constraints:
INFO - 16:23:55: g_2 = 6.698384737613416e-05
INFO - 16:23:55: Design space:
INFO - 16:23:55: +------+-------------+-------+-------------+-------+
INFO - 16:23:55: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:55: +------+-------------+-------+-------------+-------+
INFO - 16:23:55: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:55: +------+-------------+-------+-------------+-------+
INFO - 16:23:55: *** End AerodynamicsScenario execution (time: 0:00:00.012414) ***
INFO - 16:23:55: *** Start StructureScenario execution ***
INFO - 16:23:55: StructureScenario
INFO - 16:23:55: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:55: MDO formulation: MDF
INFO - 16:23:55: Optimization problem:
INFO - 16:23:55: minimize 0.001*-y_4(x_1)
INFO - 16:23:55: with respect to x_1
INFO - 16:23:55: under the inequality constraints
INFO - 16:23:55: g_1(x_1) <= 0
INFO - 16:23:55: over the design space:
INFO - 16:23:55: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:55: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:55: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:55: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:55: | x_1[1] | 0.75 | 0.7806436836764827 | 1.25 | float |
INFO - 16:23:55: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:55: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:55: 2%|▏ | 1/50 [00:00<00:00, 98.24 it/sec, feas=True, obj=-2.25]
INFO - 16:23:55: Optimization result:
INFO - 16:23:55: Optimizer info:
INFO - 16:23:55: Status: 8
INFO - 16:23:55: Message: Positive directional derivative for linesearch
INFO - 16:23:55: Solution:
INFO - 16:23:55: The solution is feasible.
INFO - 16:23:55: Objective: -2.2456645030762257
INFO - 16:23:55: Standardized constraints:
INFO - 16:23:55: g_1 = [-2.13283465e-03 -2.32314821e-03 -1.33303331e-02 -2.34264930e-02
INFO - 16:23:55: -3.16122033e-02 -2.40000000e-01 1.36557432e-14]
INFO - 16:23:55: Design space:
INFO - 16:23:55: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:55: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:55: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:55: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:55: | x_1[1] | 0.75 | 0.7806436836764827 | 1.25 | float |
INFO - 16:23:55: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:55: *** End StructureScenario execution (time: 0:00:00.012235) ***
INFO - 16:23:55: *** Start PropulsionScenario execution ***
INFO - 16:23:55: PropulsionScenario
INFO - 16:23:55: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:55: MDO formulation: MDF
INFO - 16:23:55: Optimization problem:
INFO - 16:23:55: minimize 0.001*-y_4(x_3)
INFO - 16:23:55: with respect to x_3
INFO - 16:23:55: under the inequality constraints
INFO - 16:23:55: g_3(x_3) <= 0
INFO - 16:23:55: over the design space:
INFO - 16:23:55: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:55: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:55: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:55: | x_3 | 0.1 | 0.1584554058636569 | 1 | float |
INFO - 16:23:55: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:55: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:55: 2%|▏ | 1/50 [00:00<00:00, 108.77 it/sec, feas=True, obj=-2.25]
INFO - 16:23:55: 4%|▍ | 2/50 [00:00<00:00, 67.44 it/sec, feas=True, obj=-2.25]
INFO - 16:23:55: 6%|▌ | 3/50 [00:00<00:00, 86.05 it/sec, feas=True, obj=-2.25]
INFO - 16:23:55: Optimization result:
INFO - 16:23:55: Optimizer info:
INFO - 16:23:55: Status: None
INFO - 16:23:55: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:55: Solution:
INFO - 16:23:55: The solution is feasible.
INFO - 16:23:55: Objective: -2.2456645030762274
INFO - 16:23:55: Standardized constraints:
INFO - 16:23:55: g_3 = [-8.35563399e-01 -1.64436601e-01 5.99520433e-15 -1.81271168e-01]
INFO - 16:23:55: Design space:
INFO - 16:23:55: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:55: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:55: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:55: | x_3 | 0.1 | 0.1584554058636577 | 1 | float |
INFO - 16:23:55: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:55: *** End PropulsionScenario execution (time: 0:00:00.037191) ***
INFO - 16:23:55: *** Start AerodynamicsScenario execution ***
INFO - 16:23:55: AerodynamicsScenario
INFO - 16:23:55: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:55: MDO formulation: MDF
INFO - 16:23:55: Optimization problem:
INFO - 16:23:55: minimize 0.001*-y_4(x_2)
INFO - 16:23:55: with respect to x_2
INFO - 16:23:55: under the inequality constraints
INFO - 16:23:55: g_2(x_2) <= 0
INFO - 16:23:55: over the design space:
INFO - 16:23:55: +------+-------------+-------+-------------+-------+
INFO - 16:23:55: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:55: +------+-------------+-------+-------------+-------+
INFO - 16:23:55: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:55: +------+-------------+-------+-------------+-------+
INFO - 16:23:55: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:55: 2%|▏ | 1/50 [00:00<00:00, 80.54 it/sec, feas=True, obj=-2.25]
INFO - 16:23:55: Optimization result:
INFO - 16:23:55: Optimizer info:
INFO - 16:23:55: Status: 8
INFO - 16:23:55: Message: Positive directional derivative for linesearch
INFO - 16:23:55: Solution:
INFO - 16:23:55: The solution is feasible.
INFO - 16:23:55: Objective: -2.2456645030762274
INFO - 16:23:55: Standardized constraints:
INFO - 16:23:55: g_2 = 6.698384737613416e-05
INFO - 16:23:55: Design space:
INFO - 16:23:55: +------+-------------+-------+-------------+-------+
INFO - 16:23:55: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:55: +------+-------------+-------+-------------+-------+
INFO - 16:23:55: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:55: +------+-------------+-------+-------------+-------+
INFO - 16:23:55: *** End AerodynamicsScenario execution (time: 0:00:00.014054) ***
INFO - 16:23:55: *** Start StructureScenario execution ***
INFO - 16:23:55: StructureScenario
INFO - 16:23:55: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:55: MDO formulation: MDF
INFO - 16:23:55: Optimization problem:
INFO - 16:23:55: minimize 0.001*-y_4(x_1)
INFO - 16:23:55: with respect to x_1
INFO - 16:23:55: under the inequality constraints
INFO - 16:23:55: g_1(x_1) <= 0
INFO - 16:23:55: over the design space:
INFO - 16:23:55: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:55: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:55: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:55: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:55: | x_1[1] | 0.75 | 0.7806436836764827 | 1.25 | float |
INFO - 16:23:55: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:55: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:55: 2%|▏ | 1/50 [00:00<00:00, 102.89 it/sec, feas=True, obj=-2.25]
INFO - 16:23:55: 4%|▍ | 2/50 [00:00<00:00, 127.30 it/sec, feas=True, obj=-2.25]
INFO - 16:23:55: 6%|▌ | 3/50 [00:00<00:00, 137.60 it/sec, feas=True, obj=-2.25]
INFO - 16:23:55: Optimization result:
INFO - 16:23:55: Optimizer info:
INFO - 16:23:55: Status: None
INFO - 16:23:55: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:55: Solution:
INFO - 16:23:55: The solution is feasible.
INFO - 16:23:55: Objective: -2.2456645030762274
INFO - 16:23:55: Standardized constraints:
INFO - 16:23:55: g_1 = [-2.13283465e-03 -2.32314821e-03 -1.33303331e-02 -2.34264930e-02
INFO - 16:23:55: -3.16122033e-02 -2.40000000e-01 1.36557432e-14]
INFO - 16:23:55: Design space:
INFO - 16:23:55: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:55: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:55: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:55: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:55: | x_1[1] | 0.75 | 0.7806436836764827 | 1.25 | float |
INFO - 16:23:55: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:55: *** End StructureScenario execution (time: 0:00:00.024358) ***
INFO - 16:23:55: 72%|███████▏ | 72/100 [00:38<00:15, 1.87 it/sec, feas=True, obj=-2.25]
INFO - 16:23:55: *** Start PropulsionScenario execution ***
INFO - 16:23:55: PropulsionScenario
INFO - 16:23:55: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:55: MDO formulation: MDF
INFO - 16:23:55: Optimization problem:
INFO - 16:23:55: minimize 0.001*-y_4(x_3)
INFO - 16:23:55: with respect to x_3
INFO - 16:23:55: under the inequality constraints
INFO - 16:23:55: g_3(x_3) <= 0
INFO - 16:23:55: over the design space:
INFO - 16:23:55: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:55: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:55: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:55: | x_3 | 0.1 | 0.1584554058636577 | 1 | float |
INFO - 16:23:55: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:55: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:55: 2%|▏ | 1/50 [00:00<00:01, 38.88 it/sec, feas=False, obj=-2.26]
INFO - 16:23:55: 4%|▍ | 2/50 [00:00<00:01, 39.01 it/sec, feas=True, obj=-2.26]
INFO - 16:23:55: 6%|▌ | 3/50 [00:00<00:01, 32.72 it/sec, feas=False, obj=-2.26]
INFO - 16:23:55: 8%|▊ | 4/50 [00:00<00:01, 29.56 it/sec, feas=True, obj=-2.26]
INFO - 16:23:55: 10%|█ | 5/50 [00:00<00:01, 31.06 it/sec, feas=True, obj=-2.26]
INFO - 16:23:55: 12%|█▏ | 6/50 [00:00<00:01, 29.76 it/sec, feas=True, obj=-2.26]
INFO - 16:23:55: Optimization result:
INFO - 16:23:55: Optimizer info:
INFO - 16:23:55: Status: 8
INFO - 16:23:55: Message: Positive directional derivative for linesearch
INFO - 16:23:55: Solution:
INFO - 16:23:55: The solution is feasible.
INFO - 16:23:55: Objective: -2.2625871484195677
INFO - 16:23:55: Standardized constraints:
INFO - 16:23:55: g_3 = [-8.36442923e-01 -1.63557077e-01 1.15463195e-14 -1.81756195e-01]
INFO - 16:23:55: Design space:
INFO - 16:23:55: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:55: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:55: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:55: | x_3 | 0.1 | 0.1578426571721464 | 1 | float |
INFO - 16:23:55: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:55: *** End PropulsionScenario execution (time: 0:00:00.203638) ***
INFO - 16:23:55: *** Start AerodynamicsScenario execution ***
INFO - 16:23:55: AerodynamicsScenario
INFO - 16:23:55: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:55: MDO formulation: MDF
INFO - 16:23:55: Optimization problem:
INFO - 16:23:55: minimize 0.001*-y_4(x_2)
INFO - 16:23:55: with respect to x_2
INFO - 16:23:55: under the inequality constraints
INFO - 16:23:55: g_2(x_2) <= 0
INFO - 16:23:55: over the design space:
INFO - 16:23:55: +------+-------------+-------+-------------+-------+
INFO - 16:23:55: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:55: +------+-------------+-------+-------------+-------+
INFO - 16:23:55: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:55: +------+-------------+-------+-------------+-------+
INFO - 16:23:55: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:55: 2%|▏ | 1/50 [00:00<00:00, 78.13 it/sec, feas=True, obj=-2.26]
INFO - 16:23:55: Optimization result:
INFO - 16:23:55: Optimizer info:
INFO - 16:23:55: Status: 8
INFO - 16:23:55: Message: Positive directional derivative for linesearch
INFO - 16:23:55: Solution:
INFO - 16:23:55: The solution is feasible.
INFO - 16:23:55: Objective: -2.2625871484195677
INFO - 16:23:55: Standardized constraints:
INFO - 16:23:55: g_2 = 0.0
INFO - 16:23:55: Design space:
INFO - 16:23:55: +------+-------------+-------+-------------+-------+
INFO - 16:23:55: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:55: +------+-------------+-------+-------------+-------+
INFO - 16:23:55: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:55: +------+-------------+-------+-------------+-------+
INFO - 16:23:55: *** End AerodynamicsScenario execution (time: 0:00:00.014636) ***
INFO - 16:23:55: *** Start StructureScenario execution ***
INFO - 16:23:55: StructureScenario
INFO - 16:23:55: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:55: MDO formulation: MDF
INFO - 16:23:55: Optimization problem:
INFO - 16:23:55: minimize 0.001*-y_4(x_1)
INFO - 16:23:55: with respect to x_1
INFO - 16:23:55: under the inequality constraints
INFO - 16:23:55: g_1(x_1) <= 0
INFO - 16:23:55: over the design space:
INFO - 16:23:55: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:55: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:55: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:55: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:55: | x_1[1] | 0.75 | 0.7806436836764827 | 1.25 | float |
INFO - 16:23:55: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:55: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:55: 2%|▏ | 1/50 [00:00<00:00, 98.61 it/sec, feas=True, obj=-2.26]
INFO - 16:23:55: 4%|▍ | 2/50 [00:00<00:00, 59.79 it/sec, feas=True, obj=-2.26]
INFO - 16:23:55: 6%|▌ | 3/50 [00:00<00:00, 73.97 it/sec, feas=True, obj=-2.26]
INFO - 16:23:55: Optimization result:
INFO - 16:23:55: Optimizer info:
INFO - 16:23:55: Status: None
INFO - 16:23:55: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:55: Solution:
INFO - 16:23:55: The solution is feasible.
INFO - 16:23:55: Objective: -2.2625871484195677
INFO - 16:23:55: Standardized constraints:
INFO - 16:23:55: g_1 = [-1.59589593e-03 -2.02868890e-03 -1.31333010e-02 -2.32802973e-02
INFO - 16:23:55: -3.14967236e-02 -2.40000000e-01 1.36557432e-14]
INFO - 16:23:55: Design space:
INFO - 16:23:55: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:55: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:55: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:55: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:55: | x_1[1] | 0.75 | 0.7806436836764827 | 1.25 | float |
INFO - 16:23:55: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:55: *** End StructureScenario execution (time: 0:00:00.042993) ***
INFO - 16:23:55: *** Start PropulsionScenario execution ***
INFO - 16:23:55: PropulsionScenario
INFO - 16:23:55: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:55: MDO formulation: MDF
INFO - 16:23:55: Optimization problem:
INFO - 16:23:55: minimize 0.001*-y_4(x_3)
INFO - 16:23:55: with respect to x_3
INFO - 16:23:55: under the inequality constraints
INFO - 16:23:55: g_3(x_3) <= 0
INFO - 16:23:55: over the design space:
INFO - 16:23:55: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:55: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:55: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:55: | x_3 | 0.1 | 0.1578426571721464 | 1 | float |
INFO - 16:23:55: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:55: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:55: 2%|▏ | 1/50 [00:00<00:00, 92.85 it/sec, feas=True, obj=-2.26]
INFO - 16:23:55: 4%|▍ | 2/50 [00:00<00:00, 56.11 it/sec, feas=True, obj=-2.26]
INFO - 16:23:55: Optimization result:
INFO - 16:23:55: Optimizer info:
INFO - 16:23:55: Status: 8
INFO - 16:23:55: Message: Positive directional derivative for linesearch
INFO - 16:23:55: Solution:
INFO - 16:23:55: The solution is feasible.
INFO - 16:23:55: Objective: -2.2625871484195677
INFO - 16:23:55: Standardized constraints:
INFO - 16:23:55: g_3 = [-8.36442923e-01 -1.63557077e-01 1.15463195e-14 -1.81756195e-01]
INFO - 16:23:55: Design space:
INFO - 16:23:55: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:55: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:55: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:55: | x_3 | 0.1 | 0.1578426571721464 | 1 | float |
INFO - 16:23:55: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:55: *** End PropulsionScenario execution (time: 0:00:00.037710) ***
INFO - 16:23:55: *** Start AerodynamicsScenario execution ***
INFO - 16:23:55: AerodynamicsScenario
INFO - 16:23:55: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:55: MDO formulation: MDF
INFO - 16:23:55: Optimization problem:
INFO - 16:23:55: minimize 0.001*-y_4(x_2)
INFO - 16:23:55: with respect to x_2
INFO - 16:23:55: under the inequality constraints
INFO - 16:23:55: g_2(x_2) <= 0
INFO - 16:23:55: over the design space:
INFO - 16:23:55: +------+-------------+-------+-------------+-------+
INFO - 16:23:55: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:55: +------+-------------+-------+-------------+-------+
INFO - 16:23:55: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:55: +------+-------------+-------+-------------+-------+
INFO - 16:23:55: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:55: 2%|▏ | 1/50 [00:00<00:00, 80.38 it/sec, feas=True, obj=-2.26]
INFO - 16:23:55: Optimization result:
INFO - 16:23:55: Optimizer info:
INFO - 16:23:55: Status: 8
INFO - 16:23:55: Message: Positive directional derivative for linesearch
INFO - 16:23:55: Solution:
INFO - 16:23:55: The solution is feasible.
INFO - 16:23:55: Objective: -2.2625871484195685
INFO - 16:23:55: Standardized constraints:
INFO - 16:23:55: g_2 = 0.0
INFO - 16:23:55: Design space:
INFO - 16:23:55: +------+-------------+-------+-------------+-------+
INFO - 16:23:55: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:55: +------+-------------+-------+-------------+-------+
INFO - 16:23:55: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:55: +------+-------------+-------+-------------+-------+
INFO - 16:23:55: *** End AerodynamicsScenario execution (time: 0:00:00.014104) ***
INFO - 16:23:55: *** Start StructureScenario execution ***
INFO - 16:23:55: StructureScenario
INFO - 16:23:55: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:55: MDO formulation: MDF
INFO - 16:23:55: Optimization problem:
INFO - 16:23:55: minimize 0.001*-y_4(x_1)
INFO - 16:23:55: with respect to x_1
INFO - 16:23:55: under the inequality constraints
INFO - 16:23:55: g_1(x_1) <= 0
INFO - 16:23:55: over the design space:
INFO - 16:23:55: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:55: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:55: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:55: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:55: | x_1[1] | 0.75 | 0.7806436836764827 | 1.25 | float |
INFO - 16:23:55: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:55: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:55: 2%|▏ | 1/50 [00:00<00:00, 83.65 it/sec, feas=True, obj=-2.26]
INFO - 16:23:55: 4%|▍ | 2/50 [00:00<00:00, 57.05 it/sec, feas=True, obj=-2.26]
INFO - 16:23:55: 6%|▌ | 3/50 [00:00<00:00, 72.65 it/sec, feas=True, obj=-2.26]
INFO - 16:23:55: Optimization result:
INFO - 16:23:55: Optimizer info:
INFO - 16:23:55: Status: None
INFO - 16:23:55: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:55: Solution:
INFO - 16:23:55: The solution is feasible.
INFO - 16:23:55: Objective: -2.2625871484195677
INFO - 16:23:55: Standardized constraints:
INFO - 16:23:55: g_1 = [-1.59589593e-03 -2.02868890e-03 -1.31333010e-02 -2.32802973e-02
INFO - 16:23:55: -3.14967236e-02 -2.40000000e-01 1.36557432e-14]
INFO - 16:23:55: Design space:
INFO - 16:23:55: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:55: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:55: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:55: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:55: | x_1[1] | 0.75 | 0.7806436836764827 | 1.25 | float |
INFO - 16:23:55: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:55: *** End StructureScenario execution (time: 0:00:00.043867) ***
INFO - 16:23:55: 73%|███████▎ | 73/100 [00:38<00:14, 1.87 it/sec, feas=True, obj=-2.26]
INFO - 16:23:55: *** Start PropulsionScenario execution ***
INFO - 16:23:55: PropulsionScenario
INFO - 16:23:55: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:55: MDO formulation: MDF
INFO - 16:23:55: Optimization problem:
INFO - 16:23:55: minimize 0.001*-y_4(x_3)
INFO - 16:23:55: with respect to x_3
INFO - 16:23:55: under the inequality constraints
INFO - 16:23:55: g_3(x_3) <= 0
INFO - 16:23:55: over the design space:
INFO - 16:23:55: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:55: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:55: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:55: | x_3 | 0.1 | 0.1578426571721464 | 1 | float |
INFO - 16:23:55: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:55: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:55: 2%|▏ | 1/50 [00:00<00:01, 39.91 it/sec, feas=True, obj=-2.26]
INFO - 16:23:55: 4%|▍ | 2/50 [00:00<00:01, 30.51 it/sec, feas=True, obj=-2.26]
INFO - 16:23:55: 6%|▌ | 3/50 [00:00<00:01, 28.23 it/sec, feas=True, obj=-2.26]
INFO - 16:23:56: 8%|▊ | 4/50 [00:00<00:01, 30.30 it/sec, feas=True, obj=-2.26]
INFO - 16:23:56: Optimization result:
INFO - 16:23:56: Optimizer info:
INFO - 16:23:56: Status: None
INFO - 16:23:56: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:56: Solution:
INFO - 16:23:56: The solution is feasible.
INFO - 16:23:56: Objective: -2.2557306999153472
INFO - 16:23:56: Standardized constraints:
INFO - 16:23:56: g_3 = [-8.36430214e-01 -1.63569786e-01 4.44089210e-16 -1.81564888e-01]
INFO - 16:23:56: Design space:
INFO - 16:23:56: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:56: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:56: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:56: | x_3 | 0.1 | 0.1580487553764545 | 1 | float |
INFO - 16:23:56: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:56: *** End PropulsionScenario execution (time: 0:00:00.134361) ***
INFO - 16:23:56: *** Start AerodynamicsScenario execution ***
INFO - 16:23:56: AerodynamicsScenario
INFO - 16:23:56: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:56: MDO formulation: MDF
INFO - 16:23:56: Optimization problem:
INFO - 16:23:56: minimize 0.001*-y_4(x_2)
INFO - 16:23:56: with respect to x_2
INFO - 16:23:56: under the inequality constraints
INFO - 16:23:56: g_2(x_2) <= 0
INFO - 16:23:56: over the design space:
INFO - 16:23:56: +------+-------------+-------+-------------+-------+
INFO - 16:23:56: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:56: +------+-------------+-------+-------------+-------+
INFO - 16:23:56: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:56: +------+-------------+-------+-------------+-------+
INFO - 16:23:56: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:56: 2%|▏ | 1/50 [00:00<00:00, 84.97 it/sec, feas=True, obj=-2.26]
INFO - 16:23:56: Optimization result:
INFO - 16:23:56: Optimizer info:
INFO - 16:23:56: Status: 8
INFO - 16:23:56: Message: Positive directional derivative for linesearch
INFO - 16:23:56: Solution:
INFO - 16:23:56: The solution is feasible.
INFO - 16:23:56: Objective: -2.2557306999153472
INFO - 16:23:56: Standardized constraints:
INFO - 16:23:56: g_2 = 0.0
INFO - 16:23:56: Design space:
INFO - 16:23:56: +------+-------------+-------+-------------+-------+
INFO - 16:23:56: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:56: +------+-------------+-------+-------------+-------+
INFO - 16:23:56: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:56: +------+-------------+-------+-------------+-------+
INFO - 16:23:56: *** End AerodynamicsScenario execution (time: 0:00:00.013320) ***
INFO - 16:23:56: *** Start StructureScenario execution ***
INFO - 16:23:56: StructureScenario
INFO - 16:23:56: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:56: MDO formulation: MDF
INFO - 16:23:56: Optimization problem:
INFO - 16:23:56: minimize 0.001*-y_4(x_1)
INFO - 16:23:56: with respect to x_1
INFO - 16:23:56: under the inequality constraints
INFO - 16:23:56: g_1(x_1) <= 0
INFO - 16:23:56: over the design space:
INFO - 16:23:56: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:56: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:56: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:56: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:56: | x_1[1] | 0.75 | 0.7806436836764827 | 1.25 | float |
INFO - 16:23:56: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:56: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:56: 2%|▏ | 1/50 [00:00<00:00, 97.35 it/sec, feas=True, obj=-2.26]
WARNING - 16:23:56: MDAGaussSeidel has reached its maximum number of unsuccessful iterations, but the normalized residual norm 0.0009157477359807847 is still above the tolerance 1e-06.
INFO - 16:23:56: 4%|▍ | 2/50 [00:00<00:01, 44.20 it/sec, feas=True, obj=-2.26]
WARNING - 16:23:56: MDAGaussSeidel has reached its maximum number of unsuccessful iterations, but the normalized residual norm 0.0009157477359807847 is still above the tolerance 1e-06.
INFO - 16:23:56: 6%|▌ | 3/50 [00:00<00:00, 47.01 it/sec, feas=True, obj=-2.26]
INFO - 16:23:56: Optimization result:
INFO - 16:23:56: Optimizer info:
INFO - 16:23:56: Status: None
INFO - 16:23:56: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:56: Solution:
INFO - 16:23:56: The solution is feasible.
INFO - 16:23:56: Objective: -2.2557306999153472
INFO - 16:23:56: Standardized constraints:
INFO - 16:23:56: g_1 = [-1.59589593e-03 -2.02868890e-03 -1.31333010e-02 -2.32802973e-02
INFO - 16:23:56: -3.14967236e-02 -2.40000000e-01 1.36557432e-14]
INFO - 16:23:56: Design space:
INFO - 16:23:56: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:56: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:56: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:56: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:56: | x_1[1] | 0.75 | 0.7806436836764827 | 1.25 | float |
INFO - 16:23:56: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:56: *** End StructureScenario execution (time: 0:00:00.066396) ***
INFO - 16:23:56: *** Start PropulsionScenario execution ***
INFO - 16:23:56: PropulsionScenario
INFO - 16:23:56: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:56: MDO formulation: MDF
INFO - 16:23:56: Optimization problem:
INFO - 16:23:56: minimize 0.001*-y_4(x_3)
INFO - 16:23:56: with respect to x_3
INFO - 16:23:56: under the inequality constraints
INFO - 16:23:56: g_3(x_3) <= 0
INFO - 16:23:56: over the design space:
INFO - 16:23:56: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:56: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:56: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:56: | x_3 | 0.1 | 0.1580487553764545 | 1 | float |
INFO - 16:23:56: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:56: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:56: 2%|▏ | 1/50 [00:00<00:00, 90.03 it/sec, feas=True, obj=-2.26]
INFO - 16:23:56: 4%|▍ | 2/50 [00:00<00:00, 126.54 it/sec, feas=True, obj=-2.26]
INFO - 16:23:56: 6%|▌ | 3/50 [00:00<00:00, 151.39 it/sec, feas=True, obj=-2.26]
INFO - 16:23:56: Optimization result:
INFO - 16:23:56: Optimizer info:
INFO - 16:23:56: Status: None
INFO - 16:23:56: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:56: Solution:
INFO - 16:23:56: The solution is feasible.
INFO - 16:23:56: Objective: -2.255730699915348
INFO - 16:23:56: Standardized constraints:
INFO - 16:23:56: g_3 = [-8.36430214e-01 -1.63569786e-01 4.21884749e-15 -1.81564888e-01]
INFO - 16:23:56: Design space:
INFO - 16:23:56: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:56: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:56: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:56: | x_3 | 0.1 | 0.1580487553764551 | 1 | float |
INFO - 16:23:56: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:56: *** End PropulsionScenario execution (time: 0:00:00.022214) ***
INFO - 16:23:56: *** Start AerodynamicsScenario execution ***
INFO - 16:23:56: AerodynamicsScenario
INFO - 16:23:56: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:56: MDO formulation: MDF
INFO - 16:23:56: Optimization problem:
INFO - 16:23:56: minimize 0.001*-y_4(x_2)
INFO - 16:23:56: with respect to x_2
INFO - 16:23:56: under the inequality constraints
INFO - 16:23:56: g_2(x_2) <= 0
INFO - 16:23:56: over the design space:
INFO - 16:23:56: +------+-------------+-------+-------------+-------+
INFO - 16:23:56: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:56: +------+-------------+-------+-------------+-------+
INFO - 16:23:56: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:56: +------+-------------+-------+-------------+-------+
INFO - 16:23:56: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:56: 2%|▏ | 1/50 [00:00<00:00, 80.00 it/sec, feas=True, obj=-2.26]
INFO - 16:23:56: Optimization result:
INFO - 16:23:56: Optimizer info:
INFO - 16:23:56: Status: 8
INFO - 16:23:56: Message: Positive directional derivative for linesearch
INFO - 16:23:56: Solution:
INFO - 16:23:56: The solution is feasible.
INFO - 16:23:56: Objective: -2.2557306999153472
INFO - 16:23:56: Standardized constraints:
INFO - 16:23:56: g_2 = 0.0
INFO - 16:23:56: Design space:
INFO - 16:23:56: +------+-------------+-------+-------------+-------+
INFO - 16:23:56: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:56: +------+-------------+-------+-------------+-------+
INFO - 16:23:56: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:56: +------+-------------+-------+-------------+-------+
INFO - 16:23:56: *** End AerodynamicsScenario execution (time: 0:00:00.014209) ***
INFO - 16:23:56: *** Start StructureScenario execution ***
INFO - 16:23:56: StructureScenario
INFO - 16:23:56: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:56: MDO formulation: MDF
INFO - 16:23:56: Optimization problem:
INFO - 16:23:56: minimize 0.001*-y_4(x_1)
INFO - 16:23:56: with respect to x_1
INFO - 16:23:56: under the inequality constraints
INFO - 16:23:56: g_1(x_1) <= 0
INFO - 16:23:56: over the design space:
INFO - 16:23:56: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:56: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:56: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:56: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:56: | x_1[1] | 0.75 | 0.7806436836764827 | 1.25 | float |
INFO - 16:23:56: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:56: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:56: 2%|▏ | 1/50 [00:00<00:00, 82.62 it/sec, feas=True, obj=-2.26]
INFO - 16:23:56: Optimization result:
INFO - 16:23:56: Optimizer info:
INFO - 16:23:56: Status: 8
INFO - 16:23:56: Message: Positive directional derivative for linesearch
INFO - 16:23:56: Solution:
INFO - 16:23:56: The solution is feasible.
INFO - 16:23:56: Objective: -2.255730699915348
INFO - 16:23:56: Standardized constraints:
INFO - 16:23:56: g_1 = [-1.59589593e-03 -2.02868890e-03 -1.31333010e-02 -2.32802973e-02
INFO - 16:23:56: -3.14967236e-02 -2.40000000e-01 1.36557432e-14]
INFO - 16:23:56: Design space:
INFO - 16:23:56: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:56: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:56: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:56: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:56: | x_1[1] | 0.75 | 0.7806436836764827 | 1.25 | float |
INFO - 16:23:56: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:56: *** End StructureScenario execution (time: 0:00:00.014170) ***
INFO - 16:23:56: 74%|███████▍ | 74/100 [00:39<00:13, 1.88 it/sec, feas=True, obj=-2.26]
INFO - 16:23:56: *** Start PropulsionScenario execution ***
INFO - 16:23:56: PropulsionScenario
INFO - 16:23:56: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:56: MDO formulation: MDF
INFO - 16:23:56: Optimization problem:
INFO - 16:23:56: minimize 0.001*-y_4(x_3)
INFO - 16:23:56: with respect to x_3
INFO - 16:23:56: under the inequality constraints
INFO - 16:23:56: g_3(x_3) <= 0
INFO - 16:23:56: over the design space:
INFO - 16:23:56: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:56: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:56: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:56: | x_3 | 0.1 | 0.1580487553764551 | 1 | float |
INFO - 16:23:56: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:56: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:56: 2%|▏ | 1/50 [00:00<00:01, 40.06 it/sec, feas=True, obj=-2.24]
INFO - 16:23:56: 4%|▍ | 2/50 [00:00<00:01, 30.58 it/sec, feas=True, obj=-2.24]
INFO - 16:23:56: 6%|▌ | 3/50 [00:00<00:01, 27.76 it/sec, feas=True, obj=-2.24]
INFO - 16:23:56: 8%|▊ | 4/50 [00:00<00:01, 26.81 it/sec, feas=True, obj=-2.24]
INFO - 16:23:56: Optimization result:
INFO - 16:23:56: Optimizer info:
INFO - 16:23:56: Status: 8
INFO - 16:23:56: Message: Positive directional derivative for linesearch
INFO - 16:23:56: Solution:
INFO - 16:23:56: The solution is feasible.
INFO - 16:23:56: Objective: -2.2427664474250912
INFO - 16:23:56: Standardized constraints:
INFO - 16:23:56: g_3 = [-8.36377972e-01 -1.63622028e-01 6.66133815e-16 -1.81375241e-01]
INFO - 16:23:56: Design space:
INFO - 16:23:56: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:56: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:56: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:56: | x_3 | 0.1 | 0.1584838451744719 | 1 | float |
INFO - 16:23:56: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:56: *** End PropulsionScenario execution (time: 0:00:00.151323) ***
INFO - 16:23:56: *** Start AerodynamicsScenario execution ***
INFO - 16:23:56: AerodynamicsScenario
INFO - 16:23:56: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:56: MDO formulation: MDF
INFO - 16:23:56: Optimization problem:
INFO - 16:23:56: minimize 0.001*-y_4(x_2)
INFO - 16:23:56: with respect to x_2
INFO - 16:23:56: under the inequality constraints
INFO - 16:23:56: g_2(x_2) <= 0
INFO - 16:23:56: over the design space:
INFO - 16:23:56: +------+-------------+-------+-------------+-------+
INFO - 16:23:56: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:56: +------+-------------+-------+-------------+-------+
INFO - 16:23:56: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:56: +------+-------------+-------+-------------+-------+
INFO - 16:23:56: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:56: 2%|▏ | 1/50 [00:00<00:00, 104.81 it/sec, feas=True, obj=-2.24]
INFO - 16:23:56: Optimization result:
INFO - 16:23:56: Optimizer info:
INFO - 16:23:56: Status: 8
INFO - 16:23:56: Message: Positive directional derivative for linesearch
INFO - 16:23:56: Solution:
INFO - 16:23:56: The solution is feasible.
INFO - 16:23:56: Objective: -2.2427664474250912
INFO - 16:23:56: Standardized constraints:
INFO - 16:23:56: g_2 = -5.939024638057511e-05
INFO - 16:23:56: Design space:
INFO - 16:23:56: +------+-------------+-------+-------------+-------+
INFO - 16:23:56: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:56: +------+-------------+-------+-------------+-------+
INFO - 16:23:56: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:56: +------+-------------+-------+-------------+-------+
INFO - 16:23:56: *** End AerodynamicsScenario execution (time: 0:00:00.011155) ***
INFO - 16:23:56: *** Start StructureScenario execution ***
INFO - 16:23:56: StructureScenario
INFO - 16:23:56: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:56: MDO formulation: MDF
INFO - 16:23:56: Optimization problem:
INFO - 16:23:56: minimize 0.001*-y_4(x_1)
INFO - 16:23:56: with respect to x_1
INFO - 16:23:56: under the inequality constraints
INFO - 16:23:56: g_1(x_1) <= 0
INFO - 16:23:56: over the design space:
INFO - 16:23:56: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:56: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:56: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:56: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:56: | x_1[1] | 0.75 | 0.7806436836764827 | 1.25 | float |
INFO - 16:23:56: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:56: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:56: 2%|▏ | 1/50 [00:00<00:00, 97.94 it/sec, feas=True, obj=-2.24]
INFO - 16:23:56: Optimization result:
INFO - 16:23:56: Optimizer info:
INFO - 16:23:56: Status: 8
INFO - 16:23:56: Message: Positive directional derivative for linesearch
INFO - 16:23:56: Solution:
INFO - 16:23:56: The solution is feasible.
INFO - 16:23:56: Objective: -2.2427664474250912
INFO - 16:23:56: Standardized constraints:
INFO - 16:23:56: g_1 = [-1.12006162e-03 -1.76771512e-03 -1.29586641e-02 -2.31507126e-02
INFO - 16:23:56: -3.13943612e-02 -2.40000000e-01 1.36557432e-14]
INFO - 16:23:56: Design space:
INFO - 16:23:56: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:56: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:56: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:56: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:56: | x_1[1] | 0.75 | 0.7806436836764827 | 1.25 | float |
INFO - 16:23:56: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:56: *** End StructureScenario execution (time: 0:00:00.012211) ***
INFO - 16:23:56: *** Start PropulsionScenario execution ***
INFO - 16:23:56: PropulsionScenario
INFO - 16:23:56: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:56: MDO formulation: MDF
INFO - 16:23:56: Optimization problem:
INFO - 16:23:56: minimize 0.001*-y_4(x_3)
INFO - 16:23:56: with respect to x_3
INFO - 16:23:56: under the inequality constraints
INFO - 16:23:56: g_3(x_3) <= 0
INFO - 16:23:56: over the design space:
INFO - 16:23:56: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:56: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:56: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:56: | x_3 | 0.1 | 0.1584838451744719 | 1 | float |
INFO - 16:23:56: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:56: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:56: 2%|▏ | 1/50 [00:00<00:00, 109.99 it/sec, feas=True, obj=-2.24]
INFO - 16:23:56: Optimization result:
INFO - 16:23:56: Optimizer info:
INFO - 16:23:56: Status: 8
INFO - 16:23:56: Message: Positive directional derivative for linesearch
INFO - 16:23:56: Solution:
INFO - 16:23:56: The solution is feasible.
INFO - 16:23:56: Objective: -2.2427664474250912
INFO - 16:23:56: Standardized constraints:
INFO - 16:23:56: g_3 = [-8.36377972e-01 -1.63622028e-01 6.66133815e-16 -1.81375241e-01]
INFO - 16:23:56: Design space:
INFO - 16:23:56: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:56: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:56: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:56: | x_3 | 0.1 | 0.1584838451744719 | 1 | float |
INFO - 16:23:56: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:56: *** End PropulsionScenario execution (time: 0:00:00.010880) ***
INFO - 16:23:56: 75%|███████▌ | 75/100 [00:39<00:13, 1.90 it/sec, feas=True, obj=-2.24]
INFO - 16:23:56: *** Start PropulsionScenario execution ***
INFO - 16:23:56: PropulsionScenario
INFO - 16:23:56: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:56: MDO formulation: MDF
INFO - 16:23:56: Optimization problem:
INFO - 16:23:56: minimize 0.001*-y_4(x_3)
INFO - 16:23:56: with respect to x_3
INFO - 16:23:56: under the inequality constraints
INFO - 16:23:56: g_3(x_3) <= 0
INFO - 16:23:56: over the design space:
INFO - 16:23:56: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:56: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:56: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:56: | x_3 | 0.1 | 0.1584838451744719 | 1 | float |
INFO - 16:23:56: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:56: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:56: 2%|▏ | 1/50 [00:00<00:01, 37.78 it/sec, feas=False, obj=-2.26]
INFO - 16:23:56: 4%|▍ | 2/50 [00:00<00:01, 38.44 it/sec, feas=True, obj=-2.25]
INFO - 16:23:56: 6%|▌ | 3/50 [00:00<00:01, 31.94 it/sec, feas=False, obj=-2.26]
INFO - 16:23:56: 8%|▊ | 4/50 [00:00<00:01, 29.30 it/sec, feas=True, obj=-2.25]
INFO - 16:23:56: 10%|█ | 5/50 [00:00<00:01, 30.70 it/sec, feas=True, obj=-2.25]
INFO - 16:23:56: 12%|█▏ | 6/50 [00:00<00:01, 31.70 it/sec, feas=True, obj=-2.25]
INFO - 16:23:56: Optimization result:
INFO - 16:23:56: Optimizer info:
INFO - 16:23:56: Status: None
INFO - 16:23:56: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:56: Solution:
INFO - 16:23:56: The solution is feasible.
INFO - 16:23:56: Objective: -2.2543995810773167
INFO - 16:23:56: Standardized constraints:
INFO - 16:23:56: g_3 = [-8.37434954e-01 -1.62565046e-01 -3.33066907e-16 -1.81555306e-01]
INFO - 16:23:56: Design space:
INFO - 16:23:56: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:56: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:56: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:56: | x_3 | 0.1 | 0.1580590902997958 | 1 | float |
INFO - 16:23:56: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:56: *** End PropulsionScenario execution (time: 0:00:00.191935) ***
INFO - 16:23:56: *** Start AerodynamicsScenario execution ***
INFO - 16:23:56: AerodynamicsScenario
INFO - 16:23:56: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:56: MDO formulation: MDF
INFO - 16:23:56: Optimization problem:
INFO - 16:23:56: minimize 0.001*-y_4(x_2)
INFO - 16:23:56: with respect to x_2
INFO - 16:23:56: under the inequality constraints
INFO - 16:23:56: g_2(x_2) <= 0
INFO - 16:23:56: over the design space:
INFO - 16:23:56: +------+-------------+-------+-------------+-------+
INFO - 16:23:56: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:56: +------+-------------+-------+-------------+-------+
INFO - 16:23:56: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:56: +------+-------------+-------+-------------+-------+
INFO - 16:23:56: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:56: 2%|▏ | 1/50 [00:00<00:00, 61.26 it/sec, feas=True, obj=-2.25]
INFO - 16:23:56: Optimization result:
INFO - 16:23:56: Optimizer info:
INFO - 16:23:56: Status: 8
INFO - 16:23:56: Message: Positive directional derivative for linesearch
INFO - 16:23:56: Solution:
INFO - 16:23:56: The solution is feasible.
INFO - 16:23:56: Objective: -2.2543995810773167
INFO - 16:23:56: Standardized constraints:
INFO - 16:23:56: g_2 = 0.0
INFO - 16:23:56: Design space:
INFO - 16:23:56: +------+-------------+-------+-------------+-------+
INFO - 16:23:56: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:56: +------+-------------+-------+-------------+-------+
INFO - 16:23:56: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:56: +------+-------------+-------+-------------+-------+
INFO - 16:23:56: *** End AerodynamicsScenario execution (time: 0:00:00.018591) ***
INFO - 16:23:56: *** Start StructureScenario execution ***
INFO - 16:23:56: StructureScenario
INFO - 16:23:56: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:56: MDO formulation: MDF
INFO - 16:23:56: Optimization problem:
INFO - 16:23:56: minimize 0.001*-y_4(x_1)
INFO - 16:23:56: with respect to x_1
INFO - 16:23:56: under the inequality constraints
INFO - 16:23:56: g_1(x_1) <= 0
INFO - 16:23:56: over the design space:
INFO - 16:23:56: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:56: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:56: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:56: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:56: | x_1[1] | 0.75 | 0.7806436836764827 | 1.25 | float |
INFO - 16:23:56: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:56: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:56: 2%|▏ | 1/50 [00:00<00:00, 97.67 it/sec, feas=True, obj=-2.25]
INFO - 16:23:56: 4%|▍ | 2/50 [00:00<00:00, 59.40 it/sec, feas=True, obj=-2.25]
INFO - 16:23:56: Optimization result:
INFO - 16:23:56: Optimizer info:
INFO - 16:23:56: Status: 8
INFO - 16:23:56: Message: Positive directional derivative for linesearch
INFO - 16:23:56: Solution:
INFO - 16:23:56: The solution is feasible.
INFO - 16:23:56: Objective: -2.2543995810773167
INFO - 16:23:56: Standardized constraints:
INFO - 16:23:56: g_1 = [-1.59589593e-03 -2.02868890e-03 -1.31333010e-02 -2.32802973e-02
INFO - 16:23:56: -3.14967236e-02 -2.40000000e-01 1.36557432e-14]
INFO - 16:23:56: Design space:
INFO - 16:23:56: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:56: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:56: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:56: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:56: | x_1[1] | 0.75 | 0.7806436836764827 | 1.25 | float |
INFO - 16:23:56: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:56: *** End StructureScenario execution (time: 0:00:00.035951) ***
INFO - 16:23:56: *** Start PropulsionScenario execution ***
INFO - 16:23:56: PropulsionScenario
INFO - 16:23:56: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:56: MDO formulation: MDF
INFO - 16:23:56: Optimization problem:
INFO - 16:23:56: minimize 0.001*-y_4(x_3)
INFO - 16:23:56: with respect to x_3
INFO - 16:23:56: under the inequality constraints
INFO - 16:23:56: g_3(x_3) <= 0
INFO - 16:23:56: over the design space:
INFO - 16:23:56: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:56: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:56: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:56: | x_3 | 0.1 | 0.1580590902997958 | 1 | float |
INFO - 16:23:56: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:56: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:56: 2%|▏ | 1/50 [00:00<00:00, 91.71 it/sec, feas=True, obj=-2.25]
INFO - 16:23:56: Optimization result:
INFO - 16:23:56: Optimizer info:
INFO - 16:23:56: Status: 8
INFO - 16:23:56: Message: Positive directional derivative for linesearch
INFO - 16:23:56: Solution:
INFO - 16:23:56: The solution is feasible.
INFO - 16:23:56: Objective: -2.2543995810773167
INFO - 16:23:56: Standardized constraints:
INFO - 16:23:56: g_3 = [-8.37434954e-01 -1.62565046e-01 -3.33066907e-16 -1.81555306e-01]
INFO - 16:23:56: Design space:
INFO - 16:23:56: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:56: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:56: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:56: | x_3 | 0.1 | 0.1580590902997958 | 1 | float |
INFO - 16:23:56: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:56: *** End PropulsionScenario execution (time: 0:00:00.012784) ***
INFO - 16:23:56: 76%|███████▌ | 76/100 [00:39<00:12, 1.91 it/sec, feas=True, obj=-2.25]
INFO - 16:23:56: *** Start PropulsionScenario execution ***
INFO - 16:23:56: PropulsionScenario
INFO - 16:23:56: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:56: MDO formulation: MDF
INFO - 16:23:56: Optimization problem:
INFO - 16:23:56: minimize 0.001*-y_4(x_3)
INFO - 16:23:56: with respect to x_3
INFO - 16:23:56: under the inequality constraints
INFO - 16:23:56: g_3(x_3) <= 0
INFO - 16:23:56: over the design space:
INFO - 16:23:56: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:56: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:56: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:56: | x_3 | 0.1 | 0.1580590902997958 | 1 | float |
INFO - 16:23:56: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:56: Solving optimization problem with algorithm SLSQP:
WARNING - 16:23:56: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 6.724932466608626e-05 is still above the tolerance 1e-06.
INFO - 16:23:56: 2%|▏ | 1/50 [00:00<00:01, 33.69 it/sec, feas=True, obj=-2.25]
INFO - 16:23:56: 4%|▍ | 2/50 [00:00<00:01, 27.87 it/sec, feas=True, obj=-2.25]
INFO - 16:23:56: Optimization result:
INFO - 16:23:56: Optimizer info:
INFO - 16:23:56: Status: 8
INFO - 16:23:56: Message: Positive directional derivative for linesearch
INFO - 16:23:56: Solution:
INFO - 16:23:56: The solution is feasible.
INFO - 16:23:56: Objective: -2.2514667245970315
INFO - 16:23:56: Standardized constraints:
INFO - 16:23:56: g_3 = [-8.36419430e-01 -1.63580570e-01 1.33226763e-15 -1.81469033e-01]
INFO - 16:23:56: Design space:
INFO - 16:23:56: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:56: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:56: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:56: | x_3 | 0.1 | 0.1581522009163378 | 1 | float |
INFO - 16:23:56: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:56: *** End PropulsionScenario execution (time: 0:00:00.076050) ***
INFO - 16:23:56: *** Start AerodynamicsScenario execution ***
INFO - 16:23:56: AerodynamicsScenario
INFO - 16:23:56: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:56: MDO formulation: MDF
INFO - 16:23:56: Optimization problem:
INFO - 16:23:56: minimize 0.001*-y_4(x_2)
INFO - 16:23:56: with respect to x_2
INFO - 16:23:56: under the inequality constraints
INFO - 16:23:56: g_2(x_2) <= 0
INFO - 16:23:56: over the design space:
INFO - 16:23:56: +------+-------------+-------+-------------+-------+
INFO - 16:23:56: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:56: +------+-------------+-------+-------------+-------+
INFO - 16:23:56: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:56: +------+-------------+-------+-------------+-------+
INFO - 16:23:56: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:56: 2%|▏ | 1/50 [00:00<00:00, 104.32 it/sec, feas=True, obj=-2.25]
INFO - 16:23:56: Optimization result:
INFO - 16:23:56: Optimizer info:
INFO - 16:23:56: Status: 8
INFO - 16:23:56: Message: Positive directional derivative for linesearch
INFO - 16:23:56: Solution:
INFO - 16:23:56: The solution is feasible.
INFO - 16:23:56: Objective: -2.2514667245970315
INFO - 16:23:56: Standardized constraints:
INFO - 16:23:56: g_2 = 0.0
INFO - 16:23:56: Design space:
INFO - 16:23:56: +------+-------------+-------+-------------+-------+
INFO - 16:23:56: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:56: +------+-------------+-------+-------------+-------+
INFO - 16:23:56: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:56: +------+-------------+-------+-------------+-------+
INFO - 16:23:56: *** End AerodynamicsScenario execution (time: 0:00:00.011349) ***
INFO - 16:23:56: *** Start StructureScenario execution ***
INFO - 16:23:56: StructureScenario
INFO - 16:23:56: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:56: MDO formulation: MDF
INFO - 16:23:56: Optimization problem:
INFO - 16:23:56: minimize 0.001*-y_4(x_1)
INFO - 16:23:56: with respect to x_1
INFO - 16:23:56: under the inequality constraints
INFO - 16:23:56: g_1(x_1) <= 0
INFO - 16:23:56: over the design space:
INFO - 16:23:56: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:56: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:56: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:56: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:56: | x_1[1] | 0.75 | 0.7806436836764827 | 1.25 | float |
INFO - 16:23:56: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:56: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:56: 2%|▏ | 1/50 [00:00<00:00, 98.03 it/sec, feas=True, obj=-2.25]
INFO - 16:23:56: Optimization result:
INFO - 16:23:56: Optimizer info:
INFO - 16:23:56: Status: 8
INFO - 16:23:56: Message: Positive directional derivative for linesearch
INFO - 16:23:56: Solution:
INFO - 16:23:56: The solution is feasible.
INFO - 16:23:56: Objective: -2.2514667245970315
INFO - 16:23:56: Standardized constraints:
INFO - 16:23:56: g_1 = [-1.59589593e-03 -2.02868890e-03 -1.31333010e-02 -2.32802973e-02
INFO - 16:23:56: -3.14967236e-02 -2.40000000e-01 1.36557432e-14]
INFO - 16:23:56: Design space:
INFO - 16:23:56: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:56: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:56: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:56: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:56: | x_1[1] | 0.75 | 0.7806436836764827 | 1.25 | float |
INFO - 16:23:56: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:56: *** End StructureScenario execution (time: 0:00:00.012235) ***
INFO - 16:23:56: *** Start PropulsionScenario execution ***
INFO - 16:23:56: PropulsionScenario
INFO - 16:23:56: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:56: MDO formulation: MDF
INFO - 16:23:56: Optimization problem:
INFO - 16:23:56: minimize 0.001*-y_4(x_3)
INFO - 16:23:56: with respect to x_3
INFO - 16:23:56: under the inequality constraints
INFO - 16:23:56: g_3(x_3) <= 0
INFO - 16:23:56: over the design space:
INFO - 16:23:56: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:56: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:56: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:56: | x_3 | 0.1 | 0.1581522009163378 | 1 | float |
INFO - 16:23:56: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:56: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:56: 2%|▏ | 1/50 [00:00<00:00, 90.23 it/sec, feas=True, obj=-2.25]
INFO - 16:23:56: Optimization result:
INFO - 16:23:56: Optimizer info:
INFO - 16:23:56: Status: 8
INFO - 16:23:56: Message: Positive directional derivative for linesearch
INFO - 16:23:56: Solution:
INFO - 16:23:56: The solution is feasible.
INFO - 16:23:56: Objective: -2.2514667245970315
INFO - 16:23:56: Standardized constraints:
INFO - 16:23:56: g_3 = [-8.36419430e-01 -1.63580570e-01 1.33226763e-15 -1.81469033e-01]
INFO - 16:23:56: Design space:
INFO - 16:23:56: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:56: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:56: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:56: | x_3 | 0.1 | 0.1581522009163378 | 1 | float |
INFO - 16:23:56: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:56: *** End PropulsionScenario execution (time: 0:00:00.013051) ***
INFO - 16:23:56: 77%|███████▋ | 77/100 [00:39<00:11, 1.93 it/sec, feas=True, obj=-2.25]
INFO - 16:23:56: *** Start PropulsionScenario execution ***
INFO - 16:23:56: PropulsionScenario
INFO - 16:23:56: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:56: MDO formulation: MDF
INFO - 16:23:56: Optimization problem:
INFO - 16:23:56: minimize 0.001*-y_4(x_3)
INFO - 16:23:56: with respect to x_3
INFO - 16:23:56: under the inequality constraints
INFO - 16:23:56: g_3(x_3) <= 0
INFO - 16:23:56: over the design space:
INFO - 16:23:56: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:56: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:56: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:56: | x_3 | 0.1 | 0.1581522009163378 | 1 | float |
INFO - 16:23:56: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:56: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:56: 2%|▏ | 1/50 [00:00<00:01, 39.94 it/sec, feas=True, obj=-2.25]
INFO - 16:23:56: 4%|▍ | 2/50 [00:00<00:01, 30.54 it/sec, feas=True, obj=-2.25]
INFO - 16:23:56: 6%|▌ | 3/50 [00:00<00:01, 28.34 it/sec, feas=True, obj=-2.25]
INFO - 16:23:56: Optimization result:
INFO - 16:23:56: Optimizer info:
INFO - 16:23:56: Status: 8
INFO - 16:23:56: Message: Positive directional derivative for linesearch
INFO - 16:23:56: Solution:
INFO - 16:23:56: The solution is feasible.
INFO - 16:23:56: Objective: -2.247647353312507
INFO - 16:23:56: Standardized constraints:
INFO - 16:23:56: g_3 = [-0.83611092 -0.16388908 0. -0.18137211]
INFO - 16:23:56: Design space:
INFO - 16:23:56: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:56: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:56: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:56: | x_3 | 0.1 | 0.1582572714662666 | 1 | float |
INFO - 16:23:56: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:56: *** End PropulsionScenario execution (time: 0:00:00.108650) ***
INFO - 16:23:56: *** Start AerodynamicsScenario execution ***
INFO - 16:23:56: AerodynamicsScenario
INFO - 16:23:56: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:56: MDO formulation: MDF
INFO - 16:23:56: Optimization problem:
INFO - 16:23:56: minimize 0.001*-y_4(x_2)
INFO - 16:23:56: with respect to x_2
INFO - 16:23:56: under the inequality constraints
INFO - 16:23:56: g_2(x_2) <= 0
INFO - 16:23:56: over the design space:
INFO - 16:23:56: +------+-------------+-------+-------------+-------+
INFO - 16:23:56: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:56: +------+-------------+-------+-------------+-------+
INFO - 16:23:56: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:56: +------+-------------+-------+-------------+-------+
INFO - 16:23:56: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:56: 2%|▏ | 1/50 [00:00<00:00, 102.59 it/sec, feas=True, obj=-2.25]
INFO - 16:23:56: Optimization result:
INFO - 16:23:56: Optimizer info:
INFO - 16:23:56: Status: 8
INFO - 16:23:56: Message: Positive directional derivative for linesearch
INFO - 16:23:56: Solution:
INFO - 16:23:56: The solution is feasible.
INFO - 16:23:56: Objective: -2.247647353312507
INFO - 16:23:56: Standardized constraints:
INFO - 16:23:56: g_2 = -1.83635906201296e-05
INFO - 16:23:56: Design space:
INFO - 16:23:56: +------+-------------+-------+-------------+-------+
INFO - 16:23:56: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:56: +------+-------------+-------+-------------+-------+
INFO - 16:23:56: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:56: +------+-------------+-------+-------------+-------+
INFO - 16:23:56: *** End AerodynamicsScenario execution (time: 0:00:00.011808) ***
INFO - 16:23:56: *** Start StructureScenario execution ***
INFO - 16:23:56: StructureScenario
INFO - 16:23:56: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:56: MDO formulation: MDF
INFO - 16:23:56: Optimization problem:
INFO - 16:23:56: minimize 0.001*-y_4(x_1)
INFO - 16:23:56: with respect to x_1
INFO - 16:23:56: under the inequality constraints
INFO - 16:23:56: g_1(x_1) <= 0
INFO - 16:23:56: over the design space:
INFO - 16:23:56: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:56: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:56: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:56: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:56: | x_1[1] | 0.75 | 0.7806436836764827 | 1.25 | float |
INFO - 16:23:56: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:56: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:56: 2%|▏ | 1/50 [00:00<00:00, 98.16 it/sec, feas=True, obj=-2.25]
INFO - 16:23:57: 4%|▍ | 2/50 [00:00<00:00, 117.78 it/sec, feas=True, obj=-2.25]
INFO - 16:23:57: 6%|▌ | 3/50 [00:00<00:00, 133.39 it/sec, feas=True, obj=-2.25]
INFO - 16:23:57: Optimization result:
INFO - 16:23:57: Optimizer info:
INFO - 16:23:57: Status: None
INFO - 16:23:57: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:57: Solution:
INFO - 16:23:57: The solution is feasible.
INFO - 16:23:57: Objective: -2.247647353312507
INFO - 16:23:57: Standardized constraints:
INFO - 16:23:57: g_1 = [-1.44874340e-03 -1.94798479e-03 -1.30792970e-02 -2.32402257e-02
INFO - 16:23:57: -3.14650703e-02 -2.40000000e-01 1.36557432e-14]
INFO - 16:23:57: Design space:
INFO - 16:23:57: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:57: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:57: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:57: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:57: | x_1[1] | 0.75 | 0.7806436836764827 | 1.25 | float |
INFO - 16:23:57: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:57: *** End StructureScenario execution (time: 0:00:00.024854) ***
INFO - 16:23:57: *** Start PropulsionScenario execution ***
INFO - 16:23:57: PropulsionScenario
INFO - 16:23:57: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:57: MDO formulation: MDF
INFO - 16:23:57: Optimization problem:
INFO - 16:23:57: minimize 0.001*-y_4(x_3)
INFO - 16:23:57: with respect to x_3
INFO - 16:23:57: under the inequality constraints
INFO - 16:23:57: g_3(x_3) <= 0
INFO - 16:23:57: over the design space:
INFO - 16:23:57: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:57: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:57: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:57: | x_3 | 0.1 | 0.1582572714662666 | 1 | float |
INFO - 16:23:57: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:57: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:57: 2%|▏ | 1/50 [00:00<00:00, 73.40 it/sec, feas=True, obj=-2.25]
INFO - 16:23:57: Optimization result:
INFO - 16:23:57: Optimizer info:
INFO - 16:23:57: Status: 8
INFO - 16:23:57: Message: Positive directional derivative for linesearch
INFO - 16:23:57: Solution:
INFO - 16:23:57: The solution is feasible.
INFO - 16:23:57: Objective: -2.247647353312507
INFO - 16:23:57: Standardized constraints:
INFO - 16:23:57: g_3 = [-0.83611092 -0.16388908 0. -0.18137211]
INFO - 16:23:57: Design space:
INFO - 16:23:57: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:57: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:57: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:57: | x_3 | 0.1 | 0.1582572714662666 | 1 | float |
INFO - 16:23:57: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:57: *** End PropulsionScenario execution (time: 0:00:00.015373) ***
INFO - 16:23:57: 78%|███████▊ | 78/100 [00:40<00:11, 1.94 it/sec, feas=True, obj=-2.25]
INFO - 16:23:57: *** Start PropulsionScenario execution ***
INFO - 16:23:57: PropulsionScenario
INFO - 16:23:57: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:57: MDO formulation: MDF
INFO - 16:23:57: Optimization problem:
INFO - 16:23:57: minimize 0.001*-y_4(x_3)
INFO - 16:23:57: with respect to x_3
INFO - 16:23:57: under the inequality constraints
INFO - 16:23:57: g_3(x_3) <= 0
INFO - 16:23:57: over the design space:
INFO - 16:23:57: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:57: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:57: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:57: | x_3 | 0.1 | 0.1582572714662666 | 1 | float |
INFO - 16:23:57: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:57: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:57: 2%|▏ | 1/50 [00:00<00:01, 38.93 it/sec, feas=False, obj=-2.25]
INFO - 16:23:57: 4%|▍ | 2/50 [00:00<00:01, 39.94 it/sec, feas=True, obj=-2.25]
INFO - 16:23:57: 6%|▌ | 3/50 [00:00<00:01, 33.04 it/sec, feas=False, obj=-2.25]
INFO - 16:23:57: 8%|▊ | 4/50 [00:00<00:01, 30.30 it/sec, feas=True, obj=-2.25]
WARNING - 16:23:57: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 0.00013449864933217252 is still above the tolerance 1e-06.
INFO - 16:23:57: 10%|█ | 5/50 [00:00<00:01, 30.88 it/sec, feas=True, obj=-2.25]
INFO - 16:23:57: 12%|█▏ | 6/50 [00:00<00:01, 31.94 it/sec, feas=True, obj=-2.25]
INFO - 16:23:57: Optimization result:
INFO - 16:23:57: Optimizer info:
INFO - 16:23:57: Status: None
INFO - 16:23:57: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:57: Solution:
INFO - 16:23:57: The solution is feasible.
INFO - 16:23:57: Objective: -2.2521922211537566
INFO - 16:23:57: Standardized constraints:
INFO - 16:23:57: g_3 = [-8.36678291e-01 -1.63321709e-01 1.13242749e-14 -1.81462586e-01]
INFO - 16:23:57: Design space:
INFO - 16:23:57: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:57: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:57: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:57: | x_3 | 0.1 | 0.1581591620922117 | 1 | float |
INFO - 16:23:57: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:57: *** End PropulsionScenario execution (time: 0:00:00.190412) ***
INFO - 16:23:57: *** Start AerodynamicsScenario execution ***
INFO - 16:23:57: AerodynamicsScenario
INFO - 16:23:57: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:57: MDO formulation: MDF
INFO - 16:23:57: Optimization problem:
INFO - 16:23:57: minimize 0.001*-y_4(x_2)
INFO - 16:23:57: with respect to x_2
INFO - 16:23:57: under the inequality constraints
INFO - 16:23:57: g_2(x_2) <= 0
INFO - 16:23:57: over the design space:
INFO - 16:23:57: +------+-------------+-------+-------------+-------+
INFO - 16:23:57: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:57: +------+-------------+-------+-------------+-------+
INFO - 16:23:57: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:57: +------+-------------+-------+-------------+-------+
INFO - 16:23:57: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:57: 2%|▏ | 1/50 [00:00<00:00, 76.53 it/sec, feas=True, obj=-2.25]
INFO - 16:23:57: Optimization result:
INFO - 16:23:57: Optimizer info:
INFO - 16:23:57: Status: 8
INFO - 16:23:57: Message: Positive directional derivative for linesearch
INFO - 16:23:57: Solution:
INFO - 16:23:57: The solution is feasible.
INFO - 16:23:57: Objective: -2.2521922211537566
INFO - 16:23:57: Standardized constraints:
INFO - 16:23:57: g_2 = 0.0
INFO - 16:23:57: Design space:
INFO - 16:23:57: +------+-------------+-------+-------------+-------+
INFO - 16:23:57: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:57: +------+-------------+-------+-------------+-------+
INFO - 16:23:57: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:57: +------+-------------+-------+-------------+-------+
INFO - 16:23:57: *** End AerodynamicsScenario execution (time: 0:00:00.014672) ***
INFO - 16:23:57: *** Start StructureScenario execution ***
INFO - 16:23:57: StructureScenario
INFO - 16:23:57: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:57: MDO formulation: MDF
INFO - 16:23:57: Optimization problem:
INFO - 16:23:57: minimize 0.001*-y_4(x_1)
INFO - 16:23:57: with respect to x_1
INFO - 16:23:57: under the inequality constraints
INFO - 16:23:57: g_1(x_1) <= 0
INFO - 16:23:57: over the design space:
INFO - 16:23:57: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:57: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:57: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:57: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:57: | x_1[1] | 0.75 | 0.7806436836764827 | 1.25 | float |
INFO - 16:23:57: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:57: Solving optimization problem with algorithm SLSQP:
WARNING - 16:23:57: MDAGaussSeidel has reached its maximum number of unsuccessful iterations, but the normalized residual norm 0.0018314954719615695 is still above the tolerance 1e-06.
INFO - 16:23:57: 2%|▏ | 1/50 [00:00<00:00, 53.53 it/sec, feas=True, obj=-2.25]
INFO - 16:23:57: 4%|▍ | 2/50 [00:00<00:01, 45.84 it/sec, feas=True, obj=-2.25]
INFO - 16:23:57: 6%|▌ | 3/50 [00:00<00:01, 43.86 it/sec, feas=True, obj=-2.25]
INFO - 16:23:57: Optimization result:
INFO - 16:23:57: Optimizer info:
INFO - 16:23:57: Status: None
INFO - 16:23:57: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:57: Solution:
INFO - 16:23:57: The solution is feasible.
INFO - 16:23:57: Objective: -2.2521922211537566
INFO - 16:23:57: Standardized constraints:
INFO - 16:23:57: g_1 = [-1.59589593e-03 -2.02868890e-03 -1.31333010e-02 -2.32802973e-02
INFO - 16:23:57: -3.14967236e-02 -2.40000000e-01 1.36557432e-14]
INFO - 16:23:57: Design space:
INFO - 16:23:57: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:57: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:57: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:57: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:57: | x_1[1] | 0.75 | 0.7806436836764827 | 1.25 | float |
INFO - 16:23:57: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:57: *** End StructureScenario execution (time: 0:00:00.071028) ***
WARNING - 16:23:57: MDAGaussSeidel has reached its maximum number of unsuccessful iterations, but the normalized residual norm 0.0018314954719615695 is still above the tolerance 1e-06.
INFO - 16:23:57: *** Start PropulsionScenario execution ***
INFO - 16:23:57: PropulsionScenario
INFO - 16:23:57: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:57: MDO formulation: MDF
INFO - 16:23:57: Optimization problem:
INFO - 16:23:57: minimize 0.001*-y_4(x_3)
INFO - 16:23:57: with respect to x_3
INFO - 16:23:57: under the inequality constraints
INFO - 16:23:57: g_3(x_3) <= 0
INFO - 16:23:57: over the design space:
INFO - 16:23:57: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:57: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:57: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:57: | x_3 | 0.1 | 0.1581591620922117 | 1 | float |
INFO - 16:23:57: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:57: Solving optimization problem with algorithm SLSQP:
WARNING - 16:23:57: MDAGaussSeidel has reached its maximum number of unsuccessful iterations, but the normalized residual norm 0.00013449864933217252 is still above the tolerance 1e-06.
INFO - 16:23:57: 2%|▏ | 1/50 [00:00<00:00, 51.08 it/sec, feas=True, obj=-2.25]
INFO - 16:23:57: Optimization result:
INFO - 16:23:57: Optimizer info:
INFO - 16:23:57: Status: 8
INFO - 16:23:57: Message: Positive directional derivative for linesearch
INFO - 16:23:57: Solution:
INFO - 16:23:57: The solution is feasible.
INFO - 16:23:57: Objective: -2.2521922211537566
INFO - 16:23:57: Standardized constraints:
INFO - 16:23:57: g_3 = [-8.36678291e-01 -1.63321709e-01 1.13242749e-14 -1.81462586e-01]
INFO - 16:23:57: Design space:
INFO - 16:23:57: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:57: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:57: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:57: | x_3 | 0.1 | 0.1581591620922117 | 1 | float |
INFO - 16:23:57: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:57: *** End PropulsionScenario execution (time: 0:00:00.021520) ***
INFO - 16:23:57: *** Start AerodynamicsScenario execution ***
INFO - 16:23:57: AerodynamicsScenario
INFO - 16:23:57: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:57: MDO formulation: MDF
INFO - 16:23:57: Optimization problem:
INFO - 16:23:57: minimize 0.001*-y_4(x_2)
INFO - 16:23:57: with respect to x_2
INFO - 16:23:57: under the inequality constraints
INFO - 16:23:57: g_2(x_2) <= 0
INFO - 16:23:57: over the design space:
INFO - 16:23:57: +------+-------------+-------+-------------+-------+
INFO - 16:23:57: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:57: +------+-------------+-------+-------------+-------+
INFO - 16:23:57: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:57: +------+-------------+-------+-------------+-------+
INFO - 16:23:57: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:57: 2%|▏ | 1/50 [00:00<00:00, 82.71 it/sec, feas=True, obj=-2.25]
INFO - 16:23:57: Optimization result:
INFO - 16:23:57: Optimizer info:
INFO - 16:23:57: Status: 8
INFO - 16:23:57: Message: Positive directional derivative for linesearch
INFO - 16:23:57: Solution:
INFO - 16:23:57: The solution is feasible.
INFO - 16:23:57: Objective: -2.2521922211537566
INFO - 16:23:57: Standardized constraints:
INFO - 16:23:57: g_2 = 0.0
INFO - 16:23:57: Design space:
INFO - 16:23:57: +------+-------------+-------+-------------+-------+
INFO - 16:23:57: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:57: +------+-------------+-------+-------------+-------+
INFO - 16:23:57: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:57: +------+-------------+-------+-------------+-------+
INFO - 16:23:57: *** End AerodynamicsScenario execution (time: 0:00:00.013821) ***
INFO - 16:23:57: 79%|███████▉ | 79/100 [00:40<00:10, 1.95 it/sec, feas=True, obj=-2.25]
INFO - 16:23:57: *** Start PropulsionScenario execution ***
INFO - 16:23:57: PropulsionScenario
INFO - 16:23:57: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:57: MDO formulation: MDF
INFO - 16:23:57: Optimization problem:
INFO - 16:23:57: minimize 0.001*-y_4(x_3)
INFO - 16:23:57: with respect to x_3
INFO - 16:23:57: under the inequality constraints
INFO - 16:23:57: g_3(x_3) <= 0
INFO - 16:23:57: over the design space:
INFO - 16:23:57: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:57: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:57: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:57: | x_3 | 0.1 | 0.1581591620922117 | 1 | float |
INFO - 16:23:57: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:57: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:57: 2%|▏ | 1/50 [00:00<00:01, 39.78 it/sec, feas=True, obj=-2.25]
INFO - 16:23:57: 4%|▍ | 2/50 [00:00<00:01, 30.45 it/sec, feas=True, obj=-2.25]
INFO - 16:23:57: 6%|▌ | 3/50 [00:00<00:01, 28.28 it/sec, feas=True, obj=-2.25]
INFO - 16:23:57: 8%|▊ | 4/50 [00:00<00:01, 30.63 it/sec, feas=True, obj=-2.25]
INFO - 16:23:57: Optimization result:
INFO - 16:23:57: Optimizer info:
INFO - 16:23:57: Status: None
INFO - 16:23:57: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:57: Solution:
INFO - 16:23:57: The solution is feasible.
INFO - 16:23:57: Objective: -2.24849707701976
INFO - 16:23:57: Standardized constraints:
INFO - 16:23:57: g_3 = [-8.36385219e-01 -1.63614781e-01 7.54951657e-15 -1.81372451e-01]
INFO - 16:23:57: Design space:
INFO - 16:23:57: +------+-------------+-------------------+-------------+-------+
INFO - 16:23:57: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:57: +------+-------------+-------------------+-------------+-------+
INFO - 16:23:57: | x_3 | 0.1 | 0.158270272045432 | 1 | float |
INFO - 16:23:57: +------+-------------+-------------------+-------------+-------+
INFO - 16:23:57: *** End PropulsionScenario execution (time: 0:00:00.133172) ***
INFO - 16:23:57: *** Start AerodynamicsScenario execution ***
INFO - 16:23:57: AerodynamicsScenario
INFO - 16:23:57: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:57: MDO formulation: MDF
INFO - 16:23:57: Optimization problem:
INFO - 16:23:57: minimize 0.001*-y_4(x_2)
INFO - 16:23:57: with respect to x_2
INFO - 16:23:57: under the inequality constraints
INFO - 16:23:57: g_2(x_2) <= 0
INFO - 16:23:57: over the design space:
INFO - 16:23:57: +------+-------------+-------+-------------+-------+
INFO - 16:23:57: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:57: +------+-------------+-------+-------------+-------+
INFO - 16:23:57: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:57: +------+-------------+-------+-------------+-------+
INFO - 16:23:57: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:57: 2%|▏ | 1/50 [00:00<00:00, 87.86 it/sec, feas=True, obj=-2.25]
INFO - 16:23:57: Optimization result:
INFO - 16:23:57: Optimizer info:
INFO - 16:23:57: Status: 8
INFO - 16:23:57: Message: Positive directional derivative for linesearch
INFO - 16:23:57: Solution:
INFO - 16:23:57: The solution is feasible.
INFO - 16:23:57: Objective: -2.24849707701976
INFO - 16:23:57: Standardized constraints:
INFO - 16:23:57: g_2 = 1.3145698177341458e-05
INFO - 16:23:57: Design space:
INFO - 16:23:57: +------+-------------+-------+-------------+-------+
INFO - 16:23:57: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:57: +------+-------------+-------+-------------+-------+
INFO - 16:23:57: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:57: +------+-------------+-------+-------------+-------+
INFO - 16:23:57: *** End AerodynamicsScenario execution (time: 0:00:00.013271) ***
INFO - 16:23:57: *** Start StructureScenario execution ***
INFO - 16:23:57: StructureScenario
INFO - 16:23:57: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:57: MDO formulation: MDF
INFO - 16:23:57: Optimization problem:
INFO - 16:23:57: minimize 0.001*-y_4(x_1)
INFO - 16:23:57: with respect to x_1
INFO - 16:23:57: under the inequality constraints
INFO - 16:23:57: g_1(x_1) <= 0
INFO - 16:23:57: over the design space:
INFO - 16:23:57: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:57: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:57: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:57: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:57: | x_1[1] | 0.75 | 0.7806436836764827 | 1.25 | float |
INFO - 16:23:57: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:57: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:57: 2%|▏ | 1/50 [00:00<00:00, 94.48 it/sec, feas=True, obj=-2.25]
INFO - 16:23:57: 4%|▍ | 2/50 [00:00<00:00, 105.60 it/sec, feas=True, obj=-2.25]
INFO - 16:23:57: 6%|▌ | 3/50 [00:00<00:00, 114.50 it/sec, feas=True, obj=-2.25]
INFO - 16:23:57: Optimization result:
INFO - 16:23:57: Optimizer info:
INFO - 16:23:57: Status: None
INFO - 16:23:57: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:57: Solution:
INFO - 16:23:57: The solution is feasible.
INFO - 16:23:57: Objective: -2.24849707701976
INFO - 16:23:57: Standardized constraints:
INFO - 16:23:57: g_1 = [-1.70124898e-03 -2.08646723e-03 -1.31719634e-02 -2.33089849e-02
INFO - 16:23:57: -3.15193842e-02 -2.40000000e-01 1.36557432e-14]
INFO - 16:23:57: Design space:
INFO - 16:23:57: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:57: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:57: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:57: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:57: | x_1[1] | 0.75 | 0.7806436836764827 | 1.25 | float |
INFO - 16:23:57: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:57: *** End StructureScenario execution (time: 0:00:00.028900) ***
INFO - 16:23:57: *** Start PropulsionScenario execution ***
INFO - 16:23:57: PropulsionScenario
INFO - 16:23:57: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:57: MDO formulation: MDF
INFO - 16:23:57: Optimization problem:
INFO - 16:23:57: minimize 0.001*-y_4(x_3)
INFO - 16:23:57: with respect to x_3
INFO - 16:23:57: under the inequality constraints
INFO - 16:23:57: g_3(x_3) <= 0
INFO - 16:23:57: over the design space:
INFO - 16:23:57: +------+-------------+-------------------+-------------+-------+
INFO - 16:23:57: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:57: +------+-------------+-------------------+-------------+-------+
INFO - 16:23:57: | x_3 | 0.1 | 0.158270272045432 | 1 | float |
INFO - 16:23:57: +------+-------------+-------------------+-------------+-------+
INFO - 16:23:57: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:57: 2%|▏ | 1/50 [00:00<00:00, 87.18 it/sec, feas=True, obj=-2.25]
INFO - 16:23:57: Optimization result:
INFO - 16:23:57: Optimizer info:
INFO - 16:23:57: Status: 8
INFO - 16:23:57: Message: Positive directional derivative for linesearch
INFO - 16:23:57: Solution:
INFO - 16:23:57: The solution is feasible.
INFO - 16:23:57: Objective: -2.24849707701976
INFO - 16:23:57: Standardized constraints:
INFO - 16:23:57: g_3 = [-8.36385219e-01 -1.63614781e-01 7.54951657e-15 -1.81372451e-01]
INFO - 16:23:57: Design space:
INFO - 16:23:57: +------+-------------+-------------------+-------------+-------+
INFO - 16:23:57: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:57: +------+-------------+-------------------+-------------+-------+
INFO - 16:23:57: | x_3 | 0.1 | 0.158270272045432 | 1 | float |
INFO - 16:23:57: +------+-------------+-------------------+-------------+-------+
INFO - 16:23:57: *** End PropulsionScenario execution (time: 0:00:00.013478) ***
INFO - 16:23:57: 80%|████████ | 80/100 [00:40<00:10, 1.96 it/sec, feas=True, obj=-2.25]
INFO - 16:23:57: *** Start PropulsionScenario execution ***
INFO - 16:23:57: PropulsionScenario
INFO - 16:23:57: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:57: MDO formulation: MDF
INFO - 16:23:57: Optimization problem:
INFO - 16:23:57: minimize 0.001*-y_4(x_3)
INFO - 16:23:57: with respect to x_3
INFO - 16:23:57: under the inequality constraints
INFO - 16:23:57: g_3(x_3) <= 0
INFO - 16:23:57: over the design space:
INFO - 16:23:57: +------+-------------+-------------------+-------------+-------+
INFO - 16:23:57: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:57: +------+-------------+-------------------+-------------+-------+
INFO - 16:23:57: | x_3 | 0.1 | 0.158270272045432 | 1 | float |
INFO - 16:23:57: +------+-------------+-------------------+-------------+-------+
INFO - 16:23:57: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:57: 2%|▏ | 1/50 [00:00<00:01, 39.40 it/sec, feas=False, obj=-2.25]
INFO - 16:23:57: 4%|▍ | 2/50 [00:00<00:01, 41.14 it/sec, feas=True, obj=-2.25]
INFO - 16:23:57: 6%|▌ | 3/50 [00:00<00:01, 34.31 it/sec, feas=False, obj=-2.25]
INFO - 16:23:57: 8%|▊ | 4/50 [00:00<00:01, 31.26 it/sec, feas=True, obj=-2.25]
INFO - 16:23:57: 10%|█ | 5/50 [00:00<00:01, 31.60 it/sec, feas=True, obj=-2.25]
INFO - 16:23:57: Optimization result:
INFO - 16:23:57: Optimizer info:
INFO - 16:23:57: Status: 8
INFO - 16:23:57: Message: Positive directional derivative for linesearch
INFO - 16:23:57: Solution:
INFO - 16:23:57: The solution is feasible.
INFO - 16:23:57: Objective: -2.252524402392841
INFO - 16:23:57: Standardized constraints:
INFO - 16:23:57: g_3 = [-0.83624833 -0.16375167 0. -0.18145206]
INFO - 16:23:57: Design space:
INFO - 16:23:57: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:57: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:57: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:57: | x_3 | 0.1 | 0.1581705258092849 | 1 | float |
INFO - 16:23:57: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:57: *** End PropulsionScenario execution (time: 0:00:00.160906) ***
INFO - 16:23:57: *** Start AerodynamicsScenario execution ***
INFO - 16:23:57: AerodynamicsScenario
INFO - 16:23:57: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:57: MDO formulation: MDF
INFO - 16:23:57: Optimization problem:
INFO - 16:23:57: minimize 0.001*-y_4(x_2)
INFO - 16:23:57: with respect to x_2
INFO - 16:23:57: under the inequality constraints
INFO - 16:23:57: g_2(x_2) <= 0
INFO - 16:23:57: over the design space:
INFO - 16:23:57: +------+-------------+-------+-------------+-------+
INFO - 16:23:57: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:57: +------+-------------+-------+-------------+-------+
INFO - 16:23:57: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:57: +------+-------------+-------+-------------+-------+
INFO - 16:23:57: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:57: 2%|▏ | 1/50 [00:00<00:00, 85.06 it/sec, feas=True, obj=-2.25]
INFO - 16:23:57: Optimization result:
INFO - 16:23:57: Optimizer info:
INFO - 16:23:57: Status: 8
INFO - 16:23:57: Message: Positive directional derivative for linesearch
INFO - 16:23:57: Solution:
INFO - 16:23:57: The solution is feasible.
INFO - 16:23:57: Objective: -2.252524402392841
INFO - 16:23:57: Standardized constraints:
INFO - 16:23:57: g_2 = -2.220446049250313e-16
INFO - 16:23:57: Design space:
INFO - 16:23:57: +------+-------------+-------+-------------+-------+
INFO - 16:23:57: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:57: +------+-------------+-------+-------------+-------+
INFO - 16:23:57: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:57: +------+-------------+-------+-------------+-------+
INFO - 16:23:57: *** End AerodynamicsScenario execution (time: 0:00:00.013441) ***
INFO - 16:23:57: *** Start StructureScenario execution ***
INFO - 16:23:57: StructureScenario
INFO - 16:23:57: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:57: MDO formulation: MDF
INFO - 16:23:57: Optimization problem:
INFO - 16:23:57: minimize 0.001*-y_4(x_1)
INFO - 16:23:57: with respect to x_1
INFO - 16:23:57: under the inequality constraints
INFO - 16:23:57: g_1(x_1) <= 0
INFO - 16:23:57: over the design space:
INFO - 16:23:57: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:57: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:57: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:57: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:57: | x_1[1] | 0.75 | 0.7806436836764827 | 1.25 | float |
INFO - 16:23:57: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:57: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:57: 2%|▏ | 1/50 [00:00<00:00, 97.20 it/sec, feas=True, obj=-2.25]
INFO - 16:23:57: Optimization result:
INFO - 16:23:57: Optimizer info:
INFO - 16:23:57: Status: 8
INFO - 16:23:57: Message: Positive directional derivative for linesearch
INFO - 16:23:57: Solution:
INFO - 16:23:57: The solution is feasible.
INFO - 16:23:57: Objective: -2.252524402392841
INFO - 16:23:57: Standardized constraints:
INFO - 16:23:57: g_1 = [-1.59589593e-03 -2.02868890e-03 -1.31333010e-02 -2.32802973e-02
INFO - 16:23:57: -3.14967236e-02 -2.40000000e-01 1.36557432e-14]
INFO - 16:23:57: Design space:
INFO - 16:23:57: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:57: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:57: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:57: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:57: | x_1[1] | 0.75 | 0.7806436836764827 | 1.25 | float |
INFO - 16:23:57: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:57: *** End StructureScenario execution (time: 0:00:00.012344) ***
INFO - 16:23:57: *** Start PropulsionScenario execution ***
INFO - 16:23:57: PropulsionScenario
INFO - 16:23:57: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:57: MDO formulation: MDF
INFO - 16:23:57: Optimization problem:
INFO - 16:23:57: minimize 0.001*-y_4(x_3)
INFO - 16:23:57: with respect to x_3
INFO - 16:23:57: under the inequality constraints
INFO - 16:23:57: g_3(x_3) <= 0
INFO - 16:23:57: over the design space:
INFO - 16:23:57: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:57: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:57: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:57: | x_3 | 0.1 | 0.1581705258092849 | 1 | float |
INFO - 16:23:57: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:57: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:57: 2%|▏ | 1/50 [00:00<00:00, 109.68 it/sec, feas=True, obj=-2.25]
INFO - 16:23:57: Optimization result:
INFO - 16:23:57: Optimizer info:
INFO - 16:23:57: Status: 8
INFO - 16:23:57: Message: Positive directional derivative for linesearch
INFO - 16:23:57: Solution:
INFO - 16:23:57: The solution is feasible.
INFO - 16:23:57: Objective: -2.252524402392841
INFO - 16:23:57: Standardized constraints:
INFO - 16:23:57: g_3 = [-0.83624833 -0.16375167 0. -0.18145206]
INFO - 16:23:57: Design space:
INFO - 16:23:57: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:57: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:57: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:57: | x_3 | 0.1 | 0.1581705258092849 | 1 | float |
INFO - 16:23:57: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:57: *** End PropulsionScenario execution (time: 0:00:00.010766) ***
INFO - 16:23:57: *** Start AerodynamicsScenario execution ***
INFO - 16:23:57: AerodynamicsScenario
INFO - 16:23:57: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:57: MDO formulation: MDF
INFO - 16:23:57: Optimization problem:
INFO - 16:23:57: minimize 0.001*-y_4(x_2)
INFO - 16:23:57: with respect to x_2
INFO - 16:23:57: under the inequality constraints
INFO - 16:23:57: g_2(x_2) <= 0
INFO - 16:23:57: over the design space:
INFO - 16:23:57: +------+-------------+-------+-------------+-------+
INFO - 16:23:57: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:57: +------+-------------+-------+-------------+-------+
INFO - 16:23:57: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:57: +------+-------------+-------+-------------+-------+
INFO - 16:23:57: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:57: 2%|▏ | 1/50 [00:00<00:00, 110.14 it/sec, feas=True, obj=-2.25]
INFO - 16:23:57: Optimization result:
INFO - 16:23:57: Optimizer info:
INFO - 16:23:57: Status: 8
INFO - 16:23:57: Message: Positive directional derivative for linesearch
INFO - 16:23:57: Solution:
INFO - 16:23:57: The solution is feasible.
INFO - 16:23:57: Objective: -2.252524402392841
INFO - 16:23:57: Standardized constraints:
INFO - 16:23:57: g_2 = -2.220446049250313e-16
INFO - 16:23:57: Design space:
INFO - 16:23:57: +------+-------------+-------+-------------+-------+
INFO - 16:23:57: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:57: +------+-------------+-------+-------------+-------+
INFO - 16:23:57: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:57: +------+-------------+-------+-------------+-------+
INFO - 16:23:57: *** End AerodynamicsScenario execution (time: 0:00:00.010636) ***
INFO - 16:23:57: 81%|████████ | 81/100 [00:40<00:09, 1.98 it/sec, feas=True, obj=-2.25]
INFO - 16:23:57: *** Start PropulsionScenario execution ***
INFO - 16:23:57: PropulsionScenario
INFO - 16:23:57: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:57: MDO formulation: MDF
INFO - 16:23:57: Optimization problem:
INFO - 16:23:57: minimize 0.001*-y_4(x_3)
INFO - 16:23:57: with respect to x_3
INFO - 16:23:57: under the inequality constraints
INFO - 16:23:57: g_3(x_3) <= 0
INFO - 16:23:57: over the design space:
INFO - 16:23:57: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:57: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:57: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:57: | x_3 | 0.1 | 0.1581705258092849 | 1 | float |
INFO - 16:23:57: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:57: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:57: 2%|▏ | 1/50 [00:00<00:01, 39.83 it/sec, feas=True, obj=-2.25]
INFO - 16:23:57: 4%|▍ | 2/50 [00:00<00:01, 30.51 it/sec, feas=True, obj=-2.25]
INFO - 16:23:57: Optimization result:
INFO - 16:23:57: Optimizer info:
INFO - 16:23:57: Status: 8
INFO - 16:23:57: Message: Positive directional derivative for linesearch
INFO - 16:23:57: Solution:
INFO - 16:23:57: The solution is feasible.
INFO - 16:23:57: Objective: -2.249232855975866
INFO - 16:23:57: Standardized constraints:
INFO - 16:23:57: g_3 = [-8.36215562e-01 -1.63784438e-01 2.22044605e-16 -1.81371775e-01]
INFO - 16:23:57: Design space:
INFO - 16:23:57: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:57: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:57: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:57: | x_3 | 0.1 | 0.1582610963613389 | 1 | float |
INFO - 16:23:57: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:57: *** End PropulsionScenario execution (time: 0:00:00.067846) ***
INFO - 16:23:57: *** Start AerodynamicsScenario execution ***
INFO - 16:23:57: AerodynamicsScenario
INFO - 16:23:57: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:57: MDO formulation: MDF
INFO - 16:23:57: Optimization problem:
INFO - 16:23:57: minimize 0.001*-y_4(x_2)
INFO - 16:23:57: with respect to x_2
INFO - 16:23:57: under the inequality constraints
INFO - 16:23:57: g_2(x_2) <= 0
INFO - 16:23:57: over the design space:
INFO - 16:23:57: +------+-------------+-------+-------------+-------+
INFO - 16:23:57: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:57: +------+-------------+-------+-------------+-------+
INFO - 16:23:57: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:57: +------+-------------+-------+-------------+-------+
INFO - 16:23:57: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:57: 2%|▏ | 1/50 [00:00<00:00, 104.63 it/sec, feas=False, obj=-2.25]
INFO - 16:23:57: 4%|▍ | 2/50 [00:00<00:00, 163.56 it/sec, feas=False, obj=-2.25]
INFO - 16:23:57: 6%|▌ | 3/50 [00:00<00:00, 201.52 it/sec, feas=False, obj=-2.25]
INFO - 16:23:57: 8%|▊ | 4/50 [00:00<00:00, 226.25 it/sec, feas=False, obj=-2.25]
INFO - 16:23:57: 10%|█ | 5/50 [00:00<00:00, 244.36 it/sec, feas=False, obj=-2.25]
INFO - 16:23:57: 12%|█▏ | 6/50 [00:00<00:00, 262.96 it/sec, feas=False, obj=-2.25]
INFO - 16:23:57: 14%|█▍ | 7/50 [00:00<00:00, 279.02 it/sec, feas=False, obj=-2.25]
INFO - 16:23:57: 16%|█▌ | 8/50 [00:00<00:00, 280.34 it/sec, feas=False, obj=-2.25]
INFO - 16:23:57: 18%|█▊ | 9/50 [00:00<00:00, 282.36 it/sec, feas=False, obj=-2.25]
WARNING - 16:23:57: Optimization found no feasible point; the least infeasible point is selected.
INFO - 16:23:57: 20%|██ | 10/50 [00:00<00:00, 244.27 it/sec, feas=False, obj=-2.25]
INFO - 16:23:57: Optimization result:
INFO - 16:23:57: Optimizer info:
INFO - 16:23:57: Status: 8
INFO - 16:23:57: Message: Positive directional derivative for linesearch
INFO - 16:23:57: Solution:
WARNING - 16:23:57: The solution is not feasible.
INFO - 16:23:57: Objective: -2.249232855975866
INFO - 16:23:57: Standardized constraints:
INFO - 16:23:57: g_2 = 0.00013795143625117134
INFO - 16:23:57: Design space:
INFO - 16:23:57: +------+-------------+-------+-------------+-------+
INFO - 16:23:57: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:57: +------+-------------+-------+-------------+-------+
INFO - 16:23:57: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:57: +------+-------------+-------+-------------+-------+
INFO - 16:23:57: *** End AerodynamicsScenario execution (time: 0:00:00.042565) ***
INFO - 16:23:57: *** Start StructureScenario execution ***
INFO - 16:23:57: StructureScenario
INFO - 16:23:57: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:57: MDO formulation: MDF
INFO - 16:23:58: Optimization problem:
INFO - 16:23:58: minimize 0.001*-y_4(x_1)
INFO - 16:23:58: with respect to x_1
INFO - 16:23:58: under the inequality constraints
INFO - 16:23:58: g_1(x_1) <= 0
INFO - 16:23:58: over the design space:
INFO - 16:23:58: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:58: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:58: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:58: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:58: | x_1[1] | 0.75 | 0.7806436836764827 | 1.25 | float |
INFO - 16:23:58: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:58: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:58: 2%|▏ | 1/50 [00:00<00:00, 71.95 it/sec, feas=True, obj=-2.25]
WARNING - 16:23:58: MDAGaussSeidel has reached its maximum number of unsuccessful iterations, but the normalized residual norm 0.0009157477359807847 is still above the tolerance 1e-06.
INFO - 16:23:58: 4%|▍ | 2/50 [00:00<00:01, 40.89 it/sec, feas=True, obj=-2.25]
INFO - 16:23:58: 6%|▌ | 3/50 [00:00<00:01, 40.58 it/sec, feas=True, obj=-2.25]
INFO - 16:23:58: Optimization result:
INFO - 16:23:58: Optimizer info:
INFO - 16:23:58: Status: 8
INFO - 16:23:58: Message: Positive directional derivative for linesearch
INFO - 16:23:58: Solution:
INFO - 16:23:58: The solution is feasible.
INFO - 16:23:58: Objective: -2.249232855975866
INFO - 16:23:58: Standardized constraints:
INFO - 16:23:58: g_1 = [-2.70201276e-03 -2.63525591e-03 -1.35391597e-02 -2.35814323e-02
INFO - 16:23:58: -3.17345850e-02 -2.40000000e-01 1.36557432e-14]
INFO - 16:23:58: Design space:
INFO - 16:23:58: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:58: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:58: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:58: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:58: | x_1[1] | 0.75 | 0.7806436836764827 | 1.25 | float |
INFO - 16:23:58: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:58: *** End StructureScenario execution (time: 0:00:00.075847) ***
INFO - 16:23:58: *** Start PropulsionScenario execution ***
INFO - 16:23:58: PropulsionScenario
INFO - 16:23:58: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:58: MDO formulation: MDF
INFO - 16:23:58: Optimization problem:
INFO - 16:23:58: minimize 0.001*-y_4(x_3)
INFO - 16:23:58: with respect to x_3
INFO - 16:23:58: under the inequality constraints
INFO - 16:23:58: g_3(x_3) <= 0
INFO - 16:23:58: over the design space:
INFO - 16:23:58: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:58: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:58: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:58: | x_3 | 0.1 | 0.1582610963613389 | 1 | float |
INFO - 16:23:58: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:58: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:58: 2%|▏ | 1/50 [00:00<00:00, 92.37 it/sec, feas=True, obj=-2.25]
INFO - 16:23:58: Optimization result:
INFO - 16:23:58: Optimizer info:
INFO - 16:23:58: Status: 8
INFO - 16:23:58: Message: Positive directional derivative for linesearch
INFO - 16:23:58: Solution:
INFO - 16:23:58: The solution is feasible.
INFO - 16:23:58: Objective: -2.249232855975866
INFO - 16:23:58: Standardized constraints:
INFO - 16:23:58: g_3 = [-8.36215562e-01 -1.63784438e-01 2.22044605e-16 -1.81371775e-01]
INFO - 16:23:58: Design space:
INFO - 16:23:58: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:58: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:58: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:58: | x_3 | 0.1 | 0.1582610963613389 | 1 | float |
INFO - 16:23:58: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:58: *** End PropulsionScenario execution (time: 0:00:00.012541) ***
INFO - 16:23:58: 82%|████████▏ | 82/100 [00:41<00:09, 1.99 it/sec, feas=False, obj=-2.25]
INFO - 16:23:58: *** Start PropulsionScenario execution ***
INFO - 16:23:58: PropulsionScenario
INFO - 16:23:58: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:58: MDO formulation: MDF
INFO - 16:23:58: Optimization problem:
INFO - 16:23:58: minimize 0.001*-y_4(x_3)
INFO - 16:23:58: with respect to x_3
INFO - 16:23:58: under the inequality constraints
INFO - 16:23:58: g_3(x_3) <= 0
INFO - 16:23:58: over the design space:
INFO - 16:23:58: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:58: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:58: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:58: | x_3 | 0.1 | 0.1582610963613389 | 1 | float |
INFO - 16:23:58: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:58: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:58: 2%|▏ | 1/50 [00:00<00:01, 39.80 it/sec, feas=False, obj=-2.25]
INFO - 16:23:58: 4%|▍ | 2/50 [00:00<00:01, 40.43 it/sec, feas=True, obj=-2.25]
WARNING - 16:23:58: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 6.724932466608626e-05 is still above the tolerance 1e-06.
INFO - 16:23:58: 6%|▌ | 3/50 [00:00<00:01, 31.18 it/sec, feas=False, obj=-2.25]
INFO - 16:23:58: 8%|▊ | 4/50 [00:00<00:01, 29.28 it/sec, feas=True, obj=-2.25]
INFO - 16:23:58: 10%|█ | 5/50 [00:00<00:01, 28.17 it/sec, feas=True, obj=-2.25]
INFO - 16:23:58: Optimization result:
INFO - 16:23:58: Optimizer info:
INFO - 16:23:58: Status: 8
INFO - 16:23:58: Message: Positive directional derivative for linesearch
INFO - 16:23:58: Solution:
INFO - 16:23:58: The solution is feasible.
INFO - 16:23:58: Objective: -2.250821760291785
INFO - 16:23:58: Standardized constraints:
INFO - 16:23:58: g_3 = [-8.36477056e-01 -1.63522944e-01 1.04360964e-14 -1.81460346e-01]
INFO - 16:23:58: Design space:
INFO - 16:23:58: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:58: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:58: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:58: | x_3 | 0.1 | 0.1581615810972491 | 1 | float |
INFO - 16:23:58: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:58: *** End PropulsionScenario execution (time: 0:00:00.179581) ***
INFO - 16:23:58: *** Start AerodynamicsScenario execution ***
INFO - 16:23:58: AerodynamicsScenario
INFO - 16:23:58: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:58: MDO formulation: MDF
INFO - 16:23:58: Optimization problem:
INFO - 16:23:58: minimize 0.001*-y_4(x_2)
INFO - 16:23:58: with respect to x_2
INFO - 16:23:58: under the inequality constraints
INFO - 16:23:58: g_2(x_2) <= 0
INFO - 16:23:58: over the design space:
INFO - 16:23:58: +------+-------------+-------+-------------+-------+
INFO - 16:23:58: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:58: +------+-------------+-------+-------------+-------+
INFO - 16:23:58: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:58: +------+-------------+-------+-------------+-------+
INFO - 16:23:58: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:58: 2%|▏ | 1/50 [00:00<00:00, 75.89 it/sec, feas=True, obj=-2.25]
INFO - 16:23:58: Optimization result:
INFO - 16:23:58: Optimizer info:
INFO - 16:23:58: Status: 8
INFO - 16:23:58: Message: Positive directional derivative for linesearch
INFO - 16:23:58: Solution:
INFO - 16:23:58: The solution is feasible.
INFO - 16:23:58: Objective: -2.2508217602917857
INFO - 16:23:58: Standardized constraints:
INFO - 16:23:58: g_2 = -0.00014442752851806517
INFO - 16:23:58: Design space:
INFO - 16:23:58: +------+-------------+-------+-------------+-------+
INFO - 16:23:58: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:58: +------+-------------+-------+-------------+-------+
INFO - 16:23:58: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:58: +------+-------------+-------+-------------+-------+
INFO - 16:23:58: *** End AerodynamicsScenario execution (time: 0:00:00.014928) ***
INFO - 16:23:58: *** Start StructureScenario execution ***
INFO - 16:23:58: StructureScenario
INFO - 16:23:58: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:58: MDO formulation: MDF
INFO - 16:23:58: Optimization problem:
INFO - 16:23:58: minimize 0.001*-y_4(x_1)
INFO - 16:23:58: with respect to x_1
INFO - 16:23:58: under the inequality constraints
INFO - 16:23:58: g_1(x_1) <= 0
INFO - 16:23:58: over the design space:
INFO - 16:23:58: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:58: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:58: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:58: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:58: | x_1[1] | 0.75 | 0.7806436836764827 | 1.25 | float |
INFO - 16:23:58: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:58: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:58: 2%|▏ | 1/50 [00:00<00:00, 82.10 it/sec, feas=True, obj=-2.25]
INFO - 16:23:58: Optimization result:
INFO - 16:23:58: Optimizer info:
INFO - 16:23:58: Status: 8
INFO - 16:23:58: Message: Positive directional derivative for linesearch
INFO - 16:23:58: Solution:
INFO - 16:23:58: The solution is feasible.
INFO - 16:23:58: Objective: -2.250821760291785
INFO - 16:23:58: Standardized constraints:
INFO - 16:23:58: g_1 = [-4.39127224e-04 -1.39421321e-03 -1.27087081e-02 -2.29652296e-02
INFO - 16:23:58: -3.12478375e-02 -2.40000000e-01 1.36557432e-14]
INFO - 16:23:58: Design space:
INFO - 16:23:58: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:58: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:58: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:58: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:58: | x_1[1] | 0.75 | 0.7806436836764827 | 1.25 | float |
INFO - 16:23:58: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:58: *** End StructureScenario execution (time: 0:00:00.014043) ***
INFO - 16:23:58: *** Start PropulsionScenario execution ***
INFO - 16:23:58: PropulsionScenario
INFO - 16:23:58: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:58: MDO formulation: MDF
INFO - 16:23:58: Optimization problem:
INFO - 16:23:58: minimize 0.001*-y_4(x_3)
INFO - 16:23:58: with respect to x_3
INFO - 16:23:58: under the inequality constraints
INFO - 16:23:58: g_3(x_3) <= 0
INFO - 16:23:58: over the design space:
INFO - 16:23:58: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:58: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:58: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:58: | x_3 | 0.1 | 0.1581615810972491 | 1 | float |
INFO - 16:23:58: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:58: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:58: 2%|▏ | 1/50 [00:00<00:00, 108.03 it/sec, feas=True, obj=-2.25]
INFO - 16:23:58: Optimization result:
INFO - 16:23:58: Optimizer info:
INFO - 16:23:58: Status: 8
INFO - 16:23:58: Message: Positive directional derivative for linesearch
INFO - 16:23:58: Solution:
INFO - 16:23:58: The solution is feasible.
INFO - 16:23:58: Objective: -2.250821760291785
INFO - 16:23:58: Standardized constraints:
INFO - 16:23:58: g_3 = [-8.36477056e-01 -1.63522944e-01 1.04360964e-14 -1.81460346e-01]
INFO - 16:23:58: Design space:
INFO - 16:23:58: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:58: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:58: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:58: | x_3 | 0.1 | 0.1581615810972491 | 1 | float |
INFO - 16:23:58: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:58: *** End PropulsionScenario execution (time: 0:00:00.011167) ***
INFO - 16:23:58: *** Start AerodynamicsScenario execution ***
INFO - 16:23:58: AerodynamicsScenario
INFO - 16:23:58: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:58: MDO formulation: MDF
INFO - 16:23:58: Optimization problem:
INFO - 16:23:58: minimize 0.001*-y_4(x_2)
INFO - 16:23:58: with respect to x_2
INFO - 16:23:58: under the inequality constraints
INFO - 16:23:58: g_2(x_2) <= 0
INFO - 16:23:58: over the design space:
INFO - 16:23:58: +------+-------------+-------+-------------+-------+
INFO - 16:23:58: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:58: +------+-------------+-------+-------------+-------+
INFO - 16:23:58: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:58: +------+-------------+-------+-------------+-------+
INFO - 16:23:58: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:58: 2%|▏ | 1/50 [00:00<00:00, 109.00 it/sec, feas=True, obj=-2.25]
INFO - 16:23:58: Optimization result:
INFO - 16:23:58: Optimizer info:
INFO - 16:23:58: Status: 8
INFO - 16:23:58: Message: Positive directional derivative for linesearch
INFO - 16:23:58: Solution:
INFO - 16:23:58: The solution is feasible.
INFO - 16:23:58: Objective: -2.250821760291785
INFO - 16:23:58: Standardized constraints:
INFO - 16:23:58: g_2 = -0.00014442752851806517
INFO - 16:23:58: Design space:
INFO - 16:23:58: +------+-------------+-------+-------------+-------+
INFO - 16:23:58: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:58: +------+-------------+-------+-------------+-------+
INFO - 16:23:58: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:58: +------+-------------+-------+-------------+-------+
INFO - 16:23:58: *** End AerodynamicsScenario execution (time: 0:00:00.010779) ***
INFO - 16:23:58: *** Start StructureScenario execution ***
INFO - 16:23:58: StructureScenario
INFO - 16:23:58: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:58: MDO formulation: MDF
INFO - 16:23:58: Optimization problem:
INFO - 16:23:58: minimize 0.001*-y_4(x_1)
INFO - 16:23:58: with respect to x_1
INFO - 16:23:58: under the inequality constraints
INFO - 16:23:58: g_1(x_1) <= 0
INFO - 16:23:58: over the design space:
INFO - 16:23:58: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:58: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:58: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:58: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:58: | x_1[1] | 0.75 | 0.7806436836764827 | 1.25 | float |
INFO - 16:23:58: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:58: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:58: 2%|▏ | 1/50 [00:00<00:00, 102.07 it/sec, feas=True, obj=-2.25]
INFO - 16:23:58: Optimization result:
INFO - 16:23:58: Optimizer info:
INFO - 16:23:58: Status: 8
INFO - 16:23:58: Message: Positive directional derivative for linesearch
INFO - 16:23:58: Solution:
INFO - 16:23:58: The solution is feasible.
INFO - 16:23:58: Objective: -2.250821760291785
INFO - 16:23:58: Standardized constraints:
INFO - 16:23:58: g_1 = [-4.39127224e-04 -1.39421321e-03 -1.27087081e-02 -2.29652296e-02
INFO - 16:23:58: -3.12478375e-02 -2.40000000e-01 1.36557432e-14]
INFO - 16:23:58: Design space:
INFO - 16:23:58: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:58: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:58: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:58: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:58: | x_1[1] | 0.75 | 0.7806436836764827 | 1.25 | float |
INFO - 16:23:58: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:58: *** End StructureScenario execution (time: 0:00:00.011854) ***
INFO - 16:23:58: 83%|████████▎ | 83/100 [00:41<00:08, 2.00 it/sec, feas=True, obj=-2.25]
INFO - 16:23:58: *** Start PropulsionScenario execution ***
INFO - 16:23:58: PropulsionScenario
INFO - 16:23:58: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:58: MDO formulation: MDF
INFO - 16:23:58: Optimization problem:
INFO - 16:23:58: minimize 0.001*-y_4(x_3)
INFO - 16:23:58: with respect to x_3
INFO - 16:23:58: under the inequality constraints
INFO - 16:23:58: g_3(x_3) <= 0
INFO - 16:23:58: over the design space:
INFO - 16:23:58: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:58: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:58: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:58: | x_3 | 0.1 | 0.1581615810972491 | 1 | float |
INFO - 16:23:58: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:58: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:58: 2%|▏ | 1/50 [00:00<00:01, 38.64 it/sec, feas=True, obj=-2.25]
INFO - 16:23:58: 4%|▍ | 2/50 [00:00<00:01, 29.80 it/sec, feas=True, obj=-2.25]
INFO - 16:23:58: Optimization result:
INFO - 16:23:58: Optimizer info:
INFO - 16:23:58: Status: 8
INFO - 16:23:58: Message: Positive directional derivative for linesearch
INFO - 16:23:58: Solution:
INFO - 16:23:58: The solution is feasible.
INFO - 16:23:58: Objective: -2.248510058916256
INFO - 16:23:58: Standardized constraints:
INFO - 16:23:58: g_3 = [-8.36158308e-01 -1.63841692e-01 7.54951657e-15 -1.81375215e-01]
INFO - 16:23:58: Design space:
INFO - 16:23:58: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:58: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:58: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:58: | x_3 | 0.1 | 0.1582831160420126 | 1 | float |
INFO - 16:23:58: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:58: *** End PropulsionScenario execution (time: 0:00:00.069375) ***
INFO - 16:23:58: *** Start AerodynamicsScenario execution ***
INFO - 16:23:58: AerodynamicsScenario
INFO - 16:23:58: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:58: MDO formulation: MDF
INFO - 16:23:58: Optimization problem:
INFO - 16:23:58: minimize 0.001*-y_4(x_2)
INFO - 16:23:58: with respect to x_2
INFO - 16:23:58: under the inequality constraints
INFO - 16:23:58: g_2(x_2) <= 0
INFO - 16:23:58: over the design space:
INFO - 16:23:58: +------+-------------+-------+-------------+-------+
INFO - 16:23:58: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:58: +------+-------------+-------+-------------+-------+
INFO - 16:23:58: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:58: +------+-------------+-------+-------------+-------+
INFO - 16:23:58: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:58: 2%|▏ | 1/50 [00:00<00:00, 84.75 it/sec, feas=True, obj=-2.25]
INFO - 16:23:58: Optimization result:
INFO - 16:23:58: Optimizer info:
INFO - 16:23:58: Status: 8
INFO - 16:23:58: Message: Positive directional derivative for linesearch
INFO - 16:23:58: Solution:
INFO - 16:23:58: The solution is feasible.
INFO - 16:23:58: Objective: -2.248510058916256
INFO - 16:23:58: Standardized constraints:
INFO - 16:23:58: g_2 = 7.812911475069129e-05
INFO - 16:23:58: Design space:
INFO - 16:23:58: +------+-------------+-------+-------------+-------+
INFO - 16:23:58: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:58: +------+-------------+-------+-------------+-------+
INFO - 16:23:58: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:58: +------+-------------+-------+-------------+-------+
INFO - 16:23:58: *** End AerodynamicsScenario execution (time: 0:00:00.013593) ***
INFO - 16:23:58: *** Start StructureScenario execution ***
INFO - 16:23:58: StructureScenario
INFO - 16:23:58: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:58: MDO formulation: MDF
INFO - 16:23:58: Optimization problem:
INFO - 16:23:58: minimize 0.001*-y_4(x_1)
INFO - 16:23:58: with respect to x_1
INFO - 16:23:58: under the inequality constraints
INFO - 16:23:58: g_1(x_1) <= 0
INFO - 16:23:58: over the design space:
INFO - 16:23:58: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:58: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:58: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:58: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:58: | x_1[1] | 0.75 | 0.7806436836764827 | 1.25 | float |
INFO - 16:23:58: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:58: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:58: 2%|▏ | 1/50 [00:00<00:00, 94.70 it/sec, feas=True, obj=-2.25]
INFO - 16:23:58: Optimization result:
INFO - 16:23:58: Optimizer info:
INFO - 16:23:58: Status: 8
INFO - 16:23:58: Message: Positive directional derivative for linesearch
INFO - 16:23:58: Solution:
INFO - 16:23:58: The solution is feasible.
INFO - 16:23:58: Objective: -2.248510058916256
INFO - 16:23:58: Standardized constraints:
INFO - 16:23:58: g_1 = [-2.22220169e-03 -2.37215462e-03 -1.33631235e-02 -2.34508224e-02
INFO - 16:23:58: -3.16314207e-02 -2.40000000e-01 1.36557432e-14]
INFO - 16:23:58: Design space:
INFO - 16:23:58: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:58: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:58: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:58: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:58: | x_1[1] | 0.75 | 0.7806436836764827 | 1.25 | float |
INFO - 16:23:58: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:58: *** End StructureScenario execution (time: 0:00:00.012471) ***
INFO - 16:23:58: *** Start PropulsionScenario execution ***
INFO - 16:23:58: PropulsionScenario
INFO - 16:23:58: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:58: MDO formulation: MDF
INFO - 16:23:58: Optimization problem:
INFO - 16:23:58: minimize 0.001*-y_4(x_3)
INFO - 16:23:58: with respect to x_3
INFO - 16:23:58: under the inequality constraints
INFO - 16:23:58: g_3(x_3) <= 0
INFO - 16:23:58: over the design space:
INFO - 16:23:58: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:58: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:58: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:58: | x_3 | 0.1 | 0.1582831160420126 | 1 | float |
INFO - 16:23:58: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:58: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:58: 2%|▏ | 1/50 [00:00<00:00, 107.43 it/sec, feas=True, obj=-2.25]
INFO - 16:23:58: 4%|▍ | 2/50 [00:00<00:00, 67.17 it/sec, feas=True, obj=-2.25]
INFO - 16:23:58: 6%|▌ | 3/50 [00:00<00:00, 85.85 it/sec, feas=True, obj=-2.25]
INFO - 16:23:58: Optimization result:
INFO - 16:23:58: Optimizer info:
INFO - 16:23:58: Status: None
INFO - 16:23:58: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:58: Solution:
INFO - 16:23:58: The solution is feasible.
INFO - 16:23:58: Objective: -2.248510058916257
INFO - 16:23:58: Standardized constraints:
INFO - 16:23:58: g_3 = [-8.36158308e-01 -1.63841692e-01 1.13242749e-14 -1.81375215e-01]
INFO - 16:23:58: Design space:
INFO - 16:23:58: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:58: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:58: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:58: | x_3 | 0.1 | 0.1582831160420132 | 1 | float |
INFO - 16:23:58: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:58: *** End PropulsionScenario execution (time: 0:00:00.037236) ***
INFO - 16:23:58: *** Start AerodynamicsScenario execution ***
INFO - 16:23:58: AerodynamicsScenario
INFO - 16:23:58: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:58: MDO formulation: MDF
INFO - 16:23:58: Optimization problem:
INFO - 16:23:58: minimize 0.001*-y_4(x_2)
INFO - 16:23:58: with respect to x_2
INFO - 16:23:58: under the inequality constraints
INFO - 16:23:58: g_2(x_2) <= 0
INFO - 16:23:58: over the design space:
INFO - 16:23:58: +------+-------------+-------+-------------+-------+
INFO - 16:23:58: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:58: +------+-------------+-------+-------------+-------+
INFO - 16:23:58: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:58: +------+-------------+-------+-------------+-------+
INFO - 16:23:58: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:58: 2%|▏ | 1/50 [00:00<00:00, 69.57 it/sec, feas=True, obj=-2.25]
INFO - 16:23:58: Optimization result:
INFO - 16:23:58: Optimizer info:
INFO - 16:23:58: Status: 8
INFO - 16:23:58: Message: Positive directional derivative for linesearch
INFO - 16:23:58: Solution:
INFO - 16:23:58: The solution is feasible.
INFO - 16:23:58: Objective: -2.248510058916257
INFO - 16:23:58: Standardized constraints:
INFO - 16:23:58: g_2 = 7.812911475069129e-05
INFO - 16:23:58: Design space:
INFO - 16:23:58: +------+-------------+-------+-------------+-------+
INFO - 16:23:58: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:58: +------+-------------+-------+-------------+-------+
INFO - 16:23:58: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:58: +------+-------------+-------+-------------+-------+
INFO - 16:23:58: *** End AerodynamicsScenario execution (time: 0:00:00.015939) ***
INFO - 16:23:58: *** Start StructureScenario execution ***
INFO - 16:23:58: StructureScenario
INFO - 16:23:58: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:58: MDO formulation: MDF
INFO - 16:23:58: Optimization problem:
INFO - 16:23:58: minimize 0.001*-y_4(x_1)
INFO - 16:23:58: with respect to x_1
INFO - 16:23:58: under the inequality constraints
INFO - 16:23:58: g_1(x_1) <= 0
INFO - 16:23:58: over the design space:
INFO - 16:23:58: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:58: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:58: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:58: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:58: | x_1[1] | 0.75 | 0.7806436836764827 | 1.25 | float |
INFO - 16:23:58: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:58: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:58: 2%|▏ | 1/50 [00:00<00:00, 82.52 it/sec, feas=True, obj=-2.25]
INFO - 16:23:58: Optimization result:
INFO - 16:23:58: Optimizer info:
INFO - 16:23:58: Status: 8
INFO - 16:23:58: Message: Positive directional derivative for linesearch
INFO - 16:23:58: Solution:
INFO - 16:23:58: The solution is feasible.
INFO - 16:23:58: Objective: -2.248510058916257
INFO - 16:23:58: Standardized constraints:
INFO - 16:23:58: g_1 = [-2.22220169e-03 -2.37215462e-03 -1.33631235e-02 -2.34508224e-02
INFO - 16:23:58: -3.16314207e-02 -2.40000000e-01 1.36557432e-14]
INFO - 16:23:58: Design space:
INFO - 16:23:58: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:58: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:58: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:58: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:58: | x_1[1] | 0.75 | 0.7806436836764827 | 1.25 | float |
INFO - 16:23:58: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:58: *** End StructureScenario execution (time: 0:00:00.014143) ***
INFO - 16:23:58: 84%|████████▍ | 84/100 [00:41<00:07, 2.01 it/sec, feas=True, obj=-2.25]
INFO - 16:23:58: *** Start PropulsionScenario execution ***
INFO - 16:23:58: PropulsionScenario
INFO - 16:23:58: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:58: MDO formulation: MDF
INFO - 16:23:58: Optimization problem:
INFO - 16:23:58: minimize 0.001*-y_4(x_3)
INFO - 16:23:58: with respect to x_3
INFO - 16:23:58: under the inequality constraints
INFO - 16:23:58: g_3(x_3) <= 0
INFO - 16:23:58: over the design space:
INFO - 16:23:58: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:58: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:58: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:58: | x_3 | 0.1 | 0.1582831160420132 | 1 | float |
INFO - 16:23:58: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:58: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:58: 2%|▏ | 1/50 [00:00<00:01, 37.15 it/sec, feas=False, obj=-2.25]
INFO - 16:23:58: 4%|▍ | 2/50 [00:00<00:01, 38.98 it/sec, feas=True, obj=-2.25]
INFO - 16:23:58: 6%|▌ | 3/50 [00:00<00:01, 32.65 it/sec, feas=False, obj=-2.25]
INFO - 16:23:58: 8%|▊ | 4/50 [00:00<00:01, 30.20 it/sec, feas=True, obj=-2.25]
INFO - 16:23:58: 10%|█ | 5/50 [00:00<00:01, 31.86 it/sec, feas=True, obj=-2.25]
INFO - 16:23:58: 12%|█▏ | 6/50 [00:00<00:01, 32.42 it/sec, feas=True, obj=-2.25]
INFO - 16:23:58: Optimization result:
INFO - 16:23:58: Optimizer info:
INFO - 16:23:58: Status: None
INFO - 16:23:58: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:58: Solution:
INFO - 16:23:58: The solution is feasible.
INFO - 16:23:58: Objective: -2.251605086375443
INFO - 16:23:58: Standardized constraints:
INFO - 16:23:58: g_3 = [-8.36876438e-01 -1.63123562e-01 5.10702591e-15 -1.81447185e-01]
INFO - 16:23:58: Design space:
INFO - 16:23:58: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:58: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:58: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:58: | x_3 | 0.1 | 0.1581757953398483 | 1 | float |
INFO - 16:23:58: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:58: *** End PropulsionScenario execution (time: 0:00:00.187670) ***
INFO - 16:23:58: *** Start AerodynamicsScenario execution ***
INFO - 16:23:58: AerodynamicsScenario
INFO - 16:23:58: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:58: MDO formulation: MDF
INFO - 16:23:58: Optimization problem:
INFO - 16:23:58: minimize 0.001*-y_4(x_2)
INFO - 16:23:58: with respect to x_2
INFO - 16:23:58: under the inequality constraints
INFO - 16:23:58: g_2(x_2) <= 0
INFO - 16:23:58: over the design space:
INFO - 16:23:58: +------+-------------+-------+-------------+-------+
INFO - 16:23:58: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:58: +------+-------------+-------+-------------+-------+
INFO - 16:23:58: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:58: +------+-------------+-------+-------------+-------+
INFO - 16:23:58: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:58: 2%|▏ | 1/50 [00:00<00:00, 76.17 it/sec, feas=True, obj=-2.25]
INFO - 16:23:58: Optimization result:
INFO - 16:23:58: Optimizer info:
INFO - 16:23:58: Status: 8
INFO - 16:23:58: Message: Positive directional derivative for linesearch
INFO - 16:23:58: Solution:
INFO - 16:23:58: The solution is feasible.
INFO - 16:23:58: Objective: -2.251605086375443
INFO - 16:23:58: Standardized constraints:
INFO - 16:23:58: g_2 = -0.00010118145907189735
INFO - 16:23:58: Design space:
INFO - 16:23:58: +------+-------------+-------+-------------+-------+
INFO - 16:23:58: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:58: +------+-------------+-------+-------------+-------+
INFO - 16:23:58: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:58: +------+-------------+-------+-------------+-------+
INFO - 16:23:58: *** End AerodynamicsScenario execution (time: 0:00:00.014914) ***
INFO - 16:23:58: *** Start StructureScenario execution ***
INFO - 16:23:58: StructureScenario
INFO - 16:23:58: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:58: MDO formulation: MDF
INFO - 16:23:58: Optimization problem:
INFO - 16:23:58: minimize 0.001*-y_4(x_1)
INFO - 16:23:58: with respect to x_1
INFO - 16:23:58: under the inequality constraints
INFO - 16:23:58: g_1(x_1) <= 0
INFO - 16:23:58: over the design space:
INFO - 16:23:58: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:58: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:58: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:58: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:58: | x_1[1] | 0.75 | 0.7806436836764827 | 1.25 | float |
INFO - 16:23:58: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:58: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:58: 2%|▏ | 1/50 [00:00<00:00, 97.56 it/sec, feas=True, obj=-2.25]
INFO - 16:23:58: 4%|▍ | 2/50 [00:00<00:00, 116.87 it/sec, feas=True, obj=-2.25]
INFO - 16:23:58: 6%|▌ | 3/50 [00:00<00:00, 131.68 it/sec, feas=True, obj=-2.25]
INFO - 16:23:58: Optimization result:
INFO - 16:23:58: Optimizer info:
INFO - 16:23:58: Status: None
INFO - 16:23:58: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:58: Solution:
INFO - 16:23:58: The solution is feasible.
INFO - 16:23:58: Objective: -2.251605086375443
INFO - 16:23:58: Standardized constraints:
INFO - 16:23:58: g_1 = [-7.85362814e-04 -1.58413408e-03 -1.28358101e-02 -2.30595487e-02
INFO - 16:23:58: -3.13223465e-02 -2.40000000e-01 1.36557432e-14]
INFO - 16:23:58: Design space:
INFO - 16:23:58: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:58: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:58: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:58: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:58: | x_1[1] | 0.75 | 0.7806436836764827 | 1.25 | float |
INFO - 16:23:58: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:58: *** End StructureScenario execution (time: 0:00:00.025406) ***
INFO - 16:23:58: *** Start PropulsionScenario execution ***
INFO - 16:23:58: PropulsionScenario
INFO - 16:23:58: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:58: MDO formulation: MDF
INFO - 16:23:58: Optimization problem:
INFO - 16:23:58: minimize 0.001*-y_4(x_3)
INFO - 16:23:58: with respect to x_3
INFO - 16:23:58: under the inequality constraints
INFO - 16:23:58: g_3(x_3) <= 0
INFO - 16:23:58: over the design space:
INFO - 16:23:58: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:58: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:58: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:58: | x_3 | 0.1 | 0.1581757953398483 | 1 | float |
INFO - 16:23:58: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:58: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:58: 2%|▏ | 1/50 [00:00<00:00, 72.00 it/sec, feas=True, obj=-2.25]
INFO - 16:23:58: 4%|▍ | 2/50 [00:00<00:00, 105.79 it/sec, feas=True, obj=-2.25]
INFO - 16:23:58: 6%|▌ | 3/50 [00:00<00:00, 112.69 it/sec, feas=True, obj=-2.25]
INFO - 16:23:58: Optimization result:
INFO - 16:23:58: Optimizer info:
INFO - 16:23:58: Status: 8
INFO - 16:23:58: Message: Positive directional derivative for linesearch
INFO - 16:23:58: Solution:
INFO - 16:23:58: The solution is feasible.
INFO - 16:23:58: Objective: -2.251605086375443
INFO - 16:23:58: Standardized constraints:
INFO - 16:23:58: g_3 = [-8.36876438e-01 -1.63123562e-01 5.10702591e-15 -1.81447185e-01]
INFO - 16:23:58: Design space:
INFO - 16:23:58: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:58: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:58: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:58: | x_3 | 0.1 | 0.1581757953398483 | 1 | float |
INFO - 16:23:58: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:58: *** End PropulsionScenario execution (time: 0:00:00.028951) ***
INFO - 16:23:58: *** Start AerodynamicsScenario execution ***
INFO - 16:23:58: AerodynamicsScenario
INFO - 16:23:58: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:58: MDO formulation: MDF
INFO - 16:23:58: Optimization problem:
INFO - 16:23:58: minimize 0.001*-y_4(x_2)
INFO - 16:23:58: with respect to x_2
INFO - 16:23:58: under the inequality constraints
INFO - 16:23:58: g_2(x_2) <= 0
INFO - 16:23:58: over the design space:
INFO - 16:23:58: +------+-------------+-------+-------------+-------+
INFO - 16:23:58: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:58: +------+-------------+-------+-------------+-------+
INFO - 16:23:58: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:58: +------+-------------+-------+-------------+-------+
INFO - 16:23:58: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:58: 2%|▏ | 1/50 [00:00<00:00, 86.11 it/sec, feas=True, obj=-2.25]
INFO - 16:23:58: Optimization result:
INFO - 16:23:58: Optimizer info:
INFO - 16:23:58: Status: 8
INFO - 16:23:58: Message: Positive directional derivative for linesearch
INFO - 16:23:58: Solution:
INFO - 16:23:58: The solution is feasible.
INFO - 16:23:58: Objective: -2.251605086375443
INFO - 16:23:58: Standardized constraints:
INFO - 16:23:58: g_2 = -0.00010118145907189735
INFO - 16:23:58: Design space:
INFO - 16:23:58: +------+-------------+-------+-------------+-------+
INFO - 16:23:58: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:58: +------+-------------+-------+-------------+-------+
INFO - 16:23:58: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:58: +------+-------------+-------+-------------+-------+
INFO - 16:23:58: *** End AerodynamicsScenario execution (time: 0:00:00.013095) ***
INFO - 16:23:58: 85%|████████▌ | 85/100 [00:42<00:07, 2.02 it/sec, feas=True, obj=-2.25]
INFO - 16:23:58: *** Start PropulsionScenario execution ***
INFO - 16:23:58: PropulsionScenario
INFO - 16:23:58: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:58: MDO formulation: MDF
INFO - 16:23:58: Optimization problem:
INFO - 16:23:58: minimize 0.001*-y_4(x_3)
INFO - 16:23:58: with respect to x_3
INFO - 16:23:58: under the inequality constraints
INFO - 16:23:58: g_3(x_3) <= 0
INFO - 16:23:58: over the design space:
INFO - 16:23:58: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:58: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:58: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:58: | x_3 | 0.1 | 0.1581757953398483 | 1 | float |
INFO - 16:23:58: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:58: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:58: 2%|▏ | 1/50 [00:00<00:01, 39.46 it/sec, feas=True, obj=-2.25]
INFO - 16:23:58: 4%|▍ | 2/50 [00:00<00:01, 30.43 it/sec, feas=True, obj=-2.25]
INFO - 16:23:59: 6%|▌ | 3/50 [00:00<00:01, 33.21 it/sec, feas=True, obj=-2.25]
INFO - 16:23:59: 8%|▊ | 4/50 [00:00<00:01, 34.70 it/sec, feas=True, obj=-2.25]
INFO - 16:23:59: Optimization result:
INFO - 16:23:59: Optimizer info:
INFO - 16:23:59: Status: None
INFO - 16:23:59: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:59: Solution:
INFO - 16:23:59: The solution is feasible.
INFO - 16:23:59: Objective: -2.2487055907126647
INFO - 16:23:59: Standardized constraints:
INFO - 16:23:59: g_3 = [-0.8362102 -0.1637898 0. -0.18137326]
INFO - 16:23:59: Design space:
INFO - 16:23:59: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:59: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:59: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:59: | x_3 | 0.1 | 0.1582780483573711 | 1 | float |
INFO - 16:23:59: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:59: *** End PropulsionScenario execution (time: 0:00:00.118036) ***
INFO - 16:23:59: *** Start AerodynamicsScenario execution ***
INFO - 16:23:59: AerodynamicsScenario
INFO - 16:23:59: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:59: MDO formulation: MDF
INFO - 16:23:59: Optimization problem:
INFO - 16:23:59: minimize 0.001*-y_4(x_2)
INFO - 16:23:59: with respect to x_2
INFO - 16:23:59: under the inequality constraints
INFO - 16:23:59: g_2(x_2) <= 0
INFO - 16:23:59: over the design space:
INFO - 16:23:59: +------+-------------+-------+-------------+-------+
INFO - 16:23:59: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:59: +------+-------------+-------+-------------+-------+
INFO - 16:23:59: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:59: +------+-------------+-------+-------------+-------+
INFO - 16:23:59: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:59: 2%|▏ | 1/50 [00:00<00:00, 71.34 it/sec, feas=True, obj=-2.25]
INFO - 16:23:59: Optimization result:
INFO - 16:23:59: Optimizer info:
INFO - 16:23:59: Status: 8
INFO - 16:23:59: Message: Positive directional derivative for linesearch
INFO - 16:23:59: Solution:
INFO - 16:23:59: The solution is feasible.
INFO - 16:23:59: Objective: -2.2487055907126647
INFO - 16:23:59: Standardized constraints:
INFO - 16:23:59: g_2 = 7.917965009629491e-05
INFO - 16:23:59: Design space:
INFO - 16:23:59: +------+-------------+-------+-------------+-------+
INFO - 16:23:59: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:59: +------+-------------+-------+-------------+-------+
INFO - 16:23:59: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:59: +------+-------------+-------+-------------+-------+
INFO - 16:23:59: *** End AerodynamicsScenario execution (time: 0:00:00.015786) ***
INFO - 16:23:59: *** Start StructureScenario execution ***
INFO - 16:23:59: StructureScenario
INFO - 16:23:59: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:59: MDO formulation: MDF
INFO - 16:23:59: Optimization problem:
INFO - 16:23:59: minimize 0.001*-y_4(x_1)
INFO - 16:23:59: with respect to x_1
INFO - 16:23:59: under the inequality constraints
INFO - 16:23:59: g_1(x_1) <= 0
INFO - 16:23:59: over the design space:
INFO - 16:23:59: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:59: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:59: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:59: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:59: | x_1[1] | 0.75 | 0.7806436836764827 | 1.25 | float |
INFO - 16:23:59: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:59: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:59: 2%|▏ | 1/50 [00:00<00:00, 97.78 it/sec, feas=True, obj=-2.25]
INFO - 16:23:59: Optimization result:
INFO - 16:23:59: Optimizer info:
INFO - 16:23:59: Status: 8
INFO - 16:23:59: Message: Positive directional derivative for linesearch
INFO - 16:23:59: Solution:
INFO - 16:23:59: The solution is feasible.
INFO - 16:23:59: Objective: -2.2487055907126647
INFO - 16:23:59: Standardized constraints:
INFO - 16:23:59: g_1 = [-2.23062569e-03 -2.37677406e-03 -1.33662144e-02 -2.34531158e-02
INFO - 16:23:59: -3.16332322e-02 -2.40000000e-01 1.36557432e-14]
INFO - 16:23:59: Design space:
INFO - 16:23:59: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:59: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:59: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:59: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:59: | x_1[1] | 0.75 | 0.7806436836764827 | 1.25 | float |
INFO - 16:23:59: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:59: *** End StructureScenario execution (time: 0:00:00.012116) ***
INFO - 16:23:59: *** Start PropulsionScenario execution ***
INFO - 16:23:59: PropulsionScenario
INFO - 16:23:59: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:59: MDO formulation: MDF
INFO - 16:23:59: Optimization problem:
INFO - 16:23:59: minimize 0.001*-y_4(x_3)
INFO - 16:23:59: with respect to x_3
INFO - 16:23:59: under the inequality constraints
INFO - 16:23:59: g_3(x_3) <= 0
INFO - 16:23:59: over the design space:
INFO - 16:23:59: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:59: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:59: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:59: | x_3 | 0.1 | 0.1582780483573711 | 1 | float |
INFO - 16:23:59: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:59: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:59: 2%|▏ | 1/50 [00:00<00:00, 108.69 it/sec, feas=True, obj=-2.25]
INFO - 16:23:59: 4%|▍ | 2/50 [00:00<00:00, 143.59 it/sec, feas=True, obj=-2.25]
INFO - 16:23:59: 6%|▌ | 3/50 [00:00<00:00, 84.05 it/sec, feas=True, obj=-2.25]
INFO - 16:23:59: Optimization result:
INFO - 16:23:59: Optimizer info:
INFO - 16:23:59: Status: None
INFO - 16:23:59: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:59: Solution:
INFO - 16:23:59: The solution is feasible.
INFO - 16:23:59: Objective: -2.2487055907126683
INFO - 16:23:59: Standardized constraints:
INFO - 16:23:59: g_3 = [-8.36210199e-01 -1.63789801e-01 1.37667655e-14 -1.81373259e-01]
INFO - 16:23:59: Design space:
INFO - 16:23:59: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:59: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:59: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:59: | x_3 | 0.1 | 0.1582780483573733 | 1 | float |
INFO - 16:23:59: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:59: *** End PropulsionScenario execution (time: 0:00:00.037864) ***
INFO - 16:23:59: *** Start AerodynamicsScenario execution ***
INFO - 16:23:59: AerodynamicsScenario
INFO - 16:23:59: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:59: MDO formulation: MDF
INFO - 16:23:59: Optimization problem:
INFO - 16:23:59: minimize 0.001*-y_4(x_2)
INFO - 16:23:59: with respect to x_2
INFO - 16:23:59: under the inequality constraints
INFO - 16:23:59: g_2(x_2) <= 0
INFO - 16:23:59: over the design space:
INFO - 16:23:59: +------+-------------+-------+-------------+-------+
INFO - 16:23:59: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:59: +------+-------------+-------+-------------+-------+
INFO - 16:23:59: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:59: +------+-------------+-------+-------------+-------+
INFO - 16:23:59: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:59: 2%|▏ | 1/50 [00:00<00:00, 68.73 it/sec, feas=True, obj=-2.25]
INFO - 16:23:59: Optimization result:
INFO - 16:23:59: Optimizer info:
INFO - 16:23:59: Status: 8
INFO - 16:23:59: Message: Positive directional derivative for linesearch
INFO - 16:23:59: Solution:
INFO - 16:23:59: The solution is feasible.
INFO - 16:23:59: Objective: -2.248705590712669
INFO - 16:23:59: Standardized constraints:
INFO - 16:23:59: g_2 = 7.917965009629491e-05
INFO - 16:23:59: Design space:
INFO - 16:23:59: +------+-------------+-------+-------------+-------+
INFO - 16:23:59: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:59: +------+-------------+-------+-------------+-------+
INFO - 16:23:59: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:59: +------+-------------+-------+-------------+-------+
INFO - 16:23:59: *** End AerodynamicsScenario execution (time: 0:00:00.016292) ***
INFO - 16:23:59: *** Start StructureScenario execution ***
INFO - 16:23:59: StructureScenario
INFO - 16:23:59: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:59: MDO formulation: MDF
INFO - 16:23:59: Optimization problem:
INFO - 16:23:59: minimize 0.001*-y_4(x_1)
INFO - 16:23:59: with respect to x_1
INFO - 16:23:59: under the inequality constraints
INFO - 16:23:59: g_1(x_1) <= 0
INFO - 16:23:59: over the design space:
INFO - 16:23:59: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:59: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:59: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:59: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:59: | x_1[1] | 0.75 | 0.7806436836764827 | 1.25 | float |
INFO - 16:23:59: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:59: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:59: 2%|▏ | 1/50 [00:00<00:00, 82.26 it/sec, feas=True, obj=-2.25]
INFO - 16:23:59: Optimization result:
INFO - 16:23:59: Optimizer info:
INFO - 16:23:59: Status: 8
INFO - 16:23:59: Message: Positive directional derivative for linesearch
INFO - 16:23:59: Solution:
INFO - 16:23:59: The solution is feasible.
INFO - 16:23:59: Objective: -2.2487055907126683
INFO - 16:23:59: Standardized constraints:
INFO - 16:23:59: g_1 = [-2.23062569e-03 -2.37677406e-03 -1.33662144e-02 -2.34531158e-02
INFO - 16:23:59: -3.16332322e-02 -2.40000000e-01 1.36557432e-14]
INFO - 16:23:59: Design space:
INFO - 16:23:59: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:59: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:59: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:59: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:59: | x_1[1] | 0.75 | 0.7806436836764827 | 1.25 | float |
INFO - 16:23:59: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:59: *** End StructureScenario execution (time: 0:00:00.014394) ***
INFO - 16:23:59: 86%|████████▌ | 86/100 [00:42<00:06, 2.03 it/sec, feas=True, obj=-2.25]
INFO - 16:23:59: *** Start PropulsionScenario execution ***
INFO - 16:23:59: PropulsionScenario
INFO - 16:23:59: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:59: MDO formulation: MDF
INFO - 16:23:59: Optimization problem:
INFO - 16:23:59: minimize 0.001*-y_4(x_3)
INFO - 16:23:59: with respect to x_3
INFO - 16:23:59: under the inequality constraints
INFO - 16:23:59: g_3(x_3) <= 0
INFO - 16:23:59: over the design space:
INFO - 16:23:59: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:59: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:59: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:59: | x_3 | 0.1 | 0.1582780483573733 | 1 | float |
INFO - 16:23:59: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:59: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:59: 2%|▏ | 1/50 [00:00<00:01, 39.53 it/sec, feas=False, obj=-2.25]
INFO - 16:23:59: 4%|▍ | 2/50 [00:00<00:01, 39.25 it/sec, feas=True, obj=-2.25]
INFO - 16:23:59: 6%|▌ | 3/50 [00:00<00:01, 32.92 it/sec, feas=False, obj=-2.25]
INFO - 16:23:59: 8%|▊ | 4/50 [00:00<00:01, 30.16 it/sec, feas=True, obj=-2.25]
INFO - 16:23:59: 10%|█ | 5/50 [00:00<00:01, 31.59 it/sec, feas=True, obj=-2.25]
INFO - 16:23:59: 12%|█▏ | 6/50 [00:00<00:01, 32.82 it/sec, feas=True, obj=-2.25]
INFO - 16:23:59: Optimization result:
INFO - 16:23:59: Optimizer info:
INFO - 16:23:59: Status: None
INFO - 16:23:59: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:59: Solution:
INFO - 16:23:59: The solution is feasible.
INFO - 16:23:59: Objective: -2.251047336334193
INFO - 16:23:59: Standardized constraints:
INFO - 16:23:59: g_3 = [-8.37072340e-01 -1.62927660e-01 7.54951657e-15 -1.81448581e-01]
INFO - 16:23:59: Design space:
INFO - 16:23:59: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:59: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:59: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:59: | x_3 | 0.1 | 0.1581742871032511 | 1 | float |
INFO - 16:23:59: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:59: *** End PropulsionScenario execution (time: 0:00:00.185495) ***
INFO - 16:23:59: *** Start AerodynamicsScenario execution ***
INFO - 16:23:59: AerodynamicsScenario
INFO - 16:23:59: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:59: MDO formulation: MDF
INFO - 16:23:59: Optimization problem:
INFO - 16:23:59: minimize 0.001*-y_4(x_2)
INFO - 16:23:59: with respect to x_2
INFO - 16:23:59: under the inequality constraints
INFO - 16:23:59: g_2(x_2) <= 0
INFO - 16:23:59: over the design space:
INFO - 16:23:59: +------+-------------+-------+-------------+-------+
INFO - 16:23:59: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:59: +------+-------------+-------+-------------+-------+
INFO - 16:23:59: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:59: +------+-------------+-------+-------------+-------+
INFO - 16:23:59: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:59: 2%|▏ | 1/50 [00:00<00:00, 77.34 it/sec, feas=True, obj=-2.25]
INFO - 16:23:59: Optimization result:
INFO - 16:23:59: Optimizer info:
INFO - 16:23:59: Status: 8
INFO - 16:23:59: Message: Positive directional derivative for linesearch
INFO - 16:23:59: Solution:
INFO - 16:23:59: The solution is feasible.
INFO - 16:23:59: Objective: -2.251047336334193
INFO - 16:23:59: Standardized constraints:
INFO - 16:23:59: g_2 = -0.00019915556846927807
INFO - 16:23:59: Design space:
INFO - 16:23:59: +------+-------------+-------+-------------+-------+
INFO - 16:23:59: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:59: +------+-------------+-------+-------------+-------+
INFO - 16:23:59: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:59: +------+-------------+-------+-------------+-------+
INFO - 16:23:59: *** End AerodynamicsScenario execution (time: 0:00:00.014596) ***
INFO - 16:23:59: *** Start StructureScenario execution ***
INFO - 16:23:59: StructureScenario
INFO - 16:23:59: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:59: MDO formulation: MDF
INFO - 16:23:59: Optimization problem:
INFO - 16:23:59: minimize 0.001*-y_4(x_1)
INFO - 16:23:59: with respect to x_1
INFO - 16:23:59: under the inequality constraints
INFO - 16:23:59: g_1(x_1) <= 0
INFO - 16:23:59: over the design space:
INFO - 16:23:59: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:59: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:59: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:59: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:59: | x_1[1] | 0.75 | 0.7806436836764827 | 1.25 | float |
INFO - 16:23:59: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:59: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:59: 2%|▏ | 1/50 [00:00<00:00, 98.48 it/sec, feas=True, obj=-2.25]
INFO - 16:23:59: Optimization result:
INFO - 16:23:59: Optimizer info:
INFO - 16:23:59: Status: 8
INFO - 16:23:59: Message: Positive directional derivative for linesearch
INFO - 16:23:59: Solution:
INFO - 16:23:59: The solution is feasible.
INFO - 16:23:59: Objective: -2.251047336334193
INFO - 16:23:59: Standardized constraints:
INFO - 16:23:59: g_1 = [-1.13253225e-06 -1.15394220e-03 -1.25479018e-02 -2.28458952e-02
INFO - 16:23:59: -3.11535647e-02 -2.40000000e-01 1.36557432e-14]
INFO - 16:23:59: Design space:
INFO - 16:23:59: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:59: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:59: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:59: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:59: | x_1[1] | 0.75 | 0.7806436836764827 | 1.25 | float |
INFO - 16:23:59: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:59: *** End StructureScenario execution (time: 0:00:00.012120) ***
INFO - 16:23:59: *** Start PropulsionScenario execution ***
INFO - 16:23:59: PropulsionScenario
INFO - 16:23:59: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:59: MDO formulation: MDF
INFO - 16:23:59: Optimization problem:
INFO - 16:23:59: minimize 0.001*-y_4(x_3)
INFO - 16:23:59: with respect to x_3
INFO - 16:23:59: under the inequality constraints
INFO - 16:23:59: g_3(x_3) <= 0
INFO - 16:23:59: over the design space:
INFO - 16:23:59: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:59: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:59: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:59: | x_3 | 0.1 | 0.1581742871032511 | 1 | float |
INFO - 16:23:59: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:59: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:59: 2%|▏ | 1/50 [00:00<00:00, 109.99 it/sec, feas=True, obj=-2.25]
INFO - 16:23:59: Optimization result:
INFO - 16:23:59: Optimizer info:
INFO - 16:23:59: Status: 8
INFO - 16:23:59: Message: Positive directional derivative for linesearch
INFO - 16:23:59: Solution:
INFO - 16:23:59: The solution is feasible.
INFO - 16:23:59: Objective: -2.251047336334193
INFO - 16:23:59: Standardized constraints:
INFO - 16:23:59: g_3 = [-8.37072340e-01 -1.62927660e-01 7.54951657e-15 -1.81448581e-01]
INFO - 16:23:59: Design space:
INFO - 16:23:59: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:59: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:59: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:59: | x_3 | 0.1 | 0.1581742871032511 | 1 | float |
INFO - 16:23:59: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:59: *** End PropulsionScenario execution (time: 0:00:00.010858) ***
INFO - 16:23:59: *** Start AerodynamicsScenario execution ***
INFO - 16:23:59: AerodynamicsScenario
INFO - 16:23:59: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:59: MDO formulation: MDF
INFO - 16:23:59: Optimization problem:
INFO - 16:23:59: minimize 0.001*-y_4(x_2)
INFO - 16:23:59: with respect to x_2
INFO - 16:23:59: under the inequality constraints
INFO - 16:23:59: g_2(x_2) <= 0
INFO - 16:23:59: over the design space:
INFO - 16:23:59: +------+-------------+-------+-------------+-------+
INFO - 16:23:59: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:59: +------+-------------+-------+-------------+-------+
INFO - 16:23:59: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:59: +------+-------------+-------+-------------+-------+
INFO - 16:23:59: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:59: 2%|▏ | 1/50 [00:00<00:00, 108.71 it/sec, feas=True, obj=-2.25]
INFO - 16:23:59: Optimization result:
INFO - 16:23:59: Optimizer info:
INFO - 16:23:59: Status: 8
INFO - 16:23:59: Message: Positive directional derivative for linesearch
INFO - 16:23:59: Solution:
INFO - 16:23:59: The solution is feasible.
INFO - 16:23:59: Objective: -2.251047336334193
INFO - 16:23:59: Standardized constraints:
INFO - 16:23:59: g_2 = -0.00019915556846927807
INFO - 16:23:59: Design space:
INFO - 16:23:59: +------+-------------+-------+-------------+-------+
INFO - 16:23:59: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:59: +------+-------------+-------+-------------+-------+
INFO - 16:23:59: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:59: +------+-------------+-------+-------------+-------+
INFO - 16:23:59: *** End AerodynamicsScenario execution (time: 0:00:00.010687) ***
INFO - 16:23:59: 87%|████████▋ | 87/100 [00:42<00:06, 2.05 it/sec, feas=True, obj=-2.25]
INFO - 16:23:59: *** Start PropulsionScenario execution ***
INFO - 16:23:59: PropulsionScenario
INFO - 16:23:59: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:59: MDO formulation: MDF
INFO - 16:23:59: Optimization problem:
INFO - 16:23:59: minimize 0.001*-y_4(x_3)
INFO - 16:23:59: with respect to x_3
INFO - 16:23:59: under the inequality constraints
INFO - 16:23:59: g_3(x_3) <= 0
INFO - 16:23:59: over the design space:
INFO - 16:23:59: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:59: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:59: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:59: | x_3 | 0.1 | 0.1581742871032511 | 1 | float |
INFO - 16:23:59: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:59: Solving optimization problem with algorithm SLSQP:
WARNING - 16:23:59: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 6.724932466608626e-05 is still above the tolerance 1e-06.
INFO - 16:23:59: 2%|▏ | 1/50 [00:00<00:01, 33.93 it/sec, feas=True, obj=-2.25]
INFO - 16:23:59: 4%|▍ | 2/50 [00:00<00:01, 28.12 it/sec, feas=True, obj=-2.25]
WARNING - 16:23:59: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 6.724932466608626e-05 is still above the tolerance 1e-06.
INFO - 16:23:59: 6%|▌ | 3/50 [00:00<00:01, 25.53 it/sec, feas=True, obj=-2.25]
INFO - 16:23:59: Optimization result:
INFO - 16:23:59: Optimizer info:
INFO - 16:23:59: Status: 8
INFO - 16:23:59: Message: Positive directional derivative for linesearch
INFO - 16:23:59: Solution:
INFO - 16:23:59: The solution is feasible.
INFO - 16:23:59: Objective: -2.24988669073317
INFO - 16:23:59: Standardized constraints:
INFO - 16:23:59: g_3 = [-0.83598111 -0.16401889 0. -0.18137361]
INFO - 16:23:59: Design space:
INFO - 16:23:59: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:59: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:59: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:59: | x_3 | 0.1 | 0.1582606665836423 | 1 | float |
INFO - 16:23:59: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:59: *** End PropulsionScenario execution (time: 0:00:00.119778) ***
INFO - 16:23:59: *** Start AerodynamicsScenario execution ***
INFO - 16:23:59: AerodynamicsScenario
INFO - 16:23:59: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:59: MDO formulation: MDF
INFO - 16:23:59: Optimization problem:
INFO - 16:23:59: minimize 0.001*-y_4(x_2)
INFO - 16:23:59: with respect to x_2
INFO - 16:23:59: under the inequality constraints
INFO - 16:23:59: g_2(x_2) <= 0
INFO - 16:23:59: over the design space:
INFO - 16:23:59: +------+-------------+-------+-------------+-------+
INFO - 16:23:59: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:59: +------+-------------+-------+-------------+-------+
INFO - 16:23:59: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:59: +------+-------------+-------+-------------+-------+
INFO - 16:23:59: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:59: 2%|▏ | 1/50 [00:00<00:00, 79.09 it/sec, feas=False, obj=-2.25]
INFO - 16:23:59: 4%|▍ | 2/50 [00:00<00:00, 127.35 it/sec, feas=False, obj=-2.25]
INFO - 16:23:59: 6%|▌ | 3/50 [00:00<00:00, 156.61 it/sec, feas=False, obj=-2.25]
INFO - 16:23:59: 8%|▊ | 4/50 [00:00<00:00, 176.04 it/sec, feas=False, obj=-2.25]
INFO - 16:23:59: 10%|█ | 5/50 [00:00<00:00, 191.00 it/sec, feas=False, obj=-2.25]
INFO - 16:23:59: 12%|█▏ | 6/50 [00:00<00:00, 201.51 it/sec, feas=False, obj=-2.25]
INFO - 16:23:59: 14%|█▍ | 7/50 [00:00<00:00, 209.88 it/sec, feas=False, obj=-2.25]
INFO - 16:23:59: 16%|█▌ | 8/50 [00:00<00:00, 217.55 it/sec, feas=False, obj=-2.25]
INFO - 16:23:59: 18%|█▊ | 9/50 [00:00<00:00, 211.28 it/sec, feas=False, obj=-2.25]
INFO - 16:23:59: 20%|██ | 10/50 [00:00<00:00, 215.54 it/sec, feas=False, obj=-2.25]
INFO - 16:23:59: 22%|██▏ | 11/50 [00:00<00:00, 220.48 it/sec, feas=False, obj=-2.25]
INFO - 16:23:59: 24%|██▍ | 12/50 [00:00<00:00, 224.89 it/sec, feas=False, obj=-2.25]
INFO - 16:23:59: 26%|██▌ | 13/50 [00:00<00:00, 220.71 it/sec, feas=False, obj=-2.25]
INFO - 16:23:59: 28%|██▊ | 14/50 [00:00<00:00, 224.18 it/sec, feas=False, obj=-2.25]
INFO - 16:23:59: 30%|███ | 15/50 [00:00<00:00, 227.65 it/sec, feas=False, obj=-2.25]
INFO - 16:23:59: 32%|███▏ | 16/50 [00:00<00:00, 230.73 it/sec, feas=False, obj=-2.25]
INFO - 16:23:59: 34%|███▍ | 17/50 [00:00<00:00, 233.08 it/sec, feas=False, obj=-2.25]
INFO - 16:23:59: 36%|███▌ | 18/50 [00:00<00:00, 235.10 it/sec, feas=False, obj=-2.25]
INFO - 16:23:59: 38%|███▊ | 19/50 [00:00<00:00, 237.57 it/sec, feas=False, obj=-2.25]
INFO - 16:23:59: 40%|████ | 20/50 [00:00<00:00, 239.68 it/sec, feas=False, obj=-2.25]
INFO - 16:23:59: 42%|████▏ | 21/50 [00:00<00:00, 203.12 it/sec, feas=False, obj=-2.25]
INFO - 16:23:59: 44%|████▍ | 22/50 [00:00<00:00, 205.50 it/sec, feas=False, obj=-2.25]
INFO - 16:23:59: 46%|████▌ | 23/50 [00:00<00:00, 207.93 it/sec, feas=False, obj=-2.25]
INFO - 16:23:59: 48%|████▊ | 24/50 [00:00<00:00, 210.27 it/sec, feas=False, obj=-2.25]
INFO - 16:23:59: 50%|█████ | 25/50 [00:00<00:00, 212.29 it/sec, feas=False, obj=-2.25]
INFO - 16:23:59: 52%|█████▏ | 26/50 [00:00<00:00, 214.44 it/sec, feas=False, obj=-2.25]
INFO - 16:23:59: 54%|█████▍ | 27/50 [00:00<00:00, 216.33 it/sec, feas=False, obj=-2.25]
INFO - 16:23:59: 56%|█████▌ | 28/50 [00:00<00:00, 218.23 it/sec, feas=False, obj=-2.25]
INFO - 16:23:59: 58%|█████▊ | 29/50 [00:00<00:00, 219.92 it/sec, feas=False, obj=-2.25]
INFO - 16:23:59: 60%|██████ | 30/50 [00:00<00:00, 197.82 it/sec, feas=False, obj=-2.25]
INFO - 16:23:59: 62%|██████▏ | 31/50 [00:00<00:00, 199.64 it/sec, feas=False, obj=-2.25]
INFO - 16:23:59: 64%|██████▍ | 32/50 [00:00<00:00, 201.40 it/sec, feas=False, obj=-2.25]
INFO - 16:23:59: 66%|██████▌ | 33/50 [00:00<00:00, 203.36 it/sec, feas=False, obj=-2.25]
INFO - 16:23:59: 68%|██████▊ | 34/50 [00:00<00:00, 205.10 it/sec, feas=False, obj=-2.25]
INFO - 16:23:59: 70%|███████ | 35/50 [00:00<00:00, 206.78 it/sec, feas=False, obj=-2.25]
INFO - 16:23:59: 72%|███████▏ | 36/50 [00:00<00:00, 208.43 it/sec, feas=False, obj=-2.25]
INFO - 16:23:59: 74%|███████▍ | 37/50 [00:00<00:00, 209.99 it/sec, feas=False, obj=-2.25]
INFO - 16:23:59: 76%|███████▌ | 38/50 [00:00<00:00, 190.26 it/sec, feas=False, obj=-2.25]
INFO - 16:23:59: 78%|███████▊ | 39/50 [00:00<00:00, 191.73 it/sec, feas=False, obj=-2.25]
INFO - 16:23:59: 80%|████████ | 40/50 [00:00<00:00, 193.35 it/sec, feas=False, obj=-2.25]
INFO - 16:23:59: 82%|████████▏ | 41/50 [00:00<00:00, 194.93 it/sec, feas=False, obj=-2.25]
INFO - 16:23:59: 84%|████████▍ | 42/50 [00:00<00:00, 196.41 it/sec, feas=False, obj=-2.25]
INFO - 16:23:59: 86%|████████▌ | 43/50 [00:00<00:00, 197.87 it/sec, feas=False, obj=-2.25]
INFO - 16:23:59: 88%|████████▊ | 44/50 [00:00<00:00, 199.24 it/sec, feas=False, obj=-2.25]
INFO - 16:23:59: 90%|█████████ | 45/50 [00:00<00:00, 200.61 it/sec, feas=False, obj=-2.25]
INFO - 16:23:59: 92%|█████████▏| 46/50 [00:00<00:00, 200.30 it/sec, feas=False, obj=-2.25]
INFO - 16:23:59: 94%|█████████▍| 47/50 [00:00<00:00, 201.60 it/sec, feas=False, obj=-2.25]
INFO - 16:23:59: 96%|█████████▌| 48/50 [00:00<00:00, 187.67 it/sec, feas=False, obj=-2.25]
INFO - 16:23:59: 98%|█████████▊| 49/50 [00:00<00:00, 188.86 it/sec, feas=False, obj=-2.25]
INFO - 16:23:59: 100%|██████████| 50/50 [00:00<00:00, 190.15 it/sec, feas=False, obj=-2.25]
WARNING - 16:23:59: Optimization found no feasible point; the least infeasible point is selected.
INFO - 16:23:59: Optimization result:
INFO - 16:23:59: Optimizer info:
INFO - 16:23:59: Status: None
INFO - 16:23:59: Message: Maximum number of iterations reached. GEMSEO stopped the driver.
INFO - 16:23:59: Solution:
WARNING - 16:23:59: The solution is not feasible.
INFO - 16:23:59: Objective: -2.24988669073317
INFO - 16:23:59: Standardized constraints:
INFO - 16:23:59: g_2 = 0.0002712892361895758
INFO - 16:23:59: Design space:
INFO - 16:23:59: +------+-------------+-------+-------------+-------+
INFO - 16:23:59: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:59: +------+-------------+-------+-------------+-------+
INFO - 16:23:59: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:59: +------+-------------+-------+-------------+-------+
INFO - 16:23:59: *** End AerodynamicsScenario execution (time: 0:00:00.265742) ***
INFO - 16:23:59: *** Start StructureScenario execution ***
INFO - 16:23:59: StructureScenario
INFO - 16:23:59: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:59: MDO formulation: MDF
INFO - 16:23:59: Optimization problem:
INFO - 16:23:59: minimize 0.001*-y_4(x_1)
INFO - 16:23:59: with respect to x_1
INFO - 16:23:59: under the inequality constraints
INFO - 16:23:59: g_1(x_1) <= 0
INFO - 16:23:59: over the design space:
INFO - 16:23:59: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:59: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:59: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:59: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:59: | x_1[1] | 0.75 | 0.7806436836764827 | 1.25 | float |
INFO - 16:23:59: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:59: Solving optimization problem with algorithm SLSQP:
WARNING - 16:23:59: MDAGaussSeidel has reached its maximum number of unsuccessful iterations, but the normalized residual norm 0.0009157477359807847 is still above the tolerance 1e-06.
INFO - 16:23:59: 2%|▏ | 1/50 [00:00<00:01, 46.22 it/sec, feas=True, obj=-2.25]
INFO - 16:23:59: Optimization result:
INFO - 16:23:59: Optimizer info:
INFO - 16:23:59: Status: 8
INFO - 16:23:59: Message: Positive directional derivative for linesearch
INFO - 16:23:59: Solution:
INFO - 16:23:59: The solution is feasible.
INFO - 16:23:59: Objective: -2.24988669073317
INFO - 16:23:59: Standardized constraints:
INFO - 16:23:59: g_1 = [-3.77226712e-03 -3.22203935e-03 -1.39317275e-02 -2.38726770e-02
INFO - 16:23:59: -3.19646170e-02 -2.40000000e-01 1.36557432e-14]
INFO - 16:23:59: Design space:
INFO - 16:23:59: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:59: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:59: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:59: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:23:59: | x_1[1] | 0.75 | 0.7806436836764827 | 1.25 | float |
INFO - 16:23:59: +--------+-------------+--------------------+-------------+-------+
INFO - 16:23:59: *** End StructureScenario execution (time: 0:00:00.023708) ***
INFO - 16:23:59: *** Start PropulsionScenario execution ***
INFO - 16:23:59: PropulsionScenario
INFO - 16:23:59: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:59: MDO formulation: MDF
INFO - 16:23:59: Optimization problem:
INFO - 16:23:59: minimize 0.001*-y_4(x_3)
INFO - 16:23:59: with respect to x_3
INFO - 16:23:59: under the inequality constraints
INFO - 16:23:59: g_3(x_3) <= 0
INFO - 16:23:59: over the design space:
INFO - 16:23:59: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:59: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:59: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:59: | x_3 | 0.1 | 0.1582606665836423 | 1 | float |
INFO - 16:23:59: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:59: Solving optimization problem with algorithm SLSQP:
WARNING - 16:23:59: MDAGaussSeidel has reached its maximum number of unsuccessful iterations, but the normalized residual norm 6.724932466608626e-05 is still above the tolerance 1e-06.
INFO - 16:23:59: 2%|▏ | 1/50 [00:00<00:00, 53.71 it/sec, feas=True, obj=-2.25]
INFO - 16:23:59: 4%|▍ | 2/50 [00:00<00:00, 88.28 it/sec, feas=True, obj=-2.25]
INFO - 16:23:59: 6%|▌ | 3/50 [00:00<00:00, 67.94 it/sec, feas=True, obj=-2.25]
INFO - 16:23:59: Optimization result:
INFO - 16:23:59: Optimizer info:
INFO - 16:23:59: Status: None
INFO - 16:23:59: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:23:59: Solution:
INFO - 16:23:59: The solution is feasible.
INFO - 16:23:59: Objective: -2.249886690733171
INFO - 16:23:59: Standardized constraints:
INFO - 16:23:59: g_3 = [-8.35981106e-01 -1.64018894e-01 5.10702591e-15 -1.81373615e-01]
INFO - 16:23:59: Design space:
INFO - 16:23:59: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:59: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:59: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:59: | x_3 | 0.1 | 0.1582606665836431 | 1 | float |
INFO - 16:23:59: +------+-------------+--------------------+-------------+-------+
INFO - 16:23:59: *** End PropulsionScenario execution (time: 0:00:00.046448) ***
INFO - 16:23:59: *** Start AerodynamicsScenario execution ***
INFO - 16:23:59: AerodynamicsScenario
INFO - 16:23:59: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:23:59: MDO formulation: MDF
INFO - 16:23:59: Optimization problem:
INFO - 16:23:59: minimize 0.001*-y_4(x_2)
INFO - 16:23:59: with respect to x_2
INFO - 16:23:59: under the inequality constraints
INFO - 16:23:59: g_2(x_2) <= 0
INFO - 16:23:59: over the design space:
INFO - 16:23:59: +------+-------------+-------+-------------+-------+
INFO - 16:23:59: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:23:59: +------+-------------+-------+-------------+-------+
INFO - 16:23:59: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:23:59: +------+-------------+-------+-------------+-------+
INFO - 16:23:59: Solving optimization problem with algorithm SLSQP:
INFO - 16:23:59: 2%|▏ | 1/50 [00:00<00:00, 80.76 it/sec, feas=False, obj=-2.25]
INFO - 16:23:59: 4%|▍ | 2/50 [00:00<00:00, 130.13 it/sec, feas=False, obj=-2.25]
INFO - 16:23:59: 6%|▌ | 3/50 [00:00<00:00, 161.62 it/sec, feas=False, obj=-2.25]
INFO - 16:23:59: 8%|▊ | 4/50 [00:00<00:00, 184.30 it/sec, feas=False, obj=-2.25]
INFO - 16:23:59: 10%|█ | 5/50 [00:00<00:00, 200.81 it/sec, feas=False, obj=-2.25]
INFO - 16:23:59: 12%|█▏ | 6/50 [00:00<00:00, 212.49 it/sec, feas=False, obj=-2.25]
INFO - 16:23:59: 14%|█▍ | 7/50 [00:00<00:00, 222.61 it/sec, feas=False, obj=-2.25]
INFO - 16:23:59: 16%|█▌ | 8/50 [00:00<00:00, 231.41 it/sec, feas=False, obj=-2.25]
INFO - 16:23:59: 18%|█▊ | 9/50 [00:00<00:00, 232.22 it/sec, feas=False, obj=-2.25]
INFO - 16:23:59: 20%|██ | 10/50 [00:00<00:00, 236.51 it/sec, feas=False, obj=-2.25]
INFO - 16:23:59: 22%|██▏ | 11/50 [00:00<00:00, 241.95 it/sec, feas=False, obj=-2.25]
INFO - 16:23:59: 24%|██▍ | 12/50 [00:00<00:00, 246.76 it/sec, feas=False, obj=-2.25]
INFO - 16:23:59: 26%|██▌ | 13/50 [00:00<00:00, 250.52 it/sec, feas=False, obj=-2.25]
INFO - 16:23:59: 28%|██▊ | 14/50 [00:00<00:00, 254.13 it/sec, feas=False, obj=-2.25]
INFO - 16:23:59: 30%|███ | 15/50 [00:00<00:00, 257.23 it/sec, feas=False, obj=-2.25]
INFO - 16:23:59: 32%|███▏ | 16/50 [00:00<00:00, 259.85 it/sec, feas=False, obj=-2.25]
INFO - 16:23:59: 34%|███▍ | 17/50 [00:00<00:00, 262.55 it/sec, feas=False, obj=-2.25]
INFO - 16:23:59: 36%|███▌ | 18/50 [00:00<00:00, 264.76 it/sec, feas=False, obj=-2.25]
INFO - 16:23:59: 38%|███▊ | 19/50 [00:00<00:00, 266.94 it/sec, feas=False, obj=-2.25]
INFO - 16:23:59: 40%|████ | 20/50 [00:00<00:00, 268.71 it/sec, feas=False, obj=-2.25]
INFO - 16:24:00: 42%|████▏ | 21/50 [00:00<00:00, 220.78 it/sec, feas=False, obj=-2.25]
INFO - 16:24:00: 44%|████▍ | 22/50 [00:00<00:00, 223.17 it/sec, feas=False, obj=-2.25]
INFO - 16:24:00: 46%|████▌ | 23/50 [00:00<00:00, 224.73 it/sec, feas=False, obj=-2.25]
INFO - 16:24:00: 48%|████▊ | 24/50 [00:00<00:00, 227.38 it/sec, feas=False, obj=-2.25]
INFO - 16:24:00: 50%|█████ | 25/50 [00:00<00:00, 229.85 it/sec, feas=False, obj=-2.25]
INFO - 16:24:00: 52%|█████▏ | 26/50 [00:00<00:00, 232.20 it/sec, feas=False, obj=-2.25]
INFO - 16:24:00: 54%|█████▍ | 27/50 [00:00<00:00, 234.41 it/sec, feas=False, obj=-2.25]
INFO - 16:24:00: 56%|█████▌ | 28/50 [00:00<00:00, 236.47 it/sec, feas=False, obj=-2.25]
INFO - 16:24:00: 58%|█████▊ | 29/50 [00:00<00:00, 238.54 it/sec, feas=False, obj=-2.25]
INFO - 16:24:00: 60%|██████ | 30/50 [00:00<00:00, 240.51 it/sec, feas=False, obj=-2.25]
INFO - 16:24:00: 62%|██████▏ | 31/50 [00:00<00:00, 242.20 it/sec, feas=False, obj=-2.25]
INFO - 16:24:00: 64%|██████▍ | 32/50 [00:00<00:00, 243.91 it/sec, feas=False, obj=-2.25]
INFO - 16:24:00: 66%|██████▌ | 33/50 [00:00<00:00, 245.52 it/sec, feas=False, obj=-2.25]
INFO - 16:24:00: 68%|██████▊ | 34/50 [00:00<00:00, 219.46 it/sec, feas=False, obj=-2.25]
INFO - 16:24:00: 70%|███████ | 35/50 [00:00<00:00, 221.09 it/sec, feas=False, obj=-2.25]
INFO - 16:24:00: 72%|███████▏ | 36/50 [00:00<00:00, 222.91 it/sec, feas=False, obj=-2.25]
INFO - 16:24:00: 74%|███████▍ | 37/50 [00:00<00:00, 224.69 it/sec, feas=False, obj=-2.25]
INFO - 16:24:00: 76%|███████▌ | 38/50 [00:00<00:00, 224.87 it/sec, feas=False, obj=-2.25]
INFO - 16:24:00: 78%|███████▊ | 39/50 [00:00<00:00, 226.46 it/sec, feas=False, obj=-2.25]
INFO - 16:24:00: 80%|████████ | 40/50 [00:00<00:00, 227.93 it/sec, feas=False, obj=-2.25]
INFO - 16:24:00: 82%|████████▏ | 41/50 [00:00<00:00, 229.48 it/sec, feas=False, obj=-2.25]
INFO - 16:24:00: 84%|████████▍ | 42/50 [00:00<00:00, 231.00 it/sec, feas=False, obj=-2.25]
INFO - 16:24:00: 86%|████████▌ | 43/50 [00:00<00:00, 232.41 it/sec, feas=False, obj=-2.25]
INFO - 16:24:00: 88%|████████▊ | 44/50 [00:00<00:00, 233.75 it/sec, feas=False, obj=-2.25]
INFO - 16:24:00: 90%|█████████ | 45/50 [00:00<00:00, 235.05 it/sec, feas=False, obj=-2.25]
INFO - 16:24:00: 92%|█████████▏| 46/50 [00:00<00:00, 236.38 it/sec, feas=False, obj=-2.25]
INFO - 16:24:00: 94%|█████████▍| 47/50 [00:00<00:00, 237.67 it/sec, feas=False, obj=-2.25]
WARNING - 16:24:00: Optimization found no feasible point; the least infeasible point is selected.
INFO - 16:24:00: 96%|█████████▌| 48/50 [00:00<00:00, 219.10 it/sec, feas=False, obj=-2.25]
INFO - 16:24:00: Optimization result:
INFO - 16:24:00: Optimizer info:
INFO - 16:24:00: Status: 8
INFO - 16:24:00: Message: Positive directional derivative for linesearch
INFO - 16:24:00: Solution:
WARNING - 16:24:00: The solution is not feasible.
INFO - 16:24:00: Objective: -2.249886690733171
INFO - 16:24:00: Standardized constraints:
INFO - 16:24:00: g_2 = 0.0002712892361895758
INFO - 16:24:00: Design space:
INFO - 16:24:00: +------+-------------+-------+-------------+-------+
INFO - 16:24:00: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:24:00: +------+-------------+-------+-------------+-------+
INFO - 16:24:00: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:24:00: +------+-------------+-------+-------------+-------+
INFO - 16:24:00: *** End AerodynamicsScenario execution (time: 0:00:00.220675) ***
INFO - 16:24:00: *** Start StructureScenario execution ***
INFO - 16:24:00: StructureScenario
INFO - 16:24:00: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:24:00: MDO formulation: MDF
INFO - 16:24:00: Optimization problem:
INFO - 16:24:00: minimize 0.001*-y_4(x_1)
INFO - 16:24:00: with respect to x_1
INFO - 16:24:00: under the inequality constraints
INFO - 16:24:00: g_1(x_1) <= 0
INFO - 16:24:00: over the design space:
INFO - 16:24:00: +--------+-------------+--------------------+-------------+-------+
INFO - 16:24:00: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:24:00: +--------+-------------+--------------------+-------------+-------+
INFO - 16:24:00: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:24:00: | x_1[1] | 0.75 | 0.7806436836764827 | 1.25 | float |
INFO - 16:24:00: +--------+-------------+--------------------+-------------+-------+
INFO - 16:24:00: Solving optimization problem with algorithm SLSQP:
INFO - 16:24:00: 2%|▏ | 1/50 [00:00<00:00, 70.44 it/sec, feas=True, obj=-2.25]
INFO - 16:24:00: 4%|▍ | 2/50 [00:00<00:00, 54.66 it/sec, feas=True, obj=-2.25]
INFO - 16:24:00: 6%|▌ | 3/50 [00:00<00:00, 72.05 it/sec, feas=True, obj=-2.25]
INFO - 16:24:00: Optimization result:
INFO - 16:24:00: Optimizer info:
INFO - 16:24:00: Status: None
INFO - 16:24:00: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:24:00: Solution:
INFO - 16:24:00: The solution is feasible.
INFO - 16:24:00: Objective: -2.249886690733171
INFO - 16:24:00: Standardized constraints:
INFO - 16:24:00: g_1 = [-3.77226712e-03 -3.22203935e-03 -1.39317275e-02 -2.38726770e-02
INFO - 16:24:00: -3.19646170e-02 -2.40000000e-01 1.36557432e-14]
INFO - 16:24:00: Design space:
INFO - 16:24:00: +--------+-------------+--------------------+-------------+-------+
INFO - 16:24:00: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:24:00: +--------+-------------+--------------------+-------------+-------+
INFO - 16:24:00: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:24:00: | x_1[1] | 0.75 | 0.7806436836764827 | 1.25 | float |
INFO - 16:24:00: +--------+-------------+--------------------+-------------+-------+
INFO - 16:24:00: *** End StructureScenario execution (time: 0:00:00.044063) ***
INFO - 16:24:00: 88%|████████▊ | 88/100 [00:43<00:05, 2.03 it/sec, feas=False, obj=-2.25]
INFO - 16:24:00: *** Start PropulsionScenario execution ***
INFO - 16:24:00: PropulsionScenario
INFO - 16:24:00: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:24:00: MDO formulation: MDF
INFO - 16:24:00: Optimization problem:
INFO - 16:24:00: minimize 0.001*-y_4(x_3)
INFO - 16:24:00: with respect to x_3
INFO - 16:24:00: under the inequality constraints
INFO - 16:24:00: g_3(x_3) <= 0
INFO - 16:24:00: over the design space:
INFO - 16:24:00: +------+-------------+--------------------+-------------+-------+
INFO - 16:24:00: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:24:00: +------+-------------+--------------------+-------------+-------+
INFO - 16:24:00: | x_3 | 0.1 | 0.1582606665836431 | 1 | float |
INFO - 16:24:00: +------+-------------+--------------------+-------------+-------+
INFO - 16:24:00: Solving optimization problem with algorithm SLSQP:
INFO - 16:24:00: 2%|▏ | 1/50 [00:00<00:01, 36.95 it/sec, feas=False, obj=-2.25]
INFO - 16:24:00: 4%|▍ | 2/50 [00:00<00:01, 38.87 it/sec, feas=True, obj=-2.25]
INFO - 16:24:00: 6%|▌ | 3/50 [00:00<00:01, 32.42 it/sec, feas=False, obj=-2.25]
INFO - 16:24:00: 8%|▊ | 4/50 [00:00<00:01, 29.76 it/sec, feas=True, obj=-2.25]
INFO - 16:24:00: 10%|█ | 5/50 [00:00<00:01, 28.53 it/sec, feas=True, obj=-2.25]
INFO - 16:24:00: Optimization result:
INFO - 16:24:00: Optimizer info:
INFO - 16:24:00: Status: 8
INFO - 16:24:00: Message: Positive directional derivative for linesearch
INFO - 16:24:00: Solution:
INFO - 16:24:00: The solution is feasible.
INFO - 16:24:00: Objective: -2.2505970952523993
INFO - 16:24:00: Standardized constraints:
INFO - 16:24:00: g_3 = [-8.37257984e-01 -1.62742016e-01 2.22044605e-16 -1.81449383e-01]
INFO - 16:24:00: Design space:
INFO - 16:24:00: +------+-------------+--------------------+-------------+-------+
INFO - 16:24:00: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:24:00: +------+-------------+--------------------+-------------+-------+
INFO - 16:24:00: | x_3 | 0.1 | 0.1581734215656512 | 1 | float |
INFO - 16:24:00: +------+-------------+--------------------+-------------+-------+
INFO - 16:24:00: *** End PropulsionScenario execution (time: 0:00:00.177353) ***
INFO - 16:24:00: *** Start AerodynamicsScenario execution ***
INFO - 16:24:00: AerodynamicsScenario
INFO - 16:24:00: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:24:00: MDO formulation: MDF
INFO - 16:24:00: Optimization problem:
INFO - 16:24:00: minimize 0.001*-y_4(x_2)
INFO - 16:24:00: with respect to x_2
INFO - 16:24:00: under the inequality constraints
INFO - 16:24:00: g_2(x_2) <= 0
INFO - 16:24:00: over the design space:
INFO - 16:24:00: +------+-------------+-------+-------------+-------+
INFO - 16:24:00: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:24:00: +------+-------------+-------+-------------+-------+
INFO - 16:24:00: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:24:00: +------+-------------+-------+-------------+-------+
INFO - 16:24:00: Solving optimization problem with algorithm SLSQP:
INFO - 16:24:00: 2%|▏ | 1/50 [00:00<00:00, 102.90 it/sec, feas=True, obj=-2.25]
INFO - 16:24:00: Optimization result:
INFO - 16:24:00: Optimizer info:
INFO - 16:24:00: Status: 8
INFO - 16:24:00: Message: Positive directional derivative for linesearch
INFO - 16:24:00: Solution:
INFO - 16:24:00: The solution is feasible.
INFO - 16:24:00: Objective: -2.2505970952523993
INFO - 16:24:00: Standardized constraints:
INFO - 16:24:00: g_2 = -9.902146990548033e-05
INFO - 16:24:00: Design space:
INFO - 16:24:00: +------+-------------+-------+-------------+-------+
INFO - 16:24:00: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:24:00: +------+-------------+-------+-------------+-------+
INFO - 16:24:00: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:24:00: +------+-------------+-------+-------------+-------+
INFO - 16:24:00: *** End AerodynamicsScenario execution (time: 0:00:00.011502) ***
INFO - 16:24:00: *** Start StructureScenario execution ***
INFO - 16:24:00: StructureScenario
INFO - 16:24:00: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:24:00: MDO formulation: MDF
INFO - 16:24:00: Optimization problem:
INFO - 16:24:00: minimize 0.001*-y_4(x_1)
INFO - 16:24:00: with respect to x_1
INFO - 16:24:00: under the inequality constraints
INFO - 16:24:00: g_1(x_1) <= 0
INFO - 16:24:00: over the design space:
INFO - 16:24:00: +--------+-------------+--------------------+-------------+-------+
INFO - 16:24:00: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:24:00: +--------+-------------+--------------------+-------------+-------+
INFO - 16:24:00: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:24:00: | x_1[1] | 0.75 | 0.7806436836764827 | 1.25 | float |
INFO - 16:24:00: +--------+-------------+--------------------+-------------+-------+
INFO - 16:24:00: Solving optimization problem with algorithm SLSQP:
INFO - 16:24:00: 2%|▏ | 1/50 [00:00<00:00, 94.79 it/sec, feas=True, obj=-2.25]
INFO - 16:24:00: Optimization result:
INFO - 16:24:00: Optimizer info:
INFO - 16:24:00: Status: 8
INFO - 16:24:00: Message: Positive directional derivative for linesearch
INFO - 16:24:00: Solution:
INFO - 16:24:00: The solution is feasible.
INFO - 16:24:00: Objective: -2.2505970952523993
INFO - 16:24:00: Standardized constraints:
INFO - 16:24:00: g_1 = [-8.02659130e-04 -1.59362132e-03 -1.28421592e-02 -2.30642601e-02
INFO - 16:24:00: -3.13260683e-02 -2.40000000e-01 1.36557432e-14]
INFO - 16:24:00: Design space:
INFO - 16:24:00: +--------+-------------+--------------------+-------------+-------+
INFO - 16:24:00: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:24:00: +--------+-------------+--------------------+-------------+-------+
INFO - 16:24:00: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:24:00: | x_1[1] | 0.75 | 0.7806436836764827 | 1.25 | float |
INFO - 16:24:00: +--------+-------------+--------------------+-------------+-------+
INFO - 16:24:00: *** End StructureScenario execution (time: 0:00:00.012842) ***
INFO - 16:24:00: *** Start PropulsionScenario execution ***
INFO - 16:24:00: PropulsionScenario
INFO - 16:24:00: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:24:00: MDO formulation: MDF
INFO - 16:24:00: Optimization problem:
INFO - 16:24:00: minimize 0.001*-y_4(x_3)
INFO - 16:24:00: with respect to x_3
INFO - 16:24:00: under the inequality constraints
INFO - 16:24:00: g_3(x_3) <= 0
INFO - 16:24:00: over the design space:
INFO - 16:24:00: +------+-------------+--------------------+-------------+-------+
INFO - 16:24:00: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:24:00: +------+-------------+--------------------+-------------+-------+
INFO - 16:24:00: | x_3 | 0.1 | 0.1581734215656512 | 1 | float |
INFO - 16:24:00: +------+-------------+--------------------+-------------+-------+
INFO - 16:24:00: Solving optimization problem with algorithm SLSQP:
INFO - 16:24:00: 2%|▏ | 1/50 [00:00<00:00, 106.16 it/sec, feas=True, obj=-2.25]
INFO - 16:24:00: Optimization result:
INFO - 16:24:00: Optimizer info:
INFO - 16:24:00: Status: 8
INFO - 16:24:00: Message: Positive directional derivative for linesearch
INFO - 16:24:00: Solution:
INFO - 16:24:00: The solution is feasible.
INFO - 16:24:00: Objective: -2.2505970952523993
INFO - 16:24:00: Standardized constraints:
INFO - 16:24:00: g_3 = [-8.37257984e-01 -1.62742016e-01 2.22044605e-16 -1.81449383e-01]
INFO - 16:24:00: Design space:
INFO - 16:24:00: +------+-------------+--------------------+-------------+-------+
INFO - 16:24:00: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:24:00: +------+-------------+--------------------+-------------+-------+
INFO - 16:24:00: | x_3 | 0.1 | 0.1581734215656512 | 1 | float |
INFO - 16:24:00: +------+-------------+--------------------+-------------+-------+
INFO - 16:24:00: *** End PropulsionScenario execution (time: 0:00:00.011528) ***
INFO - 16:24:00: 89%|████████▉ | 89/100 [00:43<00:05, 2.04 it/sec, feas=True, obj=-2.25]
INFO - 16:24:00: *** Start PropulsionScenario execution ***
INFO - 16:24:00: PropulsionScenario
INFO - 16:24:00: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:24:00: MDO formulation: MDF
INFO - 16:24:00: Optimization problem:
INFO - 16:24:00: minimize 0.001*-y_4(x_3)
INFO - 16:24:00: with respect to x_3
INFO - 16:24:00: under the inequality constraints
INFO - 16:24:00: g_3(x_3) <= 0
INFO - 16:24:00: over the design space:
INFO - 16:24:00: +------+-------------+--------------------+-------------+-------+
INFO - 16:24:00: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:24:00: +------+-------------+--------------------+-------------+-------+
INFO - 16:24:00: | x_3 | 0.1 | 0.1581734215656512 | 1 | float |
INFO - 16:24:00: +------+-------------+--------------------+-------------+-------+
INFO - 16:24:00: Solving optimization problem with algorithm SLSQP:
INFO - 16:24:00: 2%|▏ | 1/50 [00:00<00:01, 38.88 it/sec, feas=True, obj=-2.25]
INFO - 16:24:00: 4%|▍ | 2/50 [00:00<00:01, 29.82 it/sec, feas=True, obj=-2.25]
WARNING - 16:24:00: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 6.724932466608626e-05 is still above the tolerance 1e-06.
INFO - 16:24:00: 6%|▌ | 3/50 [00:00<00:01, 30.92 it/sec, feas=True, obj=-2.25]
INFO - 16:24:00: 8%|▊ | 4/50 [00:00<00:01, 32.92 it/sec, feas=True, obj=-2.25]
INFO - 16:24:00: Optimization result:
INFO - 16:24:00: Optimizer info:
INFO - 16:24:00: Status: None
INFO - 16:24:00: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:24:00: Solution:
INFO - 16:24:00: The solution is feasible.
INFO - 16:24:00: Objective: -2.249766244993501
INFO - 16:24:00: Standardized constraints:
INFO - 16:24:00: g_3 = [-8.36604695e-01 -1.63395305e-01 4.21884749e-15 -1.81383659e-01]
INFO - 16:24:00: Design space:
INFO - 16:24:00: +------+-------------+--------------------+-------------+-------+
INFO - 16:24:00: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:24:00: +------+-------------+--------------------+-------------+-------+
INFO - 16:24:00: | x_3 | 0.1 | 0.1582444352010079 | 1 | float |
INFO - 16:24:00: +------+-------------+--------------------+-------------+-------+
INFO - 16:24:00: *** End PropulsionScenario execution (time: 0:00:00.124338) ***
INFO - 16:24:00: *** Start AerodynamicsScenario execution ***
INFO - 16:24:00: AerodynamicsScenario
INFO - 16:24:00: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:24:00: MDO formulation: MDF
INFO - 16:24:00: Optimization problem:
INFO - 16:24:00: minimize 0.001*-y_4(x_2)
INFO - 16:24:00: with respect to x_2
INFO - 16:24:00: under the inequality constraints
INFO - 16:24:00: g_2(x_2) <= 0
INFO - 16:24:00: over the design space:
INFO - 16:24:00: +------+-------------+-------+-------------+-------+
INFO - 16:24:00: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:24:00: +------+-------------+-------+-------------+-------+
INFO - 16:24:00: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:24:00: +------+-------------+-------+-------------+-------+
INFO - 16:24:00: Solving optimization problem with algorithm SLSQP:
INFO - 16:24:00: 2%|▏ | 1/50 [00:00<00:00, 82.74 it/sec, feas=True, obj=-2.25]
INFO - 16:24:00: Optimization result:
INFO - 16:24:00: Optimizer info:
INFO - 16:24:00: Status: 8
INFO - 16:24:00: Message: Positive directional derivative for linesearch
INFO - 16:24:00: Solution:
INFO - 16:24:00: The solution is feasible.
INFO - 16:24:00: Objective: -2.249766244993501
INFO - 16:24:00: Standardized constraints:
INFO - 16:24:00: g_2 = -7.311973069579203e-05
INFO - 16:24:00: Design space:
INFO - 16:24:00: +------+-------------+-------+-------------+-------+
INFO - 16:24:00: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:24:00: +------+-------------+-------+-------------+-------+
INFO - 16:24:00: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:24:00: +------+-------------+-------+-------------+-------+
INFO - 16:24:00: *** End AerodynamicsScenario execution (time: 0:00:00.013823) ***
INFO - 16:24:00: *** Start StructureScenario execution ***
INFO - 16:24:00: StructureScenario
INFO - 16:24:00: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:24:00: MDO formulation: MDF
INFO - 16:24:00: Optimization problem:
INFO - 16:24:00: minimize 0.001*-y_4(x_1)
INFO - 16:24:00: with respect to x_1
INFO - 16:24:00: under the inequality constraints
INFO - 16:24:00: g_1(x_1) <= 0
INFO - 16:24:00: over the design space:
INFO - 16:24:00: +--------+-------------+--------------------+-------------+-------+
INFO - 16:24:00: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:24:00: +--------+-------------+--------------------+-------------+-------+
INFO - 16:24:00: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:24:00: | x_1[1] | 0.75 | 0.7806436836764827 | 1.25 | float |
INFO - 16:24:00: +--------+-------------+--------------------+-------------+-------+
INFO - 16:24:00: Solving optimization problem with algorithm SLSQP:
INFO - 16:24:00: 2%|▏ | 1/50 [00:00<00:00, 97.76 it/sec, feas=True, obj=-2.25]
INFO - 16:24:00: 4%|▍ | 2/50 [00:00<00:00, 106.93 it/sec, feas=True, obj=-2.25]
INFO - 16:24:00: 6%|▌ | 3/50 [00:00<00:00, 114.64 it/sec, feas=True, obj=-2.25]
INFO - 16:24:00: Optimization result:
INFO - 16:24:00: Optimizer info:
INFO - 16:24:00: Status: None
INFO - 16:24:00: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:24:00: Solution:
INFO - 16:24:00: The solution is feasible.
INFO - 16:24:00: Objective: -2.249766244993501
INFO - 16:24:00: Standardized constraints:
INFO - 16:24:00: g_1 = [-1.01009245e-03 -1.70739869e-03 -1.29183004e-02 -2.31207610e-02
INFO - 16:24:00: -3.13707012e-02 -2.40000000e-01 1.36557432e-14]
INFO - 16:24:00: Design space:
INFO - 16:24:00: +--------+-------------+--------------------+-------------+-------+
INFO - 16:24:00: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:24:00: +--------+-------------+--------------------+-------------+-------+
INFO - 16:24:00: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:24:00: | x_1[1] | 0.75 | 0.7806436836764827 | 1.25 | float |
INFO - 16:24:00: +--------+-------------+--------------------+-------------+-------+
INFO - 16:24:00: *** End StructureScenario execution (time: 0:00:00.028539) ***
INFO - 16:24:00: *** Start PropulsionScenario execution ***
INFO - 16:24:00: PropulsionScenario
INFO - 16:24:00: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:24:00: MDO formulation: MDF
INFO - 16:24:00: Optimization problem:
INFO - 16:24:00: minimize 0.001*-y_4(x_3)
INFO - 16:24:00: with respect to x_3
INFO - 16:24:00: under the inequality constraints
INFO - 16:24:00: g_3(x_3) <= 0
INFO - 16:24:00: over the design space:
INFO - 16:24:00: +------+-------------+--------------------+-------------+-------+
INFO - 16:24:00: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:24:00: +------+-------------+--------------------+-------------+-------+
INFO - 16:24:00: | x_3 | 0.1 | 0.1582444352010079 | 1 | float |
INFO - 16:24:00: +------+-------------+--------------------+-------------+-------+
INFO - 16:24:00: Solving optimization problem with algorithm SLSQP:
INFO - 16:24:00: 2%|▏ | 1/50 [00:00<00:00, 72.56 it/sec, feas=True, obj=-2.25]
INFO - 16:24:00: Optimization result:
INFO - 16:24:00: Optimizer info:
INFO - 16:24:00: Status: 8
INFO - 16:24:00: Message: Positive directional derivative for linesearch
INFO - 16:24:00: Solution:
INFO - 16:24:00: The solution is feasible.
INFO - 16:24:00: Objective: -2.249766244993501
INFO - 16:24:00: Standardized constraints:
INFO - 16:24:00: g_3 = [-8.36604695e-01 -1.63395305e-01 4.21884749e-15 -1.81383659e-01]
INFO - 16:24:00: Design space:
INFO - 16:24:00: +------+-------------+--------------------+-------------+-------+
INFO - 16:24:00: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:24:00: +------+-------------+--------------------+-------------+-------+
INFO - 16:24:00: | x_3 | 0.1 | 0.1582444352010079 | 1 | float |
INFO - 16:24:00: +------+-------------+--------------------+-------------+-------+
INFO - 16:24:00: *** End PropulsionScenario execution (time: 0:00:00.015514) ***
INFO - 16:24:00: *** Start AerodynamicsScenario execution ***
INFO - 16:24:00: AerodynamicsScenario
INFO - 16:24:00: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:24:00: MDO formulation: MDF
INFO - 16:24:00: Optimization problem:
INFO - 16:24:00: minimize 0.001*-y_4(x_2)
INFO - 16:24:00: with respect to x_2
INFO - 16:24:00: under the inequality constraints
INFO - 16:24:00: g_2(x_2) <= 0
INFO - 16:24:00: over the design space:
INFO - 16:24:00: +------+-------------+-------+-------------+-------+
INFO - 16:24:00: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:24:00: +------+-------------+-------+-------------+-------+
INFO - 16:24:00: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:24:00: +------+-------------+-------+-------------+-------+
INFO - 16:24:00: Solving optimization problem with algorithm SLSQP:
INFO - 16:24:00: 2%|▏ | 1/50 [00:00<00:00, 107.68 it/sec, feas=True, obj=-2.25]
INFO - 16:24:00: Optimization result:
INFO - 16:24:00: Optimizer info:
INFO - 16:24:00: Status: 8
INFO - 16:24:00: Message: Positive directional derivative for linesearch
INFO - 16:24:00: Solution:
INFO - 16:24:00: The solution is feasible.
INFO - 16:24:00: Objective: -2.249766244993501
INFO - 16:24:00: Standardized constraints:
INFO - 16:24:00: g_2 = -7.311973069579203e-05
INFO - 16:24:00: Design space:
INFO - 16:24:00: +------+-------------+-------+-------------+-------+
INFO - 16:24:00: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:24:00: +------+-------------+-------+-------------+-------+
INFO - 16:24:00: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:24:00: +------+-------------+-------+-------------+-------+
INFO - 16:24:00: *** End AerodynamicsScenario execution (time: 0:00:00.010768) ***
INFO - 16:24:00: 90%|█████████ | 90/100 [00:43<00:04, 2.06 it/sec, feas=True, obj=-2.25]
INFO - 16:24:00: *** Start PropulsionScenario execution ***
INFO - 16:24:00: PropulsionScenario
INFO - 16:24:00: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:24:00: MDO formulation: MDF
INFO - 16:24:00: Optimization problem:
INFO - 16:24:00: minimize 0.001*-y_4(x_3)
INFO - 16:24:00: with respect to x_3
INFO - 16:24:00: under the inequality constraints
INFO - 16:24:00: g_3(x_3) <= 0
INFO - 16:24:00: over the design space:
INFO - 16:24:00: +------+-------------+--------------------+-------------+-------+
INFO - 16:24:00: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:24:00: +------+-------------+--------------------+-------------+-------+
INFO - 16:24:00: | x_3 | 0.1 | 0.1582444352010079 | 1 | float |
INFO - 16:24:00: +------+-------------+--------------------+-------------+-------+
INFO - 16:24:00: Solving optimization problem with algorithm SLSQP:
INFO - 16:24:00: 2%|▏ | 1/50 [00:00<00:01, 41.07 it/sec, feas=True, obj=-2.25]
INFO - 16:24:00: 4%|▍ | 2/50 [00:00<00:01, 41.32 it/sec, feas=True, obj=-2.25]
INFO - 16:24:00: 6%|▌ | 3/50 [00:00<00:01, 34.29 it/sec, feas=True, obj=-2.25]
INFO - 16:24:00: 8%|▊ | 4/50 [00:00<00:01, 30.80 it/sec, feas=True, obj=-2.25]
INFO - 16:24:00: 10%|█ | 5/50 [00:00<00:01, 32.24 it/sec, feas=True, obj=-2.25]
INFO - 16:24:00: Optimization result:
INFO - 16:24:00: Optimizer info:
INFO - 16:24:00: Status: 8
INFO - 16:24:00: Message: Positive directional derivative for linesearch
INFO - 16:24:00: Solution:
INFO - 16:24:00: The solution is feasible.
INFO - 16:24:00: Objective: -2.2497119794288376
INFO - 16:24:00: Standardized constraints:
INFO - 16:24:00: g_3 = [-8.36451374e-01 -1.63548626e-01 8.67413351e-05 -1.81396358e-01]
INFO - 16:24:00: Design space:
INFO - 16:24:00: +------+-------------+--------------------+-------------+-------+
INFO - 16:24:00: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:24:00: +------+-------------+--------------------+-------------+-------+
INFO - 16:24:00: | x_3 | 0.1 | 0.1582444352010079 | 1 | float |
INFO - 16:24:00: +------+-------------+--------------------+-------------+-------+
INFO - 16:24:00: *** End PropulsionScenario execution (time: 0:00:00.157431) ***
INFO - 16:24:00: *** Start AerodynamicsScenario execution ***
INFO - 16:24:00: AerodynamicsScenario
INFO - 16:24:00: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:24:00: MDO formulation: MDF
INFO - 16:24:00: Optimization problem:
INFO - 16:24:00: minimize 0.001*-y_4(x_2)
INFO - 16:24:00: with respect to x_2
INFO - 16:24:00: under the inequality constraints
INFO - 16:24:00: g_2(x_2) <= 0
INFO - 16:24:00: over the design space:
INFO - 16:24:00: +------+-------------+-------+-------------+-------+
INFO - 16:24:00: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:24:00: +------+-------------+-------+-------------+-------+
INFO - 16:24:00: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:24:00: +------+-------------+-------+-------------+-------+
INFO - 16:24:00: Solving optimization problem with algorithm SLSQP:
INFO - 16:24:00: 2%|▏ | 1/50 [00:00<00:00, 91.78 it/sec, feas=True, obj=-2.25]
INFO - 16:24:00: Optimization result:
INFO - 16:24:00: Optimizer info:
INFO - 16:24:00: Status: 8
INFO - 16:24:00: Message: Positive directional derivative for linesearch
INFO - 16:24:00: Solution:
INFO - 16:24:00: The solution is feasible.
INFO - 16:24:00: Objective: -2.2497119794288376
INFO - 16:24:00: Standardized constraints:
INFO - 16:24:00: g_2 = -2.220446049250313e-16
INFO - 16:24:00: Design space:
INFO - 16:24:00: +------+-------------+-------+-------------+-------+
INFO - 16:24:00: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:24:00: +------+-------------+-------+-------------+-------+
INFO - 16:24:00: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:24:00: +------+-------------+-------+-------------+-------+
INFO - 16:24:00: *** End AerodynamicsScenario execution (time: 0:00:00.012613) ***
INFO - 16:24:00: *** Start StructureScenario execution ***
INFO - 16:24:00: StructureScenario
INFO - 16:24:00: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:24:00: MDO formulation: MDF
INFO - 16:24:00: Optimization problem:
INFO - 16:24:00: minimize 0.001*-y_4(x_1)
INFO - 16:24:00: with respect to x_1
INFO - 16:24:00: under the inequality constraints
INFO - 16:24:00: g_1(x_1) <= 0
INFO - 16:24:00: over the design space:
INFO - 16:24:00: +--------+-------------+--------------------+-------------+-------+
INFO - 16:24:00: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:24:00: +--------+-------------+--------------------+-------------+-------+
INFO - 16:24:00: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:24:00: | x_1[1] | 0.75 | 0.7806436836764827 | 1.25 | float |
INFO - 16:24:00: +--------+-------------+--------------------+-------------+-------+
INFO - 16:24:00: Solving optimization problem with algorithm SLSQP:
INFO - 16:24:00: 2%|▏ | 1/50 [00:00<00:00, 97.35 it/sec, feas=True, obj=-2.25]
INFO - 16:24:00: 4%|▍ | 2/50 [00:00<00:00, 59.29 it/sec, feas=True, obj=-2.25]
INFO - 16:24:00: Optimization result:
INFO - 16:24:00: Optimizer info:
INFO - 16:24:00: Status: 8
INFO - 16:24:00: Message: Positive directional derivative for linesearch
INFO - 16:24:00: Solution:
INFO - 16:24:00: The solution is feasible.
INFO - 16:24:00: Objective: -2.2497119794288376
INFO - 16:24:00: Standardized constraints:
INFO - 16:24:00: g_1 = [-1.59589593e-03 -2.02868890e-03 -1.31333010e-02 -2.32802973e-02
INFO - 16:24:00: -3.14967236e-02 -2.40000000e-01 1.36557432e-14]
INFO - 16:24:00: Design space:
INFO - 16:24:00: +--------+-------------+--------------------+-------------+-------+
INFO - 16:24:00: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:24:00: +--------+-------------+--------------------+-------------+-------+
INFO - 16:24:00: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:24:00: | x_1[1] | 0.75 | 0.7806436836764827 | 1.25 | float |
INFO - 16:24:00: +--------+-------------+--------------------+-------------+-------+
INFO - 16:24:00: *** End StructureScenario execution (time: 0:00:00.036121) ***
INFO - 16:24:00: *** Start PropulsionScenario execution ***
INFO - 16:24:00: PropulsionScenario
INFO - 16:24:00: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:24:00: MDO formulation: MDF
INFO - 16:24:00: Optimization problem:
INFO - 16:24:00: minimize 0.001*-y_4(x_3)
INFO - 16:24:00: with respect to x_3
INFO - 16:24:00: under the inequality constraints
INFO - 16:24:00: g_3(x_3) <= 0
INFO - 16:24:00: over the design space:
INFO - 16:24:00: +------+-------------+--------------------+-------------+-------+
INFO - 16:24:00: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:24:00: +------+-------------+--------------------+-------------+-------+
INFO - 16:24:00: | x_3 | 0.1 | 0.1582444352010079 | 1 | float |
INFO - 16:24:00: +------+-------------+--------------------+-------------+-------+
INFO - 16:24:00: Solving optimization problem with algorithm SLSQP:
INFO - 16:24:00: 2%|▏ | 1/50 [00:00<00:00, 90.51 it/sec, feas=True, obj=-2.25]
INFO - 16:24:00: 4%|▍ | 2/50 [00:00<00:00, 73.45 it/sec, feas=True, obj=-2.25]
INFO - 16:24:00: 6%|▌ | 3/50 [00:00<00:00, 49.73 it/sec, feas=True, obj=-2.25]
INFO - 16:24:01: 8%|▊ | 4/50 [00:00<00:01, 42.87 it/sec, feas=True, obj=-2.25]
INFO - 16:24:01: 10%|█ | 5/50 [00:00<00:01, 44.67 it/sec, feas=True, obj=-2.25]
INFO - 16:24:01: Optimization result:
INFO - 16:24:01: Optimizer info:
INFO - 16:24:01: Status: 8
INFO - 16:24:01: Message: Positive directional derivative for linesearch
INFO - 16:24:01: Solution:
INFO - 16:24:01: The solution is feasible.
INFO - 16:24:01: Objective: -2.2497119794288376
INFO - 16:24:01: Standardized constraints:
INFO - 16:24:01: g_3 = [-8.36451374e-01 -1.63548626e-01 8.67413351e-05 -1.81396358e-01]
INFO - 16:24:01: Design space:
INFO - 16:24:01: +------+-------------+--------------------+-------------+-------+
INFO - 16:24:01: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:24:01: +------+-------------+--------------------+-------------+-------+
INFO - 16:24:01: | x_3 | 0.1 | 0.1582444352010079 | 1 | float |
INFO - 16:24:01: +------+-------------+--------------------+-------------+-------+
INFO - 16:24:01: *** End PropulsionScenario execution (time: 0:00:00.113962) ***
INFO - 16:24:01: 91%|█████████ | 91/100 [00:44<00:04, 2.06 it/sec, feas=True, obj=-2.25]
INFO - 16:24:01: *** Start PropulsionScenario execution ***
INFO - 16:24:01: PropulsionScenario
INFO - 16:24:01: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:24:01: MDO formulation: MDF
INFO - 16:24:01: Optimization problem:
INFO - 16:24:01: minimize 0.001*-y_4(x_3)
INFO - 16:24:01: with respect to x_3
INFO - 16:24:01: under the inequality constraints
INFO - 16:24:01: g_3(x_3) <= 0
INFO - 16:24:01: over the design space:
INFO - 16:24:01: +------+-------------+--------------------+-------------+-------+
INFO - 16:24:01: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:24:01: +------+-------------+--------------------+-------------+-------+
INFO - 16:24:01: | x_3 | 0.1 | 0.1582444352010079 | 1 | float |
INFO - 16:24:01: +------+-------------+--------------------+-------------+-------+
INFO - 16:24:01: Solving optimization problem with algorithm SLSQP:
INFO - 16:24:01: 2%|▏ | 1/50 [00:00<00:01, 40.33 it/sec, feas=True, obj=-2.25]
INFO - 16:24:01: 4%|▍ | 2/50 [00:00<00:01, 30.87 it/sec, feas=True, obj=-2.25]
INFO - 16:24:01: 6%|▌ | 3/50 [00:00<00:01, 28.89 it/sec, feas=True, obj=-2.25]
INFO - 16:24:01: 8%|▊ | 4/50 [00:00<00:01, 31.51 it/sec, feas=True, obj=-2.25]
INFO - 16:24:01: Optimization result:
INFO - 16:24:01: Optimizer info:
INFO - 16:24:01: Status: None
INFO - 16:24:01: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:24:01: Solution:
INFO - 16:24:01: The solution is feasible.
INFO - 16:24:01: Objective: -2.248685842046949
INFO - 16:24:01: Standardized constraints:
INFO - 16:24:01: g_3 = [-0.83641728 -0.16358272 0. -0.18137237]
INFO - 16:24:01: Design space:
INFO - 16:24:01: +------+-------------+--------------------+-------------+-------+
INFO - 16:24:01: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:24:01: +------+-------------+--------------------+-------------+-------+
INFO - 16:24:01: | x_3 | 0.1 | 0.1582651781707321 | 1 | float |
INFO - 16:24:01: +------+-------------+--------------------+-------------+-------+
INFO - 16:24:01: *** End PropulsionScenario execution (time: 0:00:00.129553) ***
INFO - 16:24:01: *** Start AerodynamicsScenario execution ***
INFO - 16:24:01: AerodynamicsScenario
INFO - 16:24:01: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:24:01: MDO formulation: MDF
INFO - 16:24:01: Optimization problem:
INFO - 16:24:01: minimize 0.001*-y_4(x_2)
INFO - 16:24:01: with respect to x_2
INFO - 16:24:01: under the inequality constraints
INFO - 16:24:01: g_2(x_2) <= 0
INFO - 16:24:01: over the design space:
INFO - 16:24:01: +------+-------------+-------+-------------+-------+
INFO - 16:24:01: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:24:01: +------+-------------+-------+-------------+-------+
INFO - 16:24:01: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:24:01: +------+-------------+-------+-------------+-------+
INFO - 16:24:01: Solving optimization problem with algorithm SLSQP:
INFO - 16:24:01: 2%|▏ | 1/50 [00:00<00:00, 75.59 it/sec, feas=True, obj=-2.25]
INFO - 16:24:01: Optimization result:
INFO - 16:24:01: Optimizer info:
INFO - 16:24:01: Status: 8
INFO - 16:24:01: Message: Positive directional derivative for linesearch
INFO - 16:24:01: Solution:
INFO - 16:24:01: The solution is feasible.
INFO - 16:24:01: Objective: -2.248685842046949
INFO - 16:24:01: Standardized constraints:
INFO - 16:24:01: g_2 = 3.1864441574214197e-07
INFO - 16:24:01: Design space:
INFO - 16:24:01: +------+-------------+-------+-------------+-------+
INFO - 16:24:01: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:24:01: +------+-------------+-------+-------------+-------+
INFO - 16:24:01: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:24:01: +------+-------------+-------+-------------+-------+
INFO - 16:24:01: *** End AerodynamicsScenario execution (time: 0:00:00.015084) ***
INFO - 16:24:01: *** Start StructureScenario execution ***
INFO - 16:24:01: StructureScenario
INFO - 16:24:01: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:24:01: MDO formulation: MDF
INFO - 16:24:01: Optimization problem:
INFO - 16:24:01: minimize 0.001*-y_4(x_1)
INFO - 16:24:01: with respect to x_1
INFO - 16:24:01: under the inequality constraints
INFO - 16:24:01: g_1(x_1) <= 0
INFO - 16:24:01: over the design space:
INFO - 16:24:01: +--------+-------------+--------------------+-------------+-------+
INFO - 16:24:01: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:24:01: +--------+-------------+--------------------+-------------+-------+
INFO - 16:24:01: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:24:01: | x_1[1] | 0.75 | 0.7806436836764827 | 1.25 | float |
INFO - 16:24:01: +--------+-------------+--------------------+-------------+-------+
INFO - 16:24:01: Solving optimization problem with algorithm SLSQP:
INFO - 16:24:01: 2%|▏ | 1/50 [00:00<00:00, 76.33 it/sec, feas=True, obj=-2.25]
INFO - 16:24:01: Optimization result:
INFO - 16:24:01: Optimizer info:
INFO - 16:24:01: Status: 8
INFO - 16:24:01: Message: Positive directional derivative for linesearch
INFO - 16:24:01: Solution:
INFO - 16:24:01: The solution is feasible.
INFO - 16:24:01: Objective: -2.248685842046949
INFO - 16:24:01: Standardized constraints:
INFO - 16:24:01: g_1 = [-1.59844950e-03 -2.03008936e-03 -1.31342382e-02 -2.32809927e-02
INFO - 16:24:01: -3.14972729e-02 -2.40000000e-01 1.36557432e-14]
INFO - 16:24:01: Design space:
INFO - 16:24:01: +--------+-------------+--------------------+-------------+-------+
INFO - 16:24:01: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:24:01: +--------+-------------+--------------------+-------------+-------+
INFO - 16:24:01: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:24:01: | x_1[1] | 0.75 | 0.7806436836764827 | 1.25 | float |
INFO - 16:24:01: +--------+-------------+--------------------+-------------+-------+
INFO - 16:24:01: *** End StructureScenario execution (time: 0:00:00.015655) ***
INFO - 16:24:01: *** Start PropulsionScenario execution ***
INFO - 16:24:01: PropulsionScenario
INFO - 16:24:01: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:24:01: MDO formulation: MDF
INFO - 16:24:01: Optimization problem:
INFO - 16:24:01: minimize 0.001*-y_4(x_3)
INFO - 16:24:01: with respect to x_3
INFO - 16:24:01: under the inequality constraints
INFO - 16:24:01: g_3(x_3) <= 0
INFO - 16:24:01: over the design space:
INFO - 16:24:01: +------+-------------+--------------------+-------------+-------+
INFO - 16:24:01: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:24:01: +------+-------------+--------------------+-------------+-------+
INFO - 16:24:01: | x_3 | 0.1 | 0.1582651781707321 | 1 | float |
INFO - 16:24:01: +------+-------------+--------------------+-------------+-------+
INFO - 16:24:01: Solving optimization problem with algorithm SLSQP:
INFO - 16:24:01: 2%|▏ | 1/50 [00:00<00:00, 108.14 it/sec, feas=True, obj=-2.25]
INFO - 16:24:01: 4%|▍ | 2/50 [00:00<00:00, 140.99 it/sec, feas=True, obj=-2.25]
INFO - 16:24:01: 6%|▌ | 3/50 [00:00<00:00, 164.61 it/sec, feas=True, obj=-2.25]
INFO - 16:24:01: Optimization result:
INFO - 16:24:01: Optimizer info:
INFO - 16:24:01: Status: None
INFO - 16:24:01: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:24:01: Solution:
INFO - 16:24:01: The solution is feasible.
INFO - 16:24:01: Objective: -2.24868584204695
INFO - 16:24:01: Standardized constraints:
INFO - 16:24:01: g_3 = [-8.36417285e-01 -1.63582715e-01 4.88498131e-15 -1.81372370e-01]
INFO - 16:24:01: Design space:
INFO - 16:24:01: +------+-------------+--------------------+-------------+-------+
INFO - 16:24:01: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:24:01: +------+-------------+--------------------+-------------+-------+
INFO - 16:24:01: | x_3 | 0.1 | 0.1582651781707329 | 1 | float |
INFO - 16:24:01: +------+-------------+--------------------+-------------+-------+
INFO - 16:24:01: *** End PropulsionScenario execution (time: 0:00:00.020802) ***
INFO - 16:24:01: *** Start AerodynamicsScenario execution ***
INFO - 16:24:01: AerodynamicsScenario
INFO - 16:24:01: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:24:01: MDO formulation: MDF
INFO - 16:24:01: Optimization problem:
INFO - 16:24:01: minimize 0.001*-y_4(x_2)
INFO - 16:24:01: with respect to x_2
INFO - 16:24:01: under the inequality constraints
INFO - 16:24:01: g_2(x_2) <= 0
INFO - 16:24:01: over the design space:
INFO - 16:24:01: +------+-------------+-------+-------------+-------+
INFO - 16:24:01: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:24:01: +------+-------------+-------+-------------+-------+
INFO - 16:24:01: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:24:01: +------+-------------+-------+-------------+-------+
INFO - 16:24:01: Solving optimization problem with algorithm SLSQP:
INFO - 16:24:01: 2%|▏ | 1/50 [00:00<00:00, 80.38 it/sec, feas=True, obj=-2.25]
INFO - 16:24:01: Optimization result:
INFO - 16:24:01: Optimizer info:
INFO - 16:24:01: Status: 8
INFO - 16:24:01: Message: Positive directional derivative for linesearch
INFO - 16:24:01: Solution:
INFO - 16:24:01: The solution is feasible.
INFO - 16:24:01: Objective: -2.248685842046951
INFO - 16:24:01: Standardized constraints:
INFO - 16:24:01: g_2 = 3.1864441574214197e-07
INFO - 16:24:01: Design space:
INFO - 16:24:01: +------+-------------+-------+-------------+-------+
INFO - 16:24:01: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:24:01: +------+-------------+-------+-------------+-------+
INFO - 16:24:01: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:24:01: +------+-------------+-------+-------------+-------+
INFO - 16:24:01: *** End AerodynamicsScenario execution (time: 0:00:00.014314) ***
INFO - 16:24:01: *** Start StructureScenario execution ***
INFO - 16:24:01: StructureScenario
INFO - 16:24:01: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:24:01: MDO formulation: MDF
INFO - 16:24:01: Optimization problem:
INFO - 16:24:01: minimize 0.001*-y_4(x_1)
INFO - 16:24:01: with respect to x_1
INFO - 16:24:01: under the inequality constraints
INFO - 16:24:01: g_1(x_1) <= 0
INFO - 16:24:01: over the design space:
INFO - 16:24:01: +--------+-------------+--------------------+-------------+-------+
INFO - 16:24:01: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:24:01: +--------+-------------+--------------------+-------------+-------+
INFO - 16:24:01: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:24:01: | x_1[1] | 0.75 | 0.7806436836764827 | 1.25 | float |
INFO - 16:24:01: +--------+-------------+--------------------+-------------+-------+
INFO - 16:24:01: Solving optimization problem with algorithm SLSQP:
INFO - 16:24:01: 2%|▏ | 1/50 [00:00<00:00, 83.81 it/sec, feas=True, obj=-2.25]
INFO - 16:24:01: 4%|▍ | 2/50 [00:00<00:00, 57.26 it/sec, feas=True, obj=-2.25]
INFO - 16:24:01: Optimization result:
INFO - 16:24:01: Optimizer info:
INFO - 16:24:01: Status: 8
INFO - 16:24:01: Message: Positive directional derivative for linesearch
INFO - 16:24:01: Solution:
INFO - 16:24:01: The solution is feasible.
INFO - 16:24:01: Objective: -2.24868584204695
INFO - 16:24:01: Standardized constraints:
INFO - 16:24:01: g_1 = [-1.59844950e-03 -2.03008936e-03 -1.31342382e-02 -2.32809927e-02
INFO - 16:24:01: -3.14972729e-02 -2.40000000e-01 1.36557432e-14]
INFO - 16:24:01: Design space:
INFO - 16:24:01: +--------+-------------+--------------------+-------------+-------+
INFO - 16:24:01: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:24:01: +--------+-------------+--------------------+-------------+-------+
INFO - 16:24:01: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:24:01: | x_1[1] | 0.75 | 0.7806436836764827 | 1.25 | float |
INFO - 16:24:01: +--------+-------------+--------------------+-------------+-------+
INFO - 16:24:01: *** End StructureScenario execution (time: 0:00:00.037293) ***
INFO - 16:24:01: 92%|█████████▏| 92/100 [00:44<00:03, 2.07 it/sec, feas=True, obj=-2.25]
INFO - 16:24:01: *** Start PropulsionScenario execution ***
INFO - 16:24:01: PropulsionScenario
INFO - 16:24:01: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:24:01: MDO formulation: MDF
INFO - 16:24:01: Optimization problem:
INFO - 16:24:01: minimize 0.001*-y_4(x_3)
INFO - 16:24:01: with respect to x_3
INFO - 16:24:01: under the inequality constraints
INFO - 16:24:01: g_3(x_3) <= 0
INFO - 16:24:01: over the design space:
INFO - 16:24:01: +------+-------------+--------------------+-------------+-------+
INFO - 16:24:01: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:24:01: +------+-------------+--------------------+-------------+-------+
INFO - 16:24:01: | x_3 | 0.1 | 0.1582651781707329 | 1 | float |
INFO - 16:24:01: +------+-------------+--------------------+-------------+-------+
INFO - 16:24:01: Solving optimization problem with algorithm SLSQP:
INFO - 16:24:01: 2%|▏ | 1/50 [00:00<00:01, 42.80 it/sec, feas=True, obj=-2.25]
INFO - 16:24:01: 4%|▍ | 2/50 [00:00<00:01, 44.78 it/sec, feas=True, obj=-2.25]
INFO - 16:24:01: 6%|▌ | 3/50 [00:00<00:01, 36.52 it/sec, feas=True, obj=-2.25]
INFO - 16:24:01: 8%|▊ | 4/50 [00:00<00:01, 33.14 it/sec, feas=True, obj=-2.25]
INFO - 16:24:01: 10%|█ | 5/50 [00:00<00:01, 31.51 it/sec, feas=True, obj=-2.25]
WARNING - 16:24:01: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 6.724932466608626e-05 is still above the tolerance 1e-06.
INFO - 16:24:01: 12%|█▏ | 6/50 [00:00<00:01, 31.83 it/sec, feas=True, obj=-2.25]
INFO - 16:24:01: Optimization result:
INFO - 16:24:01: Optimizer info:
INFO - 16:24:01: Status: None
INFO - 16:24:01: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:24:01: Solution:
INFO - 16:24:01: The solution is feasible.
INFO - 16:24:01: Objective: -2.2495639254119877
INFO - 16:24:01: Standardized constraints:
INFO - 16:24:01: g_3 = [-8.36427671e-01 -1.63572329e-01 7.40469641e-05 -1.81375311e-01]
INFO - 16:24:01: Design space:
INFO - 16:24:01: +------+-------------+--------------------+-------------+-------+
INFO - 16:24:01: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:24:01: +------+-------------+--------------------+-------------+-------+
INFO - 16:24:01: | x_3 | 0.1 | 0.1582651781707329 | 1 | float |
INFO - 16:24:01: +------+-------------+--------------------+-------------+-------+
INFO - 16:24:01: *** End PropulsionScenario execution (time: 0:00:00.191214) ***
INFO - 16:24:01: *** Start AerodynamicsScenario execution ***
INFO - 16:24:01: AerodynamicsScenario
INFO - 16:24:01: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:24:01: MDO formulation: MDF
INFO - 16:24:01: Optimization problem:
INFO - 16:24:01: minimize 0.001*-y_4(x_2)
INFO - 16:24:01: with respect to x_2
INFO - 16:24:01: under the inequality constraints
INFO - 16:24:01: g_2(x_2) <= 0
INFO - 16:24:01: over the design space:
INFO - 16:24:01: +------+-------------+-------+-------------+-------+
INFO - 16:24:01: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:24:01: +------+-------------+-------+-------------+-------+
INFO - 16:24:01: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:24:01: +------+-------------+-------+-------------+-------+
INFO - 16:24:01: Solving optimization problem with algorithm SLSQP:
INFO - 16:24:01: 2%|▏ | 1/50 [00:00<00:00, 85.79 it/sec, feas=True, obj=-2.25]
INFO - 16:24:01: Optimization result:
INFO - 16:24:01: Optimizer info:
INFO - 16:24:01: Status: 8
INFO - 16:24:01: Message: Positive directional derivative for linesearch
INFO - 16:24:01: Solution:
INFO - 16:24:01: The solution is feasible.
INFO - 16:24:01: Objective: -2.2495639254119877
INFO - 16:24:01: Standardized constraints:
INFO - 16:24:01: g_2 = 0.0
INFO - 16:24:01: Design space:
INFO - 16:24:01: +------+-------------+-------+-------------+-------+
INFO - 16:24:01: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:24:01: +------+-------------+-------+-------------+-------+
INFO - 16:24:01: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:24:01: +------+-------------+-------+-------------+-------+
INFO - 16:24:01: *** End AerodynamicsScenario execution (time: 0:00:00.013505) ***
INFO - 16:24:01: *** Start StructureScenario execution ***
INFO - 16:24:01: StructureScenario
INFO - 16:24:01: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:24:01: MDO formulation: MDF
INFO - 16:24:01: Optimization problem:
INFO - 16:24:01: minimize 0.001*-y_4(x_1)
INFO - 16:24:01: with respect to x_1
INFO - 16:24:01: under the inequality constraints
INFO - 16:24:01: g_1(x_1) <= 0
INFO - 16:24:01: over the design space:
INFO - 16:24:01: +--------+-------------+--------------------+-------------+-------+
INFO - 16:24:01: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:24:01: +--------+-------------+--------------------+-------------+-------+
INFO - 16:24:01: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:24:01: | x_1[1] | 0.75 | 0.7806436836764827 | 1.25 | float |
INFO - 16:24:01: +--------+-------------+--------------------+-------------+-------+
INFO - 16:24:01: Solving optimization problem with algorithm SLSQP:
INFO - 16:24:01: 2%|▏ | 1/50 [00:00<00:00, 95.42 it/sec, feas=True, obj=-2.25]
INFO - 16:24:01: Optimization result:
INFO - 16:24:01: Optimizer info:
INFO - 16:24:01: Status: 8
INFO - 16:24:01: Message: Positive directional derivative for linesearch
INFO - 16:24:01: Solution:
INFO - 16:24:01: The solution is feasible.
INFO - 16:24:01: Objective: -2.2495639254119877
INFO - 16:24:01: Standardized constraints:
INFO - 16:24:01: g_1 = [-1.59589593e-03 -2.02868890e-03 -1.31333010e-02 -2.32802973e-02
INFO - 16:24:01: -3.14967236e-02 -2.40000000e-01 1.36557432e-14]
INFO - 16:24:01: Design space:
INFO - 16:24:01: +--------+-------------+--------------------+-------------+-------+
INFO - 16:24:01: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:24:01: +--------+-------------+--------------------+-------------+-------+
INFO - 16:24:01: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:24:01: | x_1[1] | 0.75 | 0.7806436836764827 | 1.25 | float |
INFO - 16:24:01: +--------+-------------+--------------------+-------------+-------+
INFO - 16:24:01: *** End StructureScenario execution (time: 0:00:00.012662) ***
INFO - 16:24:01: *** Start PropulsionScenario execution ***
INFO - 16:24:01: PropulsionScenario
INFO - 16:24:01: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:24:01: MDO formulation: MDF
INFO - 16:24:01: Optimization problem:
INFO - 16:24:01: minimize 0.001*-y_4(x_3)
INFO - 16:24:01: with respect to x_3
INFO - 16:24:01: under the inequality constraints
INFO - 16:24:01: g_3(x_3) <= 0
INFO - 16:24:01: over the design space:
INFO - 16:24:01: +------+-------------+--------------------+-------------+-------+
INFO - 16:24:01: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:24:01: +------+-------------+--------------------+-------------+-------+
INFO - 16:24:01: | x_3 | 0.1 | 0.1582651781707329 | 1 | float |
INFO - 16:24:01: +------+-------------+--------------------+-------------+-------+
INFO - 16:24:01: Solving optimization problem with algorithm SLSQP:
INFO - 16:24:01: 2%|▏ | 1/50 [00:00<00:00, 107.02 it/sec, feas=True, obj=-2.25]
INFO - 16:24:01: 4%|▍ | 2/50 [00:00<00:00, 75.90 it/sec, feas=True, obj=-2.25]
INFO - 16:24:01: 6%|▌ | 3/50 [00:00<00:00, 51.19 it/sec, feas=True, obj=-2.25]
INFO - 16:24:01: 8%|▊ | 4/50 [00:00<00:01, 43.41 it/sec, feas=True, obj=-2.25]
INFO - 16:24:01: 10%|█ | 5/50 [00:00<00:01, 39.40 it/sec, feas=True, obj=-2.25]
WARNING - 16:24:01: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 6.724932466608626e-05 is still above the tolerance 1e-06.
INFO - 16:24:01: 12%|█▏ | 6/50 [00:00<00:01, 39.61 it/sec, feas=True, obj=-2.25]
INFO - 16:24:01: Optimization result:
INFO - 16:24:01: Optimizer info:
INFO - 16:24:01: Status: None
INFO - 16:24:01: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:24:01: Solution:
INFO - 16:24:01: The solution is feasible.
INFO - 16:24:01: Objective: -2.2495639254119877
INFO - 16:24:01: Standardized constraints:
INFO - 16:24:01: g_3 = [-8.36427671e-01 -1.63572329e-01 7.40469641e-05 -1.81375311e-01]
INFO - 16:24:01: Design space:
INFO - 16:24:01: +------+-------------+--------------------+-------------+-------+
INFO - 16:24:01: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:24:01: +------+-------------+--------------------+-------------+-------+
INFO - 16:24:01: | x_3 | 0.1 | 0.1582651781707329 | 1 | float |
INFO - 16:24:01: +------+-------------+--------------------+-------------+-------+
INFO - 16:24:01: *** End PropulsionScenario execution (time: 0:00:00.154019) ***
INFO - 16:24:01: 93%|█████████▎| 93/100 [00:45<00:03, 2.06 it/sec, feas=True, obj=-2.25]
INFO - 16:24:02: *** Start PropulsionScenario execution ***
INFO - 16:24:02: PropulsionScenario
INFO - 16:24:02: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:24:02: MDO formulation: MDF
INFO - 16:24:02: Optimization problem:
INFO - 16:24:02: minimize 0.001*-y_4(x_3)
INFO - 16:24:02: with respect to x_3
INFO - 16:24:02: under the inequality constraints
INFO - 16:24:02: g_3(x_3) <= 0
INFO - 16:24:02: over the design space:
INFO - 16:24:02: +------+-------------+--------------------+-------------+-------+
INFO - 16:24:02: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:24:02: +------+-------------+--------------------+-------------+-------+
INFO - 16:24:02: | x_3 | 0.1 | 0.1582651781707329 | 1 | float |
INFO - 16:24:02: +------+-------------+--------------------+-------------+-------+
INFO - 16:24:02: Solving optimization problem with algorithm SLSQP:
WARNING - 16:24:02: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 6.724932466608626e-05 is still above the tolerance 1e-06.
INFO - 16:24:02: 2%|▏ | 1/50 [00:00<00:01, 34.08 it/sec, feas=True, obj=-2.25]
INFO - 16:24:02: 4%|▍ | 2/50 [00:00<00:01, 39.40 it/sec, feas=True, obj=-2.25]
INFO - 16:24:02: 6%|▌ | 3/50 [00:00<00:01, 34.10 it/sec, feas=True, obj=-2.25]
WARNING - 16:24:02: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 6.724932466608626e-05 is still above the tolerance 1e-06.
INFO - 16:24:02: 8%|▊ | 4/50 [00:00<00:01, 29.65 it/sec, feas=True, obj=-2.25]
INFO - 16:24:02: 10%|█ | 5/50 [00:00<00:01, 28.79 it/sec, feas=True, obj=-2.25]
INFO - 16:24:02: 12%|█▏ | 6/50 [00:00<00:01, 30.40 it/sec, feas=True, obj=-2.25]
INFO - 16:24:02: Optimization result:
INFO - 16:24:02: Optimizer info:
INFO - 16:24:02: Status: None
INFO - 16:24:02: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:24:02: Solution:
INFO - 16:24:02: The solution is feasible.
INFO - 16:24:02: Objective: -2.248908362427576
INFO - 16:24:02: Standardized constraints:
INFO - 16:24:02: g_3 = [-8.36374971e-01 -1.63625029e-01 2.28941227e-05 -1.81370874e-01]
INFO - 16:24:02: Design space:
INFO - 16:24:02: +------+-------------+--------------------+-------------+-------+
INFO - 16:24:02: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:24:02: +------+-------------+--------------------+-------------+-------+
INFO - 16:24:02: | x_3 | 0.1 | 0.1582651781707329 | 1 | float |
INFO - 16:24:02: +------+-------------+--------------------+-------------+-------+
INFO - 16:24:02: *** End PropulsionScenario execution (time: 0:00:00.199884) ***
WARNING - 16:24:02: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 6.724932466608626e-05 is still above the tolerance 1e-06.
INFO - 16:24:02: *** Start AerodynamicsScenario execution ***
INFO - 16:24:02: AerodynamicsScenario
INFO - 16:24:02: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:24:02: MDO formulation: MDF
INFO - 16:24:02: Optimization problem:
INFO - 16:24:02: minimize 0.001*-y_4(x_2)
INFO - 16:24:02: with respect to x_2
INFO - 16:24:02: under the inequality constraints
INFO - 16:24:02: g_2(x_2) <= 0
INFO - 16:24:02: over the design space:
INFO - 16:24:02: +------+-------------+-------+-------------+-------+
INFO - 16:24:02: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:24:02: +------+-------------+-------+-------------+-------+
INFO - 16:24:02: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:24:02: +------+-------------+-------+-------------+-------+
INFO - 16:24:02: Solving optimization problem with algorithm SLSQP:
INFO - 16:24:02: 2%|▏ | 1/50 [00:00<00:00, 69.66 it/sec, feas=True, obj=-2.25]
INFO - 16:24:02: Optimization result:
INFO - 16:24:02: Optimizer info:
INFO - 16:24:02: Status: 8
INFO - 16:24:02: Message: Positive directional derivative for linesearch
INFO - 16:24:02: Solution:
INFO - 16:24:02: The solution is feasible.
INFO - 16:24:02: Objective: -2.248908362427576
INFO - 16:24:02: Standardized constraints:
INFO - 16:24:02: g_2 = -5.076487097355198e-08
INFO - 16:24:02: Design space:
INFO - 16:24:02: +------+-------------+-------+-------------+-------+
INFO - 16:24:02: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:24:02: +------+-------------+-------+-------------+-------+
INFO - 16:24:02: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:24:02: +------+-------------+-------+-------------+-------+
INFO - 16:24:02: *** End AerodynamicsScenario execution (time: 0:00:00.016196) ***
INFO - 16:24:02: *** Start StructureScenario execution ***
INFO - 16:24:02: StructureScenario
INFO - 16:24:02: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:24:02: MDO formulation: MDF
INFO - 16:24:02: Optimization problem:
INFO - 16:24:02: minimize 0.001*-y_4(x_1)
INFO - 16:24:02: with respect to x_1
INFO - 16:24:02: under the inequality constraints
INFO - 16:24:02: g_1(x_1) <= 0
INFO - 16:24:02: over the design space:
INFO - 16:24:02: +--------+-------------+--------------------+-------------+-------+
INFO - 16:24:02: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:24:02: +--------+-------------+--------------------+-------------+-------+
INFO - 16:24:02: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:24:02: | x_1[1] | 0.75 | 0.7806436836764827 | 1.25 | float |
INFO - 16:24:02: +--------+-------------+--------------------+-------------+-------+
INFO - 16:24:02: Solving optimization problem with algorithm SLSQP:
WARNING - 16:24:02: MDAGaussSeidel has reached its maximum number of unsuccessful iterations, but the normalized residual norm 0.0009157477359807847 is still above the tolerance 1e-06.
INFO - 16:24:02: 2%|▏ | 1/50 [00:00<00:00, 51.76 it/sec, feas=True, obj=-2.25]
INFO - 16:24:02: Optimization result:
INFO - 16:24:02: Optimizer info:
INFO - 16:24:02: Status: 8
INFO - 16:24:02: Message: Positive directional derivative for linesearch
INFO - 16:24:02: Solution:
INFO - 16:24:02: The solution is feasible.
INFO - 16:24:02: Objective: -2.2489083624275756
INFO - 16:24:02: Standardized constraints:
INFO - 16:24:02: g_1 = [-1.59548910e-03 -2.02846579e-03 -1.31331517e-02 -2.32801865e-02
INFO - 16:24:02: -3.14966361e-02 -2.40000000e-01 1.36557432e-14]
INFO - 16:24:02: Design space:
INFO - 16:24:02: +--------+-------------+--------------------+-------------+-------+
INFO - 16:24:02: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:24:02: +--------+-------------+--------------------+-------------+-------+
INFO - 16:24:02: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:24:02: | x_1[1] | 0.75 | 0.7806436836764827 | 1.25 | float |
INFO - 16:24:02: +--------+-------------+--------------------+-------------+-------+
INFO - 16:24:02: *** End StructureScenario execution (time: 0:00:00.021417) ***
INFO - 16:24:02: *** Start PropulsionScenario execution ***
INFO - 16:24:02: PropulsionScenario
INFO - 16:24:02: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:24:02: MDO formulation: MDF
INFO - 16:24:02: Optimization problem:
INFO - 16:24:02: minimize 0.001*-y_4(x_3)
INFO - 16:24:02: with respect to x_3
INFO - 16:24:02: under the inequality constraints
INFO - 16:24:02: g_3(x_3) <= 0
INFO - 16:24:02: over the design space:
INFO - 16:24:02: +------+-------------+--------------------+-------------+-------+
INFO - 16:24:02: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:24:02: +------+-------------+--------------------+-------------+-------+
INFO - 16:24:02: | x_3 | 0.1 | 0.1582651781707329 | 1 | float |
INFO - 16:24:02: +------+-------------+--------------------+-------------+-------+
INFO - 16:24:02: Solving optimization problem with algorithm SLSQP:
WARNING - 16:24:02: MDAGaussSeidel has reached its maximum number of unsuccessful iterations, but the normalized residual norm 6.724932466608626e-05 is still above the tolerance 1e-06.
INFO - 16:24:02: 2%|▏ | 1/50 [00:00<00:00, 51.75 it/sec, feas=True, obj=-2.25]
INFO - 16:24:02: 4%|▍ | 2/50 [00:00<00:00, 55.93 it/sec, feas=True, obj=-2.25]
INFO - 16:24:02: 6%|▌ | 3/50 [00:00<00:01, 43.74 it/sec, feas=True, obj=-2.25]
WARNING - 16:24:02: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 6.724932466608626e-05 is still above the tolerance 1e-06.
INFO - 16:24:02: 8%|▊ | 4/50 [00:00<00:01, 36.14 it/sec, feas=True, obj=-2.25]
INFO - 16:24:02: 10%|█ | 5/50 [00:00<00:01, 38.85 it/sec, feas=True, obj=-2.25]
INFO - 16:24:02: 12%|█▏ | 6/50 [00:00<00:01, 36.98 it/sec, feas=True, obj=-2.25]
INFO - 16:24:02: Optimization result:
INFO - 16:24:02: Optimizer info:
INFO - 16:24:02: Status: None
INFO - 16:24:02: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:24:02: Solution:
INFO - 16:24:02: The solution is feasible.
INFO - 16:24:02: Objective: -2.248908362427576
INFO - 16:24:02: Standardized constraints:
INFO - 16:24:02: g_3 = [-8.36374971e-01 -1.63625029e-01 2.28941227e-05 -1.81370874e-01]
INFO - 16:24:02: Design space:
INFO - 16:24:02: +------+-------------+--------------------+-------------+-------+
INFO - 16:24:02: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:24:02: +------+-------------+--------------------+-------------+-------+
INFO - 16:24:02: | x_3 | 0.1 | 0.1582651781707329 | 1 | float |
INFO - 16:24:02: +------+-------------+--------------------+-------------+-------+
INFO - 16:24:02: *** End PropulsionScenario execution (time: 0:00:00.164752) ***
WARNING - 16:24:02: MDAGaussSeidel has reached its maximum number of unsuccessful iterations, but the normalized residual norm 6.724932466608626e-05 is still above the tolerance 1e-06.
INFO - 16:24:02: 94%|█████████▍| 94/100 [00:45<00:02, 2.06 it/sec, feas=True, obj=-2.25]
INFO - 16:24:02: *** Start PropulsionScenario execution ***
INFO - 16:24:02: PropulsionScenario
INFO - 16:24:02: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:24:02: MDO formulation: MDF
INFO - 16:24:02: Optimization problem:
INFO - 16:24:02: minimize 0.001*-y_4(x_3)
INFO - 16:24:02: with respect to x_3
INFO - 16:24:02: under the inequality constraints
INFO - 16:24:02: g_3(x_3) <= 0
INFO - 16:24:02: over the design space:
INFO - 16:24:02: +------+-------------+--------------------+-------------+-------+
INFO - 16:24:02: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:24:02: +------+-------------+--------------------+-------------+-------+
INFO - 16:24:02: | x_3 | 0.1 | 0.1582651781707329 | 1 | float |
INFO - 16:24:02: +------+-------------+--------------------+-------------+-------+
INFO - 16:24:02: Solving optimization problem with algorithm SLSQP:
INFO - 16:24:02: 2%|▏ | 1/50 [00:00<00:01, 39.29 it/sec, feas=False, obj=-2.25]
INFO - 16:24:02: 4%|▍ | 2/50 [00:00<00:01, 39.99 it/sec, feas=True, obj=-2.25]
INFO - 16:24:02: 6%|▌ | 3/50 [00:00<00:01, 33.61 it/sec, feas=False, obj=-2.25]
INFO - 16:24:02: 8%|▊ | 4/50 [00:00<00:01, 30.61 it/sec, feas=True, obj=-2.25]
INFO - 16:24:02: 10%|█ | 5/50 [00:00<00:01, 32.04 it/sec, feas=True, obj=-2.25]
INFO - 16:24:02: 12%|█▏ | 6/50 [00:00<00:01, 33.08 it/sec, feas=True, obj=-2.25]
INFO - 16:24:02: Optimization result:
INFO - 16:24:02: Optimizer info:
INFO - 16:24:02: Status: None
INFO - 16:24:02: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:24:02: Solution:
INFO - 16:24:02: The solution is feasible.
INFO - 16:24:02: Objective: -2.2495256018621106
INFO - 16:24:02: Standardized constraints:
INFO - 16:24:02: g_3 = [-8.36562066e-01 -1.63437934e-01 8.88178420e-15 -1.81391809e-01]
INFO - 16:24:02: Design space:
INFO - 16:24:02: +------+-------------+--------------------+-------------+-------+
INFO - 16:24:02: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:24:02: +------+-------------+--------------------+-------------+-------+
INFO - 16:24:02: | x_3 | 0.1 | 0.1582356260488137 | 1 | float |
INFO - 16:24:02: +------+-------------+--------------------+-------------+-------+
INFO - 16:24:02: *** End PropulsionScenario execution (time: 0:00:00.184041) ***
INFO - 16:24:02: *** Start AerodynamicsScenario execution ***
INFO - 16:24:02: AerodynamicsScenario
INFO - 16:24:02: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:24:02: MDO formulation: MDF
INFO - 16:24:02: Optimization problem:
INFO - 16:24:02: minimize 0.001*-y_4(x_2)
INFO - 16:24:02: with respect to x_2
INFO - 16:24:02: under the inequality constraints
INFO - 16:24:02: g_2(x_2) <= 0
INFO - 16:24:02: over the design space:
INFO - 16:24:02: +------+-------------+-------+-------------+-------+
INFO - 16:24:02: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:24:02: +------+-------------+-------+-------------+-------+
INFO - 16:24:02: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:24:02: +------+-------------+-------+-------------+-------+
INFO - 16:24:02: Solving optimization problem with algorithm SLSQP:
INFO - 16:24:02: 2%|▏ | 1/50 [00:00<00:00, 90.00 it/sec, feas=True, obj=-2.25]
INFO - 16:24:02: Optimization result:
INFO - 16:24:02: Optimizer info:
INFO - 16:24:02: Status: 8
INFO - 16:24:02: Message: Positive directional derivative for linesearch
INFO - 16:24:02: Solution:
INFO - 16:24:02: The solution is feasible.
INFO - 16:24:02: Objective: -2.2495256018621106
INFO - 16:24:02: Standardized constraints:
INFO - 16:24:02: g_2 = -6.661338147750939e-16
INFO - 16:24:02: Design space:
INFO - 16:24:02: +------+-------------+-------+-------------+-------+
INFO - 16:24:02: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:24:02: +------+-------------+-------+-------------+-------+
INFO - 16:24:02: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:24:02: +------+-------------+-------+-------------+-------+
INFO - 16:24:02: *** End AerodynamicsScenario execution (time: 0:00:00.012923) ***
INFO - 16:24:02: *** Start StructureScenario execution ***
INFO - 16:24:02: StructureScenario
INFO - 16:24:02: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:24:02: MDO formulation: MDF
INFO - 16:24:02: Optimization problem:
INFO - 16:24:02: minimize 0.001*-y_4(x_1)
INFO - 16:24:02: with respect to x_1
INFO - 16:24:02: under the inequality constraints
INFO - 16:24:02: g_1(x_1) <= 0
INFO - 16:24:02: over the design space:
INFO - 16:24:02: +--------+-------------+--------------------+-------------+-------+
INFO - 16:24:02: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:24:02: +--------+-------------+--------------------+-------------+-------+
INFO - 16:24:02: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:24:02: | x_1[1] | 0.75 | 0.7806436836764827 | 1.25 | float |
INFO - 16:24:02: +--------+-------------+--------------------+-------------+-------+
INFO - 16:24:02: Solving optimization problem with algorithm SLSQP:
INFO - 16:24:02: 2%|▏ | 1/50 [00:00<00:00, 97.33 it/sec, feas=True, obj=-2.25]
INFO - 16:24:02: 4%|▍ | 2/50 [00:00<00:00, 59.90 it/sec, feas=True, obj=-2.25]
INFO - 16:24:02: 6%|▌ | 3/50 [00:00<00:00, 74.53 it/sec, feas=True, obj=-2.25]
INFO - 16:24:02: Optimization result:
INFO - 16:24:02: Optimizer info:
INFO - 16:24:02: Status: None
INFO - 16:24:02: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:24:02: Solution:
INFO - 16:24:02: The solution is feasible.
INFO - 16:24:02: Objective: -2.2495256018621106
INFO - 16:24:02: Standardized constraints:
INFO - 16:24:02: g_1 = [-1.59589593e-03 -2.02868890e-03 -1.31333010e-02 -2.32802973e-02
INFO - 16:24:02: -3.14967236e-02 -2.40000000e-01 1.36557432e-14]
INFO - 16:24:02: Design space:
INFO - 16:24:02: +--------+-------------+--------------------+-------------+-------+
INFO - 16:24:02: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:24:02: +--------+-------------+--------------------+-------------+-------+
INFO - 16:24:02: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:24:02: | x_1[1] | 0.75 | 0.7806436836764827 | 1.25 | float |
INFO - 16:24:02: +--------+-------------+--------------------+-------------+-------+
INFO - 16:24:02: *** End StructureScenario execution (time: 0:00:00.042558) ***
INFO - 16:24:02: *** Start PropulsionScenario execution ***
INFO - 16:24:02: PropulsionScenario
INFO - 16:24:02: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:24:02: MDO formulation: MDF
INFO - 16:24:02: Optimization problem:
INFO - 16:24:02: minimize 0.001*-y_4(x_3)
INFO - 16:24:02: with respect to x_3
INFO - 16:24:02: under the inequality constraints
INFO - 16:24:02: g_3(x_3) <= 0
INFO - 16:24:02: over the design space:
INFO - 16:24:02: +------+-------------+--------------------+-------------+-------+
INFO - 16:24:02: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:24:02: +------+-------------+--------------------+-------------+-------+
INFO - 16:24:02: | x_3 | 0.1 | 0.1582356260488137 | 1 | float |
INFO - 16:24:02: +------+-------------+--------------------+-------------+-------+
INFO - 16:24:02: Solving optimization problem with algorithm SLSQP:
INFO - 16:24:02: 2%|▏ | 1/50 [00:00<00:00, 93.67 it/sec, feas=True, obj=-2.25]
INFO - 16:24:02: Optimization result:
INFO - 16:24:02: Optimizer info:
INFO - 16:24:02: Status: 8
INFO - 16:24:02: Message: Positive directional derivative for linesearch
INFO - 16:24:02: Solution:
INFO - 16:24:02: The solution is feasible.
INFO - 16:24:02: Objective: -2.2495256018621106
INFO - 16:24:02: Standardized constraints:
INFO - 16:24:02: g_3 = [-8.36562066e-01 -1.63437934e-01 8.88178420e-15 -1.81391809e-01]
INFO - 16:24:02: Design space:
INFO - 16:24:02: +------+-------------+--------------------+-------------+-------+
INFO - 16:24:02: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:24:02: +------+-------------+--------------------+-------------+-------+
INFO - 16:24:02: | x_3 | 0.1 | 0.1582356260488137 | 1 | float |
INFO - 16:24:02: +------+-------------+--------------------+-------------+-------+
INFO - 16:24:02: *** End PropulsionScenario execution (time: 0:00:00.012454) ***
INFO - 16:24:02: 95%|█████████▌| 95/100 [00:45<00:02, 2.07 it/sec, feas=True, obj=-2.25]
INFO - 16:24:02: *** Start PropulsionScenario execution ***
INFO - 16:24:02: PropulsionScenario
INFO - 16:24:02: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:24:02: MDO formulation: MDF
INFO - 16:24:02: Optimization problem:
INFO - 16:24:02: minimize 0.001*-y_4(x_3)
INFO - 16:24:02: with respect to x_3
INFO - 16:24:02: under the inequality constraints
INFO - 16:24:02: g_3(x_3) <= 0
INFO - 16:24:02: over the design space:
INFO - 16:24:02: +------+-------------+--------------------+-------------+-------+
INFO - 16:24:02: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:24:02: +------+-------------+--------------------+-------------+-------+
INFO - 16:24:02: | x_3 | 0.1 | 0.1582356260488137 | 1 | float |
INFO - 16:24:02: +------+-------------+--------------------+-------------+-------+
INFO - 16:24:02: Solving optimization problem with algorithm SLSQP:
INFO - 16:24:02: 2%|▏ | 1/50 [00:00<00:01, 40.27 it/sec, feas=True, obj=-2.25]
INFO - 16:24:02: 4%|▍ | 2/50 [00:00<00:01, 30.46 it/sec, feas=True, obj=-2.25]
INFO - 16:24:02: 6%|▌ | 3/50 [00:00<00:01, 27.90 it/sec, feas=True, obj=-2.25]
INFO - 16:24:02: Optimization result:
INFO - 16:24:02: Optimizer info:
INFO - 16:24:02: Status: 8
INFO - 16:24:02: Message: Positive directional derivative for linesearch
INFO - 16:24:02: Solution:
INFO - 16:24:02: The solution is feasible.
INFO - 16:24:02: Objective: -2.2480722331481657
INFO - 16:24:02: Standardized constraints:
INFO - 16:24:02: g_3 = [-8.36360195e-01 -1.63639805e-01 2.22044605e-16 -1.81371504e-01]
INFO - 16:24:02: Design space:
INFO - 16:24:02: +------+-------------+--------------------+-------------+-------+
INFO - 16:24:02: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:24:02: +------+-------------+--------------------+-------------+-------+
INFO - 16:24:02: | x_3 | 0.1 | 0.1582932024799551 | 1 | float |
INFO - 16:24:02: +------+-------------+--------------------+-------------+-------+
INFO - 16:24:02: *** End PropulsionScenario execution (time: 0:00:00.110088) ***
INFO - 16:24:02: *** Start AerodynamicsScenario execution ***
INFO - 16:24:02: AerodynamicsScenario
INFO - 16:24:02: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:24:02: MDO formulation: MDF
INFO - 16:24:02: Optimization problem:
INFO - 16:24:02: minimize 0.001*-y_4(x_2)
INFO - 16:24:02: with respect to x_2
INFO - 16:24:02: under the inequality constraints
INFO - 16:24:02: g_2(x_2) <= 0
INFO - 16:24:02: over the design space:
INFO - 16:24:02: +------+-------------+-------+-------------+-------+
INFO - 16:24:02: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:24:02: +------+-------------+-------+-------------+-------+
INFO - 16:24:02: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:24:02: +------+-------------+-------+-------------+-------+
INFO - 16:24:02: Solving optimization problem with algorithm SLSQP:
INFO - 16:24:02: 2%|▏ | 1/50 [00:00<00:00, 103.87 it/sec, feas=True, obj=-2.25]
INFO - 16:24:02: Optimization result:
INFO - 16:24:02: Optimizer info:
INFO - 16:24:02: Status: 8
INFO - 16:24:02: Message: Positive directional derivative for linesearch
INFO - 16:24:02: Solution:
INFO - 16:24:02: The solution is feasible.
INFO - 16:24:02: Objective: -2.2480722331481657
INFO - 16:24:02: Standardized constraints:
INFO - 16:24:02: g_2 = -1.2769884460972492e-07
INFO - 16:24:02: Design space:
INFO - 16:24:02: +------+-------------+-------+-------------+-------+
INFO - 16:24:02: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:24:02: +------+-------------+-------+-------------+-------+
INFO - 16:24:02: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:24:02: +------+-------------+-------+-------------+-------+
INFO - 16:24:02: *** End AerodynamicsScenario execution (time: 0:00:00.011713) ***
INFO - 16:24:02: *** Start StructureScenario execution ***
INFO - 16:24:02: StructureScenario
INFO - 16:24:02: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:24:02: MDO formulation: MDF
INFO - 16:24:02: Optimization problem:
INFO - 16:24:02: minimize 0.001*-y_4(x_1)
INFO - 16:24:02: with respect to x_1
INFO - 16:24:02: under the inequality constraints
INFO - 16:24:02: g_1(x_1) <= 0
INFO - 16:24:02: over the design space:
INFO - 16:24:02: +--------+-------------+--------------------+-------------+-------+
INFO - 16:24:02: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:24:02: +--------+-------------+--------------------+-------------+-------+
INFO - 16:24:02: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:24:02: | x_1[1] | 0.75 | 0.7806436836764827 | 1.25 | float |
INFO - 16:24:02: +--------+-------------+--------------------+-------------+-------+
INFO - 16:24:02: Solving optimization problem with algorithm SLSQP:
INFO - 16:24:02: 2%|▏ | 1/50 [00:00<00:00, 96.91 it/sec, feas=True, obj=-2.25]
INFO - 16:24:02: Optimization result:
INFO - 16:24:02: Optimizer info:
INFO - 16:24:02: Status: 8
INFO - 16:24:02: Message: Positive directional derivative for linesearch
INFO - 16:24:02: Solution:
INFO - 16:24:02: The solution is feasible.
INFO - 16:24:02: Objective: -2.2480722331481657
INFO - 16:24:02: Standardized constraints:
INFO - 16:24:02: g_1 = [-1.59487257e-03 -2.02812766e-03 -1.31329255e-02 -2.32800187e-02
INFO - 16:24:02: -3.14965035e-02 -2.40000000e-01 1.36557432e-14]
INFO - 16:24:02: Design space:
INFO - 16:24:02: +--------+-------------+--------------------+-------------+-------+
INFO - 16:24:02: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:24:02: +--------+-------------+--------------------+-------------+-------+
INFO - 16:24:02: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:24:02: | x_1[1] | 0.75 | 0.7806436836764827 | 1.25 | float |
INFO - 16:24:02: +--------+-------------+--------------------+-------------+-------+
INFO - 16:24:02: *** End StructureScenario execution (time: 0:00:00.012538) ***
INFO - 16:24:02: *** Start PropulsionScenario execution ***
INFO - 16:24:02: PropulsionScenario
INFO - 16:24:02: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:24:02: MDO formulation: MDF
INFO - 16:24:02: Optimization problem:
INFO - 16:24:02: minimize 0.001*-y_4(x_3)
INFO - 16:24:02: with respect to x_3
INFO - 16:24:02: under the inequality constraints
INFO - 16:24:02: g_3(x_3) <= 0
INFO - 16:24:02: over the design space:
INFO - 16:24:02: +------+-------------+--------------------+-------------+-------+
INFO - 16:24:02: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:24:02: +------+-------------+--------------------+-------------+-------+
INFO - 16:24:02: | x_3 | 0.1 | 0.1582932024799551 | 1 | float |
INFO - 16:24:02: +------+-------------+--------------------+-------------+-------+
INFO - 16:24:02: Solving optimization problem with algorithm SLSQP:
INFO - 16:24:02: 2%|▏ | 1/50 [00:00<00:00, 88.12 it/sec, feas=True, obj=-2.25]
INFO - 16:24:02: Optimization result:
INFO - 16:24:02: Optimizer info:
INFO - 16:24:02: Status: 8
INFO - 16:24:02: Message: Positive directional derivative for linesearch
INFO - 16:24:02: Solution:
INFO - 16:24:02: The solution is feasible.
INFO - 16:24:02: Objective: -2.2480722331481657
INFO - 16:24:02: Standardized constraints:
INFO - 16:24:02: g_3 = [-8.36360195e-01 -1.63639805e-01 2.22044605e-16 -1.81371504e-01]
INFO - 16:24:02: Design space:
INFO - 16:24:02: +------+-------------+--------------------+-------------+-------+
INFO - 16:24:02: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:24:02: +------+-------------+--------------------+-------------+-------+
INFO - 16:24:02: | x_3 | 0.1 | 0.1582932024799551 | 1 | float |
INFO - 16:24:02: +------+-------------+--------------------+-------------+-------+
INFO - 16:24:02: *** End PropulsionScenario execution (time: 0:00:00.013296) ***
INFO - 16:24:02: 96%|█████████▌| 96/100 [00:46<00:01, 2.09 it/sec, feas=True, obj=-2.25]
INFO - 16:24:02: *** Start PropulsionScenario execution ***
INFO - 16:24:02: PropulsionScenario
INFO - 16:24:02: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:24:02: MDO formulation: MDF
INFO - 16:24:02: Optimization problem:
INFO - 16:24:02: minimize 0.001*-y_4(x_3)
INFO - 16:24:02: with respect to x_3
INFO - 16:24:02: under the inequality constraints
INFO - 16:24:02: g_3(x_3) <= 0
INFO - 16:24:02: over the design space:
INFO - 16:24:02: +------+-------------+--------------------+-------------+-------+
INFO - 16:24:02: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:24:02: +------+-------------+--------------------+-------------+-------+
INFO - 16:24:02: | x_3 | 0.1 | 0.1582932024799551 | 1 | float |
INFO - 16:24:02: +------+-------------+--------------------+-------------+-------+
INFO - 16:24:02: Solving optimization problem with algorithm SLSQP:
INFO - 16:24:02: 2%|▏ | 1/50 [00:00<00:01, 40.92 it/sec, feas=False, obj=-2.25]
INFO - 16:24:02: 4%|▍ | 2/50 [00:00<00:01, 41.14 it/sec, feas=True, obj=-2.25]
INFO - 16:24:03: 6%|▌ | 3/50 [00:00<00:01, 33.84 it/sec, feas=False, obj=-2.25]
INFO - 16:24:03: 8%|▊ | 4/50 [00:00<00:01, 31.02 it/sec, feas=True, obj=-2.25]
INFO - 16:24:03: 10%|█ | 5/50 [00:00<00:01, 29.73 it/sec, feas=True, obj=-2.25]
INFO - 16:24:03: 12%|█▏ | 6/50 [00:00<00:01, 28.94 it/sec, feas=True, obj=-2.25]
INFO - 16:24:03: Optimization result:
INFO - 16:24:03: Optimizer info:
INFO - 16:24:03: Status: None
INFO - 16:24:03: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:24:03: Solution:
INFO - 16:24:03: The solution is feasible.
INFO - 16:24:03: Objective: -2.2490580978619104
INFO - 16:24:03: Standardized constraints:
INFO - 16:24:03: g_3 = [-8.36425931e-01 -1.63574069e-01 2.44249065e-15 -1.81387679e-01]
INFO - 16:24:03: Design space:
INFO - 16:24:03: +------+-------------+--------------------+-------------+-------+
INFO - 16:24:03: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:24:03: +------+-------------+--------------------+-------------+-------+
INFO - 16:24:03: | x_3 | 0.1 | 0.1582400906277537 | 1 | float |
INFO - 16:24:03: +------+-------------+--------------------+-------------+-------+
INFO - 16:24:03: *** End PropulsionScenario execution (time: 0:00:00.209759) ***
INFO - 16:24:03: *** Start AerodynamicsScenario execution ***
INFO - 16:24:03: AerodynamicsScenario
INFO - 16:24:03: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:24:03: MDO formulation: MDF
INFO - 16:24:03: Optimization problem:
INFO - 16:24:03: minimize 0.001*-y_4(x_2)
INFO - 16:24:03: with respect to x_2
INFO - 16:24:03: under the inequality constraints
INFO - 16:24:03: g_2(x_2) <= 0
INFO - 16:24:03: over the design space:
INFO - 16:24:03: +------+-------------+-------+-------------+-------+
INFO - 16:24:03: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:24:03: +------+-------------+-------+-------------+-------+
INFO - 16:24:03: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:24:03: +------+-------------+-------+-------------+-------+
INFO - 16:24:03: Solving optimization problem with algorithm SLSQP:
INFO - 16:24:03: 2%|▏ | 1/50 [00:00<00:00, 101.05 it/sec, feas=True, obj=-2.25]
INFO - 16:24:03: Optimization result:
INFO - 16:24:03: Optimizer info:
INFO - 16:24:03: Status: 8
INFO - 16:24:03: Message: Positive directional derivative for linesearch
INFO - 16:24:03: Solution:
INFO - 16:24:03: The solution is feasible.
INFO - 16:24:03: Objective: -2.2490580978619104
INFO - 16:24:03: Standardized constraints:
INFO - 16:24:03: g_2 = 0.0
INFO - 16:24:03: Design space:
INFO - 16:24:03: +------+-------------+-------+-------------+-------+
INFO - 16:24:03: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:24:03: +------+-------------+-------+-------------+-------+
INFO - 16:24:03: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:24:03: +------+-------------+-------+-------------+-------+
INFO - 16:24:03: *** End AerodynamicsScenario execution (time: 0:00:00.011555) ***
INFO - 16:24:03: *** Start StructureScenario execution ***
INFO - 16:24:03: StructureScenario
INFO - 16:24:03: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:24:03: MDO formulation: MDF
INFO - 16:24:03: Optimization problem:
INFO - 16:24:03: minimize 0.001*-y_4(x_1)
INFO - 16:24:03: with respect to x_1
INFO - 16:24:03: under the inequality constraints
INFO - 16:24:03: g_1(x_1) <= 0
INFO - 16:24:03: over the design space:
INFO - 16:24:03: +--------+-------------+--------------------+-------------+-------+
INFO - 16:24:03: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:24:03: +--------+-------------+--------------------+-------------+-------+
INFO - 16:24:03: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:24:03: | x_1[1] | 0.75 | 0.7806436836764827 | 1.25 | float |
INFO - 16:24:03: +--------+-------------+--------------------+-------------+-------+
INFO - 16:24:03: Solving optimization problem with algorithm SLSQP:
INFO - 16:24:03: 2%|▏ | 1/50 [00:00<00:00, 95.90 it/sec, feas=True, obj=-2.25]
INFO - 16:24:03: 4%|▍ | 2/50 [00:00<00:00, 114.13 it/sec, feas=True, obj=-2.25]
INFO - 16:24:03: 6%|▌ | 3/50 [00:00<00:00, 130.09 it/sec, feas=True, obj=-2.25]
INFO - 16:24:03: Optimization result:
INFO - 16:24:03: Optimizer info:
INFO - 16:24:03: Status: None
INFO - 16:24:03: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:24:03: Solution:
INFO - 16:24:03: The solution is feasible.
INFO - 16:24:03: Objective: -2.2490580978619104
INFO - 16:24:03: Standardized constraints:
INFO - 16:24:03: g_1 = [-1.59589593e-03 -2.02868890e-03 -1.31333010e-02 -2.32802973e-02
INFO - 16:24:03: -3.14967236e-02 -2.40000000e-01 1.36557432e-14]
INFO - 16:24:03: Design space:
INFO - 16:24:03: +--------+-------------+--------------------+-------------+-------+
INFO - 16:24:03: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:24:03: +--------+-------------+--------------------+-------------+-------+
INFO - 16:24:03: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:24:03: | x_1[1] | 0.75 | 0.7806436836764827 | 1.25 | float |
INFO - 16:24:03: +--------+-------------+--------------------+-------------+-------+
INFO - 16:24:03: *** End StructureScenario execution (time: 0:00:00.025799) ***
INFO - 16:24:03: *** Start PropulsionScenario execution ***
INFO - 16:24:03: PropulsionScenario
INFO - 16:24:03: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:24:03: MDO formulation: MDF
INFO - 16:24:03: Optimization problem:
INFO - 16:24:03: minimize 0.001*-y_4(x_3)
INFO - 16:24:03: with respect to x_3
INFO - 16:24:03: under the inequality constraints
INFO - 16:24:03: g_3(x_3) <= 0
INFO - 16:24:03: over the design space:
INFO - 16:24:03: +------+-------------+--------------------+-------------+-------+
INFO - 16:24:03: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:24:03: +------+-------------+--------------------+-------------+-------+
INFO - 16:24:03: | x_3 | 0.1 | 0.1582400906277537 | 1 | float |
INFO - 16:24:03: +------+-------------+--------------------+-------------+-------+
INFO - 16:24:03: Solving optimization problem with algorithm SLSQP:
INFO - 16:24:03: 2%|▏ | 1/50 [00:00<00:00, 72.09 it/sec, feas=True, obj=-2.25]
INFO - 16:24:03: Optimization result:
INFO - 16:24:03: Optimizer info:
INFO - 16:24:03: Status: 8
INFO - 16:24:03: Message: Positive directional derivative for linesearch
INFO - 16:24:03: Solution:
INFO - 16:24:03: The solution is feasible.
INFO - 16:24:03: Objective: -2.2490580978619104
INFO - 16:24:03: Standardized constraints:
INFO - 16:24:03: g_3 = [-8.36425931e-01 -1.63574069e-01 2.44249065e-15 -1.81387679e-01]
INFO - 16:24:03: Design space:
INFO - 16:24:03: +------+-------------+--------------------+-------------+-------+
INFO - 16:24:03: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:24:03: +------+-------------+--------------------+-------------+-------+
INFO - 16:24:03: | x_3 | 0.1 | 0.1582400906277537 | 1 | float |
INFO - 16:24:03: +------+-------------+--------------------+-------------+-------+
INFO - 16:24:03: *** End PropulsionScenario execution (time: 0:00:00.015758) ***
INFO - 16:24:03: 97%|█████████▋| 97/100 [00:46<00:01, 2.09 it/sec, feas=True, obj=-2.25]
INFO - 16:24:03: *** Start PropulsionScenario execution ***
INFO - 16:24:03: PropulsionScenario
INFO - 16:24:03: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:24:03: MDO formulation: MDF
INFO - 16:24:03: Optimization problem:
INFO - 16:24:03: minimize 0.001*-y_4(x_3)
INFO - 16:24:03: with respect to x_3
INFO - 16:24:03: under the inequality constraints
INFO - 16:24:03: g_3(x_3) <= 0
INFO - 16:24:03: over the design space:
INFO - 16:24:03: +------+-------------+--------------------+-------------+-------+
INFO - 16:24:03: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:24:03: +------+-------------+--------------------+-------------+-------+
INFO - 16:24:03: | x_3 | 0.1 | 0.1582400906277537 | 1 | float |
INFO - 16:24:03: +------+-------------+--------------------+-------------+-------+
INFO - 16:24:03: Solving optimization problem with algorithm SLSQP:
INFO - 16:24:03: 2%|▏ | 1/50 [00:00<00:01, 42.37 it/sec, feas=True, obj=-2.25]
INFO - 16:24:03: 4%|▍ | 2/50 [00:00<00:01, 32.14 it/sec, feas=True, obj=-2.25]
INFO - 16:24:03: 6%|▌ | 3/50 [00:00<00:01, 29.70 it/sec, feas=True, obj=-2.25]
INFO - 16:24:03: Optimization result:
INFO - 16:24:03: Optimizer info:
INFO - 16:24:03: Status: 8
INFO - 16:24:03: Message: Positive directional derivative for linesearch
INFO - 16:24:03: Solution:
INFO - 16:24:03: The solution is feasible.
INFO - 16:24:03: Objective: -2.2490100980870946
INFO - 16:24:03: Standardized constraints:
INFO - 16:24:03: g_3 = [-8.36410101e-01 -1.63589899e-01 -2.22044605e-16 -1.81379592e-01]
INFO - 16:24:03: Design space:
INFO - 16:24:03: +------+-------------+--------------------+-------------+-------+
INFO - 16:24:03: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:24:03: +------+-------------+--------------------+-------------+-------+
INFO - 16:24:03: | x_3 | 0.1 | 0.1582488320460216 | 1 | float |
INFO - 16:24:03: +------+-------------+--------------------+-------------+-------+
INFO - 16:24:03: *** End PropulsionScenario execution (time: 0:00:00.102988) ***
INFO - 16:24:03: *** Start AerodynamicsScenario execution ***
INFO - 16:24:03: AerodynamicsScenario
INFO - 16:24:03: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:24:03: MDO formulation: MDF
INFO - 16:24:03: Optimization problem:
INFO - 16:24:03: minimize 0.001*-y_4(x_2)
INFO - 16:24:03: with respect to x_2
INFO - 16:24:03: under the inequality constraints
INFO - 16:24:03: g_2(x_2) <= 0
INFO - 16:24:03: over the design space:
INFO - 16:24:03: +------+-------------+-------+-------------+-------+
INFO - 16:24:03: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:24:03: +------+-------------+-------+-------------+-------+
INFO - 16:24:03: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:24:03: +------+-------------+-------+-------------+-------+
INFO - 16:24:03: Solving optimization problem with algorithm SLSQP:
INFO - 16:24:03: 2%|▏ | 1/50 [00:00<00:00, 105.34 it/sec, feas=True, obj=-2.25]
INFO - 16:24:03: Optimization result:
INFO - 16:24:03: Optimizer info:
INFO - 16:24:03: Status: 8
INFO - 16:24:03: Message: Positive directional derivative for linesearch
INFO - 16:24:03: Solution:
INFO - 16:24:03: The solution is feasible.
INFO - 16:24:03: Objective: -2.2490100980870946
INFO - 16:24:03: Standardized constraints:
INFO - 16:24:03: g_2 = 0.0
INFO - 16:24:03: Design space:
INFO - 16:24:03: +------+-------------+-------+-------------+-------+
INFO - 16:24:03: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:24:03: +------+-------------+-------+-------------+-------+
INFO - 16:24:03: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:24:03: +------+-------------+-------+-------------+-------+
INFO - 16:24:03: *** End AerodynamicsScenario execution (time: 0:00:00.011188) ***
INFO - 16:24:03: *** Start StructureScenario execution ***
INFO - 16:24:03: StructureScenario
INFO - 16:24:03: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:24:03: MDO formulation: MDF
INFO - 16:24:03: Optimization problem:
INFO - 16:24:03: minimize 0.001*-y_4(x_1)
INFO - 16:24:03: with respect to x_1
INFO - 16:24:03: under the inequality constraints
INFO - 16:24:03: g_1(x_1) <= 0
INFO - 16:24:03: over the design space:
INFO - 16:24:03: +--------+-------------+--------------------+-------------+-------+
INFO - 16:24:03: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:24:03: +--------+-------------+--------------------+-------------+-------+
INFO - 16:24:03: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:24:03: | x_1[1] | 0.75 | 0.7806436836764827 | 1.25 | float |
INFO - 16:24:03: +--------+-------------+--------------------+-------------+-------+
INFO - 16:24:03: Solving optimization problem with algorithm SLSQP:
INFO - 16:24:03: 2%|▏ | 1/50 [00:00<00:00, 96.21 it/sec, feas=True, obj=-2.25]
INFO - 16:24:03: Optimization result:
INFO - 16:24:03: Optimizer info:
INFO - 16:24:03: Status: 8
INFO - 16:24:03: Message: Positive directional derivative for linesearch
INFO - 16:24:03: Solution:
INFO - 16:24:03: The solution is feasible.
INFO - 16:24:03: Objective: -2.2490100980870946
INFO - 16:24:03: Standardized constraints:
INFO - 16:24:03: g_1 = [-1.59589593e-03 -2.02868890e-03 -1.31333010e-02 -2.32802973e-02
INFO - 16:24:03: -3.14967236e-02 -2.40000000e-01 1.36557432e-14]
INFO - 16:24:03: Design space:
INFO - 16:24:03: +--------+-------------+--------------------+-------------+-------+
INFO - 16:24:03: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:24:03: +--------+-------------+--------------------+-------------+-------+
INFO - 16:24:03: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:24:03: | x_1[1] | 0.75 | 0.7806436836764827 | 1.25 | float |
INFO - 16:24:03: +--------+-------------+--------------------+-------------+-------+
INFO - 16:24:03: *** End StructureScenario execution (time: 0:00:00.012601) ***
INFO - 16:24:03: *** Start PropulsionScenario execution ***
INFO - 16:24:03: PropulsionScenario
INFO - 16:24:03: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:24:03: MDO formulation: MDF
INFO - 16:24:03: Optimization problem:
INFO - 16:24:03: minimize 0.001*-y_4(x_3)
INFO - 16:24:03: with respect to x_3
INFO - 16:24:03: under the inequality constraints
INFO - 16:24:03: g_3(x_3) <= 0
INFO - 16:24:03: over the design space:
INFO - 16:24:03: +------+-------------+--------------------+-------------+-------+
INFO - 16:24:03: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:24:03: +------+-------------+--------------------+-------------+-------+
INFO - 16:24:03: | x_3 | 0.1 | 0.1582488320460216 | 1 | float |
INFO - 16:24:03: +------+-------------+--------------------+-------------+-------+
INFO - 16:24:03: Solving optimization problem with algorithm SLSQP:
INFO - 16:24:03: 2%|▏ | 1/50 [00:00<00:00, 107.49 it/sec, feas=True, obj=-2.25]
INFO - 16:24:03: Optimization result:
INFO - 16:24:03: Optimizer info:
INFO - 16:24:03: Status: 8
INFO - 16:24:03: Message: Positive directional derivative for linesearch
INFO - 16:24:03: Solution:
INFO - 16:24:03: The solution is feasible.
INFO - 16:24:03: Objective: -2.2490100980870946
INFO - 16:24:03: Standardized constraints:
INFO - 16:24:03: g_3 = [-8.36410101e-01 -1.63589899e-01 -2.22044605e-16 -1.81379592e-01]
INFO - 16:24:03: Design space:
INFO - 16:24:03: +------+-------------+--------------------+-------------+-------+
INFO - 16:24:03: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:24:03: +------+-------------+--------------------+-------------+-------+
INFO - 16:24:03: | x_3 | 0.1 | 0.1582488320460216 | 1 | float |
INFO - 16:24:03: +------+-------------+--------------------+-------------+-------+
INFO - 16:24:03: *** End PropulsionScenario execution (time: 0:00:00.011184) ***
INFO - 16:24:03: 98%|█████████▊| 98/100 [00:46<00:00, 2.11 it/sec, feas=True, obj=-2.25]
INFO - 16:24:03: *** Start PropulsionScenario execution ***
INFO - 16:24:03: PropulsionScenario
INFO - 16:24:03: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:24:03: MDO formulation: MDF
INFO - 16:24:03: Optimization problem:
INFO - 16:24:03: minimize 0.001*-y_4(x_3)
INFO - 16:24:03: with respect to x_3
INFO - 16:24:03: under the inequality constraints
INFO - 16:24:03: g_3(x_3) <= 0
INFO - 16:24:03: over the design space:
INFO - 16:24:03: +------+-------------+--------------------+-------------+-------+
INFO - 16:24:03: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:24:03: +------+-------------+--------------------+-------------+-------+
INFO - 16:24:03: | x_3 | 0.1 | 0.1582488320460216 | 1 | float |
INFO - 16:24:03: +------+-------------+--------------------+-------------+-------+
INFO - 16:24:03: Solving optimization problem with algorithm SLSQP:
INFO - 16:24:03: 2%|▏ | 1/50 [00:00<00:01, 42.75 it/sec, feas=True, obj=-2.25]
INFO - 16:24:03: 4%|▍ | 2/50 [00:00<00:01, 32.46 it/sec, feas=True, obj=-2.25]
INFO - 16:24:03: Optimization result:
INFO - 16:24:03: Optimizer info:
INFO - 16:24:03: Status: 8
INFO - 16:24:03: Message: Positive directional derivative for linesearch
INFO - 16:24:03: Solution:
INFO - 16:24:03: The solution is feasible.
INFO - 16:24:03: Objective: -2.2488224917254263
INFO - 16:24:03: Standardized constraints:
INFO - 16:24:03: g_3 = [-8.36444795e-01 -1.63555205e-01 5.99520433e-15 -1.81371504e-01]
INFO - 16:24:03: Design space:
INFO - 16:24:03: +------+-------------+--------------------+-------------+-------+
INFO - 16:24:03: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:24:03: +------+-------------+--------------------+-------------+-------+
INFO - 16:24:03: | x_3 | 0.1 | 0.1582576074177016 | 1 | float |
INFO - 16:24:03: +------+-------------+--------------------+-------------+-------+
INFO - 16:24:03: *** End PropulsionScenario execution (time: 0:00:00.063707) ***
INFO - 16:24:03: *** Start AerodynamicsScenario execution ***
INFO - 16:24:03: AerodynamicsScenario
INFO - 16:24:03: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:24:03: MDO formulation: MDF
INFO - 16:24:03: Optimization problem:
INFO - 16:24:03: minimize 0.001*-y_4(x_2)
INFO - 16:24:03: with respect to x_2
INFO - 16:24:03: under the inequality constraints
INFO - 16:24:03: g_2(x_2) <= 0
INFO - 16:24:03: over the design space:
INFO - 16:24:03: +------+-------------+-------+-------------+-------+
INFO - 16:24:03: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:24:03: +------+-------------+-------+-------------+-------+
INFO - 16:24:03: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:24:03: +------+-------------+-------+-------------+-------+
INFO - 16:24:03: Solving optimization problem with algorithm SLSQP:
INFO - 16:24:03: 2%|▏ | 1/50 [00:00<00:00, 104.15 it/sec, feas=True, obj=-2.25]
INFO - 16:24:03: Optimization result:
INFO - 16:24:03: Optimizer info:
INFO - 16:24:03: Status: 8
INFO - 16:24:03: Message: Positive directional derivative for linesearch
INFO - 16:24:03: Solution:
INFO - 16:24:03: The solution is feasible.
INFO - 16:24:03: Objective: -2.2488224917254263
INFO - 16:24:03: Standardized constraints:
INFO - 16:24:03: g_2 = -3.654386013818289e-05
INFO - 16:24:03: Design space:
INFO - 16:24:03: +------+-------------+-------+-------------+-------+
INFO - 16:24:03: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:24:03: +------+-------------+-------+-------------+-------+
INFO - 16:24:03: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:24:03: +------+-------------+-------+-------------+-------+
INFO - 16:24:03: *** End AerodynamicsScenario execution (time: 0:00:00.011277) ***
INFO - 16:24:03: *** Start StructureScenario execution ***
INFO - 16:24:03: StructureScenario
INFO - 16:24:03: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:24:03: MDO formulation: MDF
INFO - 16:24:03: Optimization problem:
INFO - 16:24:03: minimize 0.001*-y_4(x_1)
INFO - 16:24:03: with respect to x_1
INFO - 16:24:03: under the inequality constraints
INFO - 16:24:03: g_1(x_1) <= 0
INFO - 16:24:03: over the design space:
INFO - 16:24:03: +--------+-------------+--------------------+-------------+-------+
INFO - 16:24:03: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:24:03: +--------+-------------+--------------------+-------------+-------+
INFO - 16:24:03: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:24:03: | x_1[1] | 0.75 | 0.7806436836764827 | 1.25 | float |
INFO - 16:24:03: +--------+-------------+--------------------+-------------+-------+
INFO - 16:24:03: Solving optimization problem with algorithm SLSQP:
INFO - 16:24:03: 2%|▏ | 1/50 [00:00<00:00, 97.70 it/sec, feas=True, obj=-2.25]
INFO - 16:24:03: 4%|▍ | 2/50 [00:00<00:00, 62.52 it/sec, feas=True, obj=-2.25]
INFO - 16:24:03: 6%|▌ | 3/50 [00:00<00:00, 76.08 it/sec, feas=True, obj=-2.25]
INFO - 16:24:03: Optimization result:
INFO - 16:24:03: Optimizer info:
INFO - 16:24:03: Status: None
INFO - 16:24:03: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:24:03: Solution:
INFO - 16:24:03: The solution is feasible.
INFO - 16:24:03: Objective: -2.2488224917254263
INFO - 16:24:03: Standardized constraints:
INFO - 16:24:03: g_1 = [-1.30308064e-03 -1.86809556e-03 -1.30258373e-02 -2.32005574e-02
INFO - 16:24:03: -3.14337353e-02 -2.40000000e-01 1.36557432e-14]
INFO - 16:24:03: Design space:
INFO - 16:24:03: +--------+-------------+--------------------+-------------+-------+
INFO - 16:24:03: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:24:03: +--------+-------------+--------------------+-------------+-------+
INFO - 16:24:03: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:24:03: | x_1[1] | 0.75 | 0.7806436836764827 | 1.25 | float |
INFO - 16:24:03: +--------+-------------+--------------------+-------------+-------+
INFO - 16:24:03: *** End StructureScenario execution (time: 0:00:00.041703) ***
INFO - 16:24:03: *** Start PropulsionScenario execution ***
INFO - 16:24:03: PropulsionScenario
INFO - 16:24:03: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:24:03: MDO formulation: MDF
INFO - 16:24:03: Optimization problem:
INFO - 16:24:03: minimize 0.001*-y_4(x_3)
INFO - 16:24:03: with respect to x_3
INFO - 16:24:03: under the inequality constraints
INFO - 16:24:03: g_3(x_3) <= 0
INFO - 16:24:03: over the design space:
INFO - 16:24:03: +------+-------------+--------------------+-------------+-------+
INFO - 16:24:03: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:24:03: +------+-------------+--------------------+-------------+-------+
INFO - 16:24:03: | x_3 | 0.1 | 0.1582576074177016 | 1 | float |
INFO - 16:24:03: +------+-------------+--------------------+-------------+-------+
INFO - 16:24:03: Solving optimization problem with algorithm SLSQP:
INFO - 16:24:03: 2%|▏ | 1/50 [00:00<00:00, 93.77 it/sec, feas=True, obj=-2.25]
INFO - 16:24:03: Optimization result:
INFO - 16:24:03: Optimizer info:
INFO - 16:24:03: Status: 8
INFO - 16:24:03: Message: Positive directional derivative for linesearch
INFO - 16:24:03: Solution:
INFO - 16:24:03: The solution is feasible.
INFO - 16:24:03: Objective: -2.2488224917254263
INFO - 16:24:03: Standardized constraints:
INFO - 16:24:03: g_3 = [-8.36444795e-01 -1.63555205e-01 5.99520433e-15 -1.81371504e-01]
INFO - 16:24:03: Design space:
INFO - 16:24:03: +------+-------------+--------------------+-------------+-------+
INFO - 16:24:03: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:24:03: +------+-------------+--------------------+-------------+-------+
INFO - 16:24:03: | x_3 | 0.1 | 0.1582576074177016 | 1 | float |
INFO - 16:24:03: +------+-------------+--------------------+-------------+-------+
INFO - 16:24:03: *** End PropulsionScenario execution (time: 0:00:00.012440) ***
INFO - 16:24:03: 99%|█████████▉| 99/100 [00:46<00:00, 2.12 it/sec, feas=True, obj=-2.25]
INFO - 16:24:03: *** Start PropulsionScenario execution ***
INFO - 16:24:03: PropulsionScenario
INFO - 16:24:03: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:24:03: MDO formulation: MDF
INFO - 16:24:03: Optimization problem:
INFO - 16:24:03: minimize 0.001*-y_4(x_3)
INFO - 16:24:03: with respect to x_3
INFO - 16:24:03: under the inequality constraints
INFO - 16:24:03: g_3(x_3) <= 0
INFO - 16:24:03: over the design space:
INFO - 16:24:03: +------+-------------+--------------------+-------------+-------+
INFO - 16:24:03: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:24:03: +------+-------------+--------------------+-------------+-------+
INFO - 16:24:03: | x_3 | 0.1 | 0.1582576074177016 | 1 | float |
INFO - 16:24:03: +------+-------------+--------------------+-------------+-------+
INFO - 16:24:03: Solving optimization problem with algorithm SLSQP:
INFO - 16:24:03: 2%|▏ | 1/50 [00:00<00:01, 41.65 it/sec, feas=True, obj=-2.25]
INFO - 16:24:03: 4%|▍ | 2/50 [00:00<00:01, 43.81 it/sec, feas=True, obj=-2.25]
WARNING - 16:24:03: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 6.724932466608626e-05 is still above the tolerance 1e-06.
INFO - 16:24:03: 6%|▌ | 3/50 [00:00<00:01, 32.05 it/sec, feas=True, obj=-2.25]
INFO - 16:24:03: 8%|▊ | 4/50 [00:00<00:01, 30.12 it/sec, feas=True, obj=-2.25]
INFO - 16:24:03: Optimization result:
INFO - 16:24:03: Optimizer info:
INFO - 16:24:03: Status: 8
INFO - 16:24:03: Message: Positive directional derivative for linesearch
INFO - 16:24:03: Solution:
INFO - 16:24:03: The solution is feasible.
INFO - 16:24:03: Objective: -2.249221595016689
INFO - 16:24:03: Standardized constraints:
INFO - 16:24:03: g_3 = [-8.36494188e-01 -1.63505812e-01 4.03660121e-05 -1.81377383e-01]
INFO - 16:24:03: Design space:
INFO - 16:24:03: +------+-------------+--------------------+-------------+-------+
INFO - 16:24:03: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:24:03: +------+-------------+--------------------+-------------+-------+
INFO - 16:24:03: | x_3 | 0.1 | 0.1582576074177016 | 1 | float |
INFO - 16:24:03: +------+-------------+--------------------+-------------+-------+
INFO - 16:24:03: *** End PropulsionScenario execution (time: 0:00:00.134756) ***
INFO - 16:24:03: *** Start AerodynamicsScenario execution ***
INFO - 16:24:03: AerodynamicsScenario
INFO - 16:24:03: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:24:03: MDO formulation: MDF
INFO - 16:24:03: Optimization problem:
INFO - 16:24:03: minimize 0.001*-y_4(x_2)
INFO - 16:24:03: with respect to x_2
INFO - 16:24:03: under the inequality constraints
INFO - 16:24:03: g_2(x_2) <= 0
INFO - 16:24:03: over the design space:
INFO - 16:24:03: +------+-------------+-------+-------------+-------+
INFO - 16:24:03: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:24:03: +------+-------------+-------+-------------+-------+
INFO - 16:24:03: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:24:03: +------+-------------+-------+-------------+-------+
INFO - 16:24:03: Solving optimization problem with algorithm SLSQP:
INFO - 16:24:03: 2%|▏ | 1/50 [00:00<00:00, 90.52 it/sec, feas=True, obj=-2.25]
INFO - 16:24:03: Optimization result:
INFO - 16:24:03: Optimizer info:
INFO - 16:24:03: Status: 8
INFO - 16:24:03: Message: Positive directional derivative for linesearch
INFO - 16:24:03: Solution:
INFO - 16:24:03: The solution is feasible.
INFO - 16:24:03: Objective: -2.249221595016689
INFO - 16:24:03: Standardized constraints:
INFO - 16:24:03: g_2 = 0.0
INFO - 16:24:03: Design space:
INFO - 16:24:03: +------+-------------+-------+-------------+-------+
INFO - 16:24:03: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:24:03: +------+-------------+-------+-------------+-------+
INFO - 16:24:03: | x_2 | 0.75 | 0.75 | 1.25 | float |
INFO - 16:24:03: +------+-------------+-------+-------------+-------+
INFO - 16:24:03: *** End AerodynamicsScenario execution (time: 0:00:00.012834) ***
INFO - 16:24:03: *** Start StructureScenario execution ***
INFO - 16:24:03: StructureScenario
INFO - 16:24:03: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:24:03: MDO formulation: MDF
INFO - 16:24:03: Optimization problem:
INFO - 16:24:03: minimize 0.001*-y_4(x_1)
INFO - 16:24:03: with respect to x_1
INFO - 16:24:03: under the inequality constraints
INFO - 16:24:03: g_1(x_1) <= 0
INFO - 16:24:03: over the design space:
INFO - 16:24:03: +--------+-------------+--------------------+-------------+-------+
INFO - 16:24:03: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:24:03: +--------+-------------+--------------------+-------------+-------+
INFO - 16:24:03: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:24:03: | x_1[1] | 0.75 | 0.7806436836764827 | 1.25 | float |
INFO - 16:24:03: +--------+-------------+--------------------+-------------+-------+
INFO - 16:24:03: Solving optimization problem with algorithm SLSQP:
INFO - 16:24:03: 2%|▏ | 1/50 [00:00<00:00, 97.17 it/sec, feas=True, obj=-2.25]
INFO - 16:24:03: 4%|▍ | 2/50 [00:00<00:00, 117.15 it/sec, feas=True, obj=-2.25]
INFO - 16:24:03: 6%|▌ | 3/50 [00:00<00:00, 124.13 it/sec, feas=True, obj=-2.25]
INFO - 16:24:03: Optimization result:
INFO - 16:24:03: Optimizer info:
INFO - 16:24:03: Status: None
INFO - 16:24:03: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO stopped the driver.
INFO - 16:24:03: Solution:
INFO - 16:24:03: The solution is feasible.
INFO - 16:24:03: Objective: -2.249221595016689
INFO - 16:24:03: Standardized constraints:
INFO - 16:24:03: g_1 = [-1.59589593e-03 -2.02868890e-03 -1.31333010e-02 -2.32802973e-02
INFO - 16:24:03: -3.14967236e-02 -2.40000000e-01 1.36557432e-14]
INFO - 16:24:03: Design space:
INFO - 16:24:03: +--------+-------------+--------------------+-------------+-------+
INFO - 16:24:03: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:24:03: +--------+-------------+--------------------+-------------+-------+
INFO - 16:24:03: | x_1[0] | 0.1 | 0.1 | 0.4 | float |
INFO - 16:24:03: | x_1[1] | 0.75 | 0.7806436836764827 | 1.25 | float |
INFO - 16:24:03: +--------+-------------+--------------------+-------------+-------+
INFO - 16:24:03: *** End StructureScenario execution (time: 0:00:00.026669) ***
INFO - 16:24:03: *** Start PropulsionScenario execution ***
INFO - 16:24:03: PropulsionScenario
INFO - 16:24:03: Disciplines: SobieskiAerodynamics SobieskiMission SobieskiPropulsion SobieskiStructure
INFO - 16:24:03: MDO formulation: MDF
INFO - 16:24:03: Optimization problem:
INFO - 16:24:03: minimize 0.001*-y_4(x_3)
INFO - 16:24:03: with respect to x_3
INFO - 16:24:03: under the inequality constraints
INFO - 16:24:03: g_3(x_3) <= 0
INFO - 16:24:03: over the design space:
INFO - 16:24:03: +------+-------------+--------------------+-------------+-------+
INFO - 16:24:03: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:24:03: +------+-------------+--------------------+-------------+-------+
INFO - 16:24:03: | x_3 | 0.1 | 0.1582576074177016 | 1 | float |
INFO - 16:24:03: +------+-------------+--------------------+-------------+-------+
INFO - 16:24:03: Solving optimization problem with algorithm SLSQP:
INFO - 16:24:03: 2%|▏ | 1/50 [00:00<00:00, 92.40 it/sec, feas=True, obj=-2.25]
INFO - 16:24:03: 4%|▍ | 2/50 [00:00<00:00, 67.26 it/sec, feas=True, obj=-2.25]
WARNING - 16:24:03: MDAGaussSeidel has reached its maximum number of iterations, but the normalized residual norm 6.724932466608626e-05 is still above the tolerance 1e-06.
INFO - 16:24:03: 6%|▌ | 3/50 [00:00<00:01, 42.78 it/sec, feas=True, obj=-2.25]
INFO - 16:24:03: 8%|▊ | 4/50 [00:00<00:01, 38.56 it/sec, feas=True, obj=-2.25]
INFO - 16:24:03: Optimization result:
INFO - 16:24:03: Optimizer info:
INFO - 16:24:03: Status: 8
INFO - 16:24:03: Message: Positive directional derivative for linesearch
INFO - 16:24:03: Solution:
INFO - 16:24:03: The solution is feasible.
INFO - 16:24:03: Objective: -2.249221595016689
INFO - 16:24:03: Standardized constraints:
INFO - 16:24:03: g_3 = [-8.36494188e-01 -1.63505812e-01 4.03660121e-05 -1.81377383e-01]
INFO - 16:24:03: Design space:
INFO - 16:24:03: +------+-------------+--------------------+-------------+-------+
INFO - 16:24:03: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:24:03: +------+-------------+--------------------+-------------+-------+
INFO - 16:24:03: | x_3 | 0.1 | 0.1582576074177016 | 1 | float |
INFO - 16:24:03: +------+-------------+--------------------+-------------+-------+
INFO - 16:24:03: *** End PropulsionScenario execution (time: 0:00:00.105680) ***
INFO - 16:24:03: 100%|██████████| 100/100 [00:46<00:00, 2.13 it/sec, feas=True, obj=-2.25]
INFO - 16:24:03: Optimization result:
INFO - 16:24:03: Optimizer info:
INFO - 16:24:03: Status: None
INFO - 16:24:03: Message: Maximum number of iterations reached. GEMSEO stopped the driver.
INFO - 16:24:03: Solution:
INFO - 16:24:03: The solution is feasible.
INFO - 16:24:03: Objective: -2.306618792686065
INFO - 16:24:03: Standardized constraints:
INFO - 16:24:03: g_1 = [-1.59589593e-03 -2.02868890e-03 -1.31333010e-02 -2.32802973e-02
INFO - 16:24:03: -3.14967236e-02 -2.40000000e-01 1.36557432e-14]
INFO - 16:24:03: g_2 = 0.0
INFO - 16:24:03: g_3 = [-8.36190321e-01 -1.63809679e-01 7.99360578e-15 -1.82740552e-01]
INFO - 16:24:03: Design space:
INFO - 16:24:03: +-------------+-------------+---------------------+-------------+-------+
INFO - 16:24:03: | Name | Lower bound | Value | Upper bound | Type |
INFO - 16:24:03: +-------------+-------------+---------------------+-------------+-------+
INFO - 16:24:03: | x_shared[0] | 0.01 | 0.05999999999999998 | 0.09 | float |
INFO - 16:24:03: | x_shared[1] | 30000 | 60000 | 60000 | float |
INFO - 16:24:03: | x_shared[2] | 1.4 | 1.403944527703097 | 1.8 | float |
INFO - 16:24:03: | x_shared[3] | 2.5 | 6.487676433158127 | 8.5 | float |
INFO - 16:24:03: | x_shared[4] | 40 | 70 | 70 | float |
INFO - 16:24:03: | x_shared[5] | 500 | 1355.325596479095 | 1500 | float |
INFO - 16:24:03: +-------------+-------------+---------------------+-------------+-------+
INFO - 16:24:03: *** End MDOScenario execution (time: 0:00:46.991108) ***
Plot the history of the MDA residuals#
For the first MDA:
system_scenario.formulation.mda1.plot_residual_history(save=False, show=True)
For the second MDA:
system_scenario.formulation.mda2.plot_residual_history(save=False, show=True)
For the BCD MDA:
system_scenario.formulation.bcd_mda.plot_residual_history(save=False, show=True)
<Figure size 640x480 with 1 Axes>
Plot the system optimization history view#
system_scenario.post_process(post_name="OptHistoryView", save=False, show=True)
<gemseo.post.opt_history_view.OptHistoryView object at 0x72a4d89f1a90>
Plot the structure optimization histories of the 2 first iterations#
struct_databases = system_scenario.formulation.scenario_adapters[2].databases
for database in struct_databases[:2]:
opt_problem = deepcopy(structure_sc.formulation.optimization_problem)
opt_problem.database = database
execute_post(opt_problem, post_name="OptHistoryView", save=False, show=True)
Print execution metrics on disciplines and sub-scenarios#
for disc in [propulsion_disc, aerodynamics_disc, mission_disc, structure_disc]:
print(f"{disc.name}: {disc.execution_statistics.n_executions} calls.")
for sub_sc in [propulsion_sc, aerodynamics_sc, structure_sc]:
print(f"{sub_sc.name}: {sub_sc.execution_statistics.n_executions} calls.")
configuration.enable_discipline_statistics = False
SobieskiPropulsion: 17119 calls.
SobieskiAerodynamics: 19646 calls.
SobieskiMission: 17343 calls.
SobieskiStructure: 20153 calls.
PropulsionScenario: 218 calls.
AerodynamicsScenario: 189 calls.
StructureScenario: 177 calls.
Total running time of the script: (0 minutes 49.027 seconds)