Note
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MDO formulations for a toy example in aerostructure¶
from __future__ import annotations
from copy import deepcopy
from gemseo.api import configure_logger
from gemseo.api import create_discipline
from gemseo.api import create_scenario
from gemseo.api import generate_n2_plot
from gemseo.problems.aerostructure.aerostructure_design_space import (
AerostructureDesignSpace,
)
configure_logger()
algo_options = {
"xtol_rel": 1e-8,
"xtol_abs": 1e-8,
"ftol_rel": 1e-8,
"ftol_abs": 1e-8,
"ineq_tolerance": 1e-5,
"eq_tolerance": 1e-3,
}
Create discipline¶
First, we create disciplines (aero, structure, mission) with dummy formulas
using the AnalyticDiscipline class.
aero_formulas = {
"drag": "0.1*((sweep/360)**2 + 200 + "
+ "thick_airfoils**2-thick_airfoils -4*displ)",
"forces": "10*sweep + 0.2*thick_airfoils-0.2*displ",
"lift": "(sweep + 0.2*thick_airfoils-2.*displ)/3000.",
}
aerodynamics = create_discipline(
"AnalyticDiscipline", name="Aerodynamics", expressions=aero_formulas
)
struc_formulas = {
"mass": "4000*(sweep/360)**3 + 200000 + " + "100*thick_panels +200.0*forces",
"reserve_fact": "-3*sweep " + "-6*thick_panels+0.1*forces+55",
"displ": "2*sweep + 3*thick_panels-2.*forces",
}
structure = create_discipline(
"AnalyticDiscipline", name="Structure", expressions=struc_formulas
)
mission_formulas = {"range": "8e11*lift/(mass*drag)"}
mission = create_discipline(
"AnalyticDiscipline", name="Mission", expressions=mission_formulas
)
disciplines = [aerodynamics, structure, mission]
We can see that structure and aerodynamics are strongly coupled:
generate_n2_plot(disciplines, save=False, show=True)
Create an MDO scenario with MDF formulation¶
Then, we create an MDO scenario based on the MDF formulation
design_space = AerostructureDesignSpace()
scenario = create_scenario(
disciplines=disciplines,
formulation="MDF",
objective_name="range",
design_space=design_space,
maximize_objective=True,
)
scenario.add_constraint("reserve_fact", "ineq", value=0.5)
scenario.add_constraint("lift", "eq", value=0.5)
scenario.execute({"algo": "NLOPT_SLSQP", "max_iter": 10, "algo_options": algo_options})
scenario.post_process("OptHistoryView", save=False, show=True)
/home/docs/checkouts/readthedocs.org/user_builds/gemseo/envs/4.2.0/lib/python3.9/site-packages/gemseo/algos/design_space.py:459: ComplexWarning: Casting complex values to real discards the imaginary part
self.__current_value[name] = array_value.astype(
INFO - 17:24:57: Variable reserve_fact was removed from the Design Space, it is not an input of any discipline.
INFO - 17:24:57:
INFO - 17:24:57: *** Start MDOScenario execution ***
INFO - 17:24:57: MDOScenario
INFO - 17:24:57: Disciplines: Aerodynamics Mission Structure
INFO - 17:24:57: MDO formulation: MDF
INFO - 17:24:57: Optimization problem:
INFO - 17:24:57: minimize -range(thick_airfoils, thick_panels, sweep)
INFO - 17:24:57: with respect to sweep, thick_airfoils, thick_panels
INFO - 17:24:57: subject to constraints:
INFO - 17:24:57: reserve_fact(thick_airfoils, thick_panels, sweep) <= 0.5
INFO - 17:24:57: lift(thick_airfoils, thick_panels, sweep) == 0.5
INFO - 17:24:57: over the design space:
INFO - 17:24:57: +----------------+-------------+-------+-------------+-------+
INFO - 17:24:57: | name | lower_bound | value | upper_bound | type |
INFO - 17:24:57: +----------------+-------------+-------+-------------+-------+
INFO - 17:24:57: | thick_airfoils | 5 | 15 | 25 | float |
INFO - 17:24:57: | thick_panels | 1 | 3 | 20 | float |
INFO - 17:24:57: | sweep | 10 | 25 | 35 | float |
INFO - 17:24:57: +----------------+-------------+-------+-------------+-------+
INFO - 17:24:57: Solving optimization problem with algorithm NLOPT_SLSQP:
INFO - 17:24:57: ... 0%| | 0/10 [00:00<?, ?it]
INFO - 17:24:58: ... 10%|█ | 1/10 [00:00<00:00, 18.62 it/sec, obj=-4.25e+3]
INFO - 17:24:58: ... 20%|██ | 2/10 [00:00<00:00, 9.16 it/sec, obj=-4.51e+3]
ERROR - 17:24:58: NLopt run failed: NLopt roundoff-limited, RoundoffLimited
INFO - 17:24:58: ... 30%|███ | 3/10 [00:00<00:00, 13.31 it/sec, obj=-4.51e+3]
INFO - 17:24:58: Optimization result:
INFO - 17:24:58: Optimizer info:
INFO - 17:24:58: Status: None
INFO - 17:24:58: Message: GEMSEO Stopped the driver
INFO - 17:24:58: Number of calls to the objective function by the optimizer: 4
INFO - 17:24:58: Solution:
INFO - 17:24:58: The solution is feasible.
INFO - 17:24:58: Objective: -4509.505446938985
INFO - 17:24:58: Standardized constraints:
INFO - 17:24:58: lift - 0.5 = 1.4988010832439613e-14
INFO - 17:24:58: reserve_fact - 0.5 = 1.1013668199666427e-08
INFO - 17:24:58: Design space:
INFO - 17:24:58: +----------------+-------------+-------------------+-------------+-------+
INFO - 17:24:58: | name | lower_bound | value | upper_bound | type |
INFO - 17:24:58: +----------------+-------------+-------------------+-------------+-------+
INFO - 17:24:58: | thick_airfoils | 5 | 5 | 25 | float |
INFO - 17:24:58: | thick_panels | 1 | 3.225589223849015 | 20 | float |
INFO - 17:24:58: | sweep | 10 | 24.99326599298144 | 35 | float |
INFO - 17:24:58: +----------------+-------------+-------------------+-------------+-------+
INFO - 17:24:58: *** End MDOScenario execution (time: 0:00:00.248354) ***
<gemseo.post.opt_history_view.OptHistoryView object at 0x7fcce87f7100>
Create an MDO scenario with bilevel formulation¶
Then, we create an MDO scenario based on the bilevel formulation
sub_scenario_options = {
"max_iter": 5,
"algo": "NLOPT_SLSQP",
"algo_options": algo_options,
}
design_space_ref = AerostructureDesignSpace()
/home/docs/checkouts/readthedocs.org/user_builds/gemseo/envs/4.2.0/lib/python3.9/site-packages/gemseo/algos/design_space.py:459: ComplexWarning: Casting complex values to real discards the imaginary part
self.__current_value[name] = array_value.astype(
Create the aeronautics sub-scenario¶
For this purpose, we create a first sub-scenario to maximize the range with respect to the thick airfoils, based on the aerodynamics discipline.
design_space_aero = deepcopy(design_space_ref).filter(["thick_airfoils"])
aero_scenario = create_scenario(
disciplines=[aerodynamics, mission],
formulation="DisciplinaryOpt",
objective_name="range",
design_space=design_space_aero,
maximize_objective=True,
)
aero_scenario.default_inputs = sub_scenario_options
Create the structure sub-scenario¶
We create a second sub-scenario to maximize the range with respect to the thick panels, based on the structure discipline.
design_space_struct = deepcopy(design_space_ref).filter(["thick_panels"])
struct_scenario = create_scenario(
disciplines=[structure, mission],
formulation="DisciplinaryOpt",
objective_name="range",
design_space=design_space_struct,
maximize_objective=True,
)
struct_scenario.default_inputs = sub_scenario_options
Create the system scenario¶
Lastly, we build a system scenario to maximize the range with respect to the sweep, which is a shared variable, based on the previous sub-scenarios.
design_space_system = deepcopy(design_space_ref).filter(["sweep"])
system_scenario = create_scenario(
disciplines=[aero_scenario, struct_scenario, mission],
formulation="BiLevel",
objective_name="range",
design_space=design_space_system,
maximize_objective=True,
inner_mda_name="MDAJacobi",
tolerance=1e-8,
)
system_scenario.add_constraint("reserve_fact", "ineq", value=0.5)
system_scenario.add_constraint("lift", "eq", value=0.5)
system_scenario.execute(
{"algo": "NLOPT_COBYLA", "max_iter": 7, "algo_options": algo_options}
)
system_scenario.post_process("OptHistoryView", save=False, show=True)
INFO - 17:25:00:
INFO - 17:25:00: *** Start MDOScenario execution ***
INFO - 17:25:00: MDOScenario
INFO - 17:25:00: Disciplines: MDOScenario MDOScenario Mission
INFO - 17:25:00: MDO formulation: BiLevel
INFO - 17:25:00: Optimization problem:
INFO - 17:25:00: minimize -range(sweep)
INFO - 17:25:00: with respect to sweep
INFO - 17:25:00: subject to constraints:
INFO - 17:25:00: reserve_fact(sweep) <= 0.5
INFO - 17:25:00: lift(sweep) == 0.5
INFO - 17:25:00: over the design space:
INFO - 17:25:00: +-------+-------------+-------+-------------+-------+
INFO - 17:25:00: | name | lower_bound | value | upper_bound | type |
INFO - 17:25:00: +-------+-------------+-------+-------------+-------+
INFO - 17:25:00: | sweep | 10 | 25 | 35 | float |
INFO - 17:25:00: +-------+-------------+-------+-------------+-------+
INFO - 17:25:00: Solving optimization problem with algorithm NLOPT_COBYLA:
INFO - 17:25:00: ... 0%| | 0/7 [00:00<?, ?it]
INFO - 17:25:00:
INFO - 17:25:00: *** Start MDOScenario execution ***
INFO - 17:25:00: MDOScenario
INFO - 17:25:00: Disciplines: Aerodynamics Mission
INFO - 17:25:00: MDO formulation: DisciplinaryOpt
INFO - 17:25:00: Optimization problem:
INFO - 17:25:00: minimize -range(thick_airfoils)
INFO - 17:25:00: with respect to thick_airfoils
INFO - 17:25:00: subject to constraints:
INFO - 17:25:00: lift(thick_airfoils) == 0.5
INFO - 17:25:00: over the design space:
INFO - 17:25:00: +----------------+-------------+-------+-------------+-------+
INFO - 17:25:00: | name | lower_bound | value | upper_bound | type |
INFO - 17:25:00: +----------------+-------------+-------+-------------+-------+
INFO - 17:25:00: | thick_airfoils | 5 | 15 | 25 | float |
INFO - 17:25:00: +----------------+-------------+-------+-------------+-------+
INFO - 17:25:00: Solving optimization problem with algorithm NLOPT_SLSQP:
INFO - 17:25:00: ... 0%| | 0/5 [00:00<?, ?it]
INFO - 17:25:00:
INFO - 17:25:00: ... 20%|██ | 1/5 [00:00<00:00, 115.60 it/sec, obj=-4.25e+3]
INFO - 17:25:00:
WARNING - 17:25:00: Optimization found no feasible point ! The least infeasible point is selected.
INFO - 17:25:00: ... 40%|████ | 2/5 [00:00<00:00, 94.91 it/sec, obj=-4.5e+3]
INFO - 17:25:00:
INFO - 17:25:00:
INFO - 17:25:00: Optimization result:
INFO - 17:25:00: Optimizer info:
INFO - 17:25:00: Status: 5
INFO - 17:25:00: Message: NLOPT_MAXEVAL_REACHED: Optimization stopped because maxeval (above) was reached
INFO - 17:25:00: Number of calls to the objective function by the optimizer: 8
INFO - 17:25:00: Solution:
WARNING - 17:25:00: The solution is not feasible.
INFO - 17:25:00: Objective: -4500.62486797491
INFO - 17:25:00: Standardized constraints:
INFO - 17:25:00: lift - 0.5 = 0.005333333333333634
INFO - 17:25:00: Design space:
INFO - 17:25:00: +----------------+-------------+-------+-------------+-------+
INFO - 17:25:00: | name | lower_bound | value | upper_bound | type |
INFO - 17:25:00: +----------------+-------------+-------+-------------+-------+
INFO - 17:25:00: | thick_airfoils | 5 | 5 | 25 | float |
INFO - 17:25:00: +----------------+-------------+-------+-------------+-------+
INFO - 17:25:00: *** End MDOScenario execution (time: 0:00:00.042018) ***
INFO - 17:25:00:
INFO - 17:25:00: *** Start MDOScenario execution ***
INFO - 17:25:00: MDOScenario
INFO - 17:25:00: Disciplines: Mission Structure
INFO - 17:25:00: MDO formulation: DisciplinaryOpt
INFO - 17:25:00: Optimization problem:
INFO - 17:25:00: minimize -range(thick_panels)
INFO - 17:25:00: with respect to thick_panels
INFO - 17:25:00: subject to constraints:
INFO - 17:25:00: reserve_fact(thick_panels) <= 0.5
INFO - 17:25:00: over the design space:
INFO - 17:25:00: +--------------+-------------+-------+-------------+-------+
INFO - 17:25:00: | name | lower_bound | value | upper_bound | type |
INFO - 17:25:00: +--------------+-------------+-------+-------------+-------+
INFO - 17:25:00: | thick_panels | 1 | 3 | 20 | float |
INFO - 17:25:00: +--------------+-------------+-------+-------------+-------+
INFO - 17:25:00: Solving optimization problem with algorithm NLOPT_SLSQP:
INFO - 17:25:00: ... 0%| | 0/5 [00:00<?, ?it]
INFO - 17:25:00:
INFO - 17:25:00: ... 20%|██ | 1/5 [00:00<00:00, 106.18 it/sec, obj=-4.51e+3]
INFO - 17:25:00:
INFO - 17:25:00: ... 40%|████ | 2/5 [00:00<00:00, 86.49 it/sec, obj=-4.51e+3]
INFO - 17:25:00:
INFO - 17:25:00: ... 60%|██████ | 3/5 [00:00<00:00, 102.91 it/sec, obj=-4.51e+3]
INFO - 17:25:00:
INFO - 17:25:00: ... 80%|████████ | 4/5 [00:00<00:00, 134.43 it/sec, obj=-4.51e+3]
INFO - 17:25:00:
INFO - 17:25:00:
INFO - 17:25:00: Optimization result:
INFO - 17:25:00: Optimizer info:
INFO - 17:25:00: Status: None
INFO - 17:25:00: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO Stopped the driver
INFO - 17:25:00: Number of calls to the objective function by the optimizer: 5
INFO - 17:25:00: Solution:
INFO - 17:25:00: The solution is feasible.
INFO - 17:25:00: Objective: -4506.645473559042
INFO - 17:25:00: Standardized constraints:
INFO - 17:25:00: reserve_fact - 0.5 = 4.75033345992415e-10
INFO - 17:25:00: Design space:
INFO - 17:25:00: +--------------+-------------+-------------------+-------------+-------+
INFO - 17:25:00: | name | lower_bound | value | upper_bound | type |
INFO - 17:25:00: +--------------+-------------+-------------------+-------------+-------+
INFO - 17:25:00: | thick_panels | 1 | 3.249999999920828 | 20 | float |
INFO - 17:25:00: +--------------+-------------+-------------------+-------------+-------+
INFO - 17:25:00: *** End MDOScenario execution (time: 0:00:00.051144) ***
INFO - 17:25:00: ... 14%|█▍ | 1/7 [00:00<00:01, 4.90 it/sec, obj=-4.51e+3]
INFO - 17:25:00:
INFO - 17:25:00: *** Start MDOScenario execution ***
INFO - 17:25:00: MDOScenario
INFO - 17:25:00: Disciplines: Aerodynamics Mission
INFO - 17:25:00: MDO formulation: DisciplinaryOpt
INFO - 17:25:00: Optimization problem:
INFO - 17:25:00: minimize -range(thick_airfoils)
INFO - 17:25:00: with respect to thick_airfoils
INFO - 17:25:00: subject to constraints:
INFO - 17:25:00: lift(thick_airfoils) == 0.5
INFO - 17:25:00: over the design space:
INFO - 17:25:00: +----------------+-------------+-------+-------------+-------+
INFO - 17:25:00: | name | lower_bound | value | upper_bound | type |
INFO - 17:25:00: +----------------+-------------+-------+-------------+-------+
INFO - 17:25:00: | thick_airfoils | 5 | 5 | 25 | float |
INFO - 17:25:00: +----------------+-------------+-------+-------------+-------+
INFO - 17:25:00: Solving optimization problem with algorithm NLOPT_SLSQP:
INFO - 17:25:00: ... 0%| | 0/5 [00:00<?, ?it]
INFO - 17:25:00:
INFO - 17:25:00: ... 20%|██ | 1/5 [00:00<00:00, 464.49 it/sec, obj=-4.27e+3]
INFO - 17:25:00:
WARNING - 17:25:00: Optimization found no feasible point ! The least infeasible point is selected.
INFO - 17:25:00:
INFO - 17:25:00: Optimization result:
INFO - 17:25:00: Optimizer info:
INFO - 17:25:00: Status: 5
INFO - 17:25:00: Message: NLOPT_MAXEVAL_REACHED: Optimization stopped because maxeval (above) was reached
INFO - 17:25:00: Number of calls to the objective function by the optimizer: 8
INFO - 17:25:00: Solution:
WARNING - 17:25:00: The solution is not feasible.
INFO - 17:25:00: Objective: -4267.901616337772
INFO - 17:25:00: Standardized constraints:
INFO - 17:25:00: lift - 0.5 = 0.12713888888915292
INFO - 17:25:00: Design space:
INFO - 17:25:00: +----------------+-------------+-------+-------------+-------+
INFO - 17:25:00: | name | lower_bound | value | upper_bound | type |
INFO - 17:25:00: +----------------+-------------+-------+-------------+-------+
INFO - 17:25:00: | thick_airfoils | 5 | 5 | 25 | float |
INFO - 17:25:00: +----------------+-------------+-------+-------------+-------+
INFO - 17:25:00: *** End MDOScenario execution (time: 0:00:00.014007) ***
INFO - 17:25:00:
INFO - 17:25:00: *** Start MDOScenario execution ***
INFO - 17:25:00: MDOScenario
INFO - 17:25:00: Disciplines: Mission Structure
INFO - 17:25:00: MDO formulation: DisciplinaryOpt
INFO - 17:25:00: Optimization problem:
INFO - 17:25:00: minimize -range(thick_panels)
INFO - 17:25:00: with respect to thick_panels
INFO - 17:25:00: subject to constraints:
INFO - 17:25:00: reserve_fact(thick_panels) <= 0.5
INFO - 17:25:00: over the design space:
INFO - 17:25:00: +--------------+-------------+-------------------+-------------+-------+
INFO - 17:25:00: | name | lower_bound | value | upper_bound | type |
INFO - 17:25:00: +--------------+-------------+-------------------+-------------+-------+
INFO - 17:25:00: | thick_panels | 1 | 3.249999999920828 | 20 | float |
INFO - 17:25:00: +--------------+-------------+-------------------+-------------+-------+
INFO - 17:25:00: Solving optimization problem with algorithm NLOPT_SLSQP:
INFO - 17:25:00: ... 0%| | 0/5 [00:00<?, ?it]
INFO - 17:25:00:
INFO - 17:25:00: ... 20%|██ | 1/5 [00:00<00:00, 599.87 it/sec, obj=-4.27e+3]
INFO - 17:25:00:
ERROR - 17:25:00: NLopt run failed: NLopt roundoff-limited, RoundoffLimited
INFO - 17:25:00: ... 40%|████ | 2/5 [00:00<00:00, 167.45 it/sec, obj=-4.27e+3]
INFO - 17:25:00:
INFO - 17:25:00:
INFO - 17:25:00: Optimization result:
INFO - 17:25:00: Optimizer info:
INFO - 17:25:00: Status: None
INFO - 17:25:00: Message: GEMSEO Stopped the driver
INFO - 17:25:00: Number of calls to the objective function by the optimizer: 3
INFO - 17:25:00: Solution:
INFO - 17:25:00: The solution is feasible.
INFO - 17:25:00: Objective: -4270.014801163224
INFO - 17:25:00: Standardized constraints:
INFO - 17:25:00: reserve_fact - 0.5 = 1.3178436120142578e-10
INFO - 17:25:00: Design space:
INFO - 17:25:00: +--------------+-------------+-------------------+-------------+-------+
INFO - 17:25:00: | name | lower_bound | value | upper_bound | type |
INFO - 17:25:00: +--------------+-------------+-------------------+-------------+-------+
INFO - 17:25:00: | thick_panels | 1 | 1.765277777757134 | 20 | float |
INFO - 17:25:00: +--------------+-------------+-------------------+-------------+-------+
INFO - 17:25:00: *** End MDOScenario execution (time: 0:00:00.017599) ***
INFO - 17:25:00: ... 29%|██▊ | 2/7 [00:00<00:00, 7.56 it/sec, obj=-4.27e+3]
INFO - 17:25:00:
INFO - 17:25:00: *** Start MDOScenario execution ***
INFO - 17:25:00: MDOScenario
INFO - 17:25:00: Disciplines: Aerodynamics Mission
INFO - 17:25:00: MDO formulation: DisciplinaryOpt
INFO - 17:25:00: Optimization problem:
INFO - 17:25:00: minimize -range(thick_airfoils)
INFO - 17:25:00: with respect to thick_airfoils
INFO - 17:25:00: subject to constraints:
INFO - 17:25:00: lift(thick_airfoils) == 0.5
INFO - 17:25:00: over the design space:
INFO - 17:25:00: +----------------+-------------+-------+-------------+-------+
INFO - 17:25:00: | name | lower_bound | value | upper_bound | type |
INFO - 17:25:00: +----------------+-------------+-------+-------------+-------+
INFO - 17:25:00: | thick_airfoils | 5 | 5 | 25 | float |
INFO - 17:25:00: +----------------+-------------+-------+-------------+-------+
INFO - 17:25:00: Solving optimization problem with algorithm NLOPT_SLSQP:
INFO - 17:25:00: ... 0%| | 0/5 [00:00<?, ?it]
INFO - 17:25:00:
INFO - 17:25:00: ... 20%|██ | 1/5 [00:00<00:00, 475.98 it/sec, obj=-4.53e+3]
INFO - 17:25:00:
INFO - 17:25:00: ... 40%|████ | 2/5 [00:00<00:00, 147.90 it/sec, obj=-3.83e+3]
INFO - 17:25:00:
INFO - 17:25:00: ... 60%|██████ | 3/5 [00:00<00:00, 212.29 it/sec, obj=-4.43e+3]
INFO - 17:25:00:
INFO - 17:25:00: ... 80%|████████ | 4/5 [00:00<00:00, 228.31 it/sec, obj=-4.5e+3]
INFO - 17:25:00:
INFO - 17:25:00: ... 100%|██████████| 5/5 [00:00<00:00, 237.24 it/sec, obj=-4.51e+3]
INFO - 17:25:00:
WARNING - 17:25:00: Optimization found no feasible point ! The least infeasible point is selected.
INFO - 17:25:00:
INFO - 17:25:00: Optimization result:
INFO - 17:25:00: Optimizer info:
INFO - 17:25:00: Status: None
INFO - 17:25:00: Message: Maximum number of iterations reached. GEMSEO Stopped the driver
INFO - 17:25:00: Number of calls to the objective function by the optimizer: 7
INFO - 17:25:00: Solution:
WARNING - 17:25:00: The solution is not feasible.
INFO - 17:25:00: Objective: -3831.8061828212526
INFO - 17:25:00: Standardized constraints:
INFO - 17:25:00: lift - 0.5 = -0.0023383323939722422
INFO - 17:25:00: Design space:
INFO - 17:25:00: +----------------+-------------+-------+-------------+-------+
INFO - 17:25:00: | name | lower_bound | value | upper_bound | type |
INFO - 17:25:00: +----------------+-------------+-------+-------------+-------+
INFO - 17:25:00: | thick_airfoils | 5 | 25 | 25 | float |
INFO - 17:25:00: +----------------+-------------+-------+-------------+-------+
INFO - 17:25:00: *** End MDOScenario execution (time: 0:00:00.028899) ***
INFO - 17:25:00:
INFO - 17:25:00: *** Start MDOScenario execution ***
INFO - 17:25:00: MDOScenario
INFO - 17:25:00: Disciplines: Mission Structure
INFO - 17:25:00: MDO formulation: DisciplinaryOpt
INFO - 17:25:00: Optimization problem:
INFO - 17:25:00: minimize -range(thick_panels)
INFO - 17:25:00: with respect to thick_panels
INFO - 17:25:00: subject to constraints:
INFO - 17:25:00: reserve_fact(thick_panels) <= 0.5
INFO - 17:25:00: over the design space:
INFO - 17:25:00: +--------------+-------------+-------------------+-------------+-------+
INFO - 17:25:00: | name | lower_bound | value | upper_bound | type |
INFO - 17:25:00: +--------------+-------------+-------------------+-------------+-------+
INFO - 17:25:00: | thick_panels | 1 | 1.765277777757134 | 20 | float |
INFO - 17:25:00: +--------------+-------------+-------------------+-------------+-------+
INFO - 17:25:00: Solving optimization problem with algorithm NLOPT_SLSQP:
INFO - 17:25:00: ... 0%| | 0/5 [00:00<?, ?it]
INFO - 17:25:00:
INFO - 17:25:00: ... 20%|██ | 1/5 [00:00<00:00, 452.51 it/sec, obj=-3.82e+3]
INFO - 17:25:00:
INFO - 17:25:00: ... 40%|████ | 2/5 [00:00<00:00, 133.23 it/sec, obj=-3.82e+3]
INFO - 17:25:00:
INFO - 17:25:00: ... 60%|██████ | 3/5 [00:00<00:00, 136.39 it/sec, obj=-3.82e+3]
INFO - 17:25:00:
INFO - 17:25:00: ... 80%|████████ | 4/5 [00:00<00:00, 172.62 it/sec, obj=Not evaluated]
INFO - 17:25:00:
INFO - 17:25:00:
INFO - 17:25:00: Optimization result:
INFO - 17:25:00: Optimizer info:
INFO - 17:25:00: Status: None
INFO - 17:25:00: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO Stopped the driver
INFO - 17:25:00: Number of calls to the objective function by the optimizer: 4
INFO - 17:25:00: Solution:
INFO - 17:25:00: The solution is feasible.
INFO - 17:25:00: Objective: -3818.589637887225
INFO - 17:25:00: Standardized constraints:
INFO - 17:25:00: reserve_fact - 0.5 = -1.0631850955178379e-10
INFO - 17:25:00: Design space:
INFO - 17:25:00: +--------------+-------------+-------------------+-------------+-------+
INFO - 17:25:00: | name | lower_bound | value | upper_bound | type |
INFO - 17:25:00: +--------------+-------------+-------------------+-------------+-------+
INFO - 17:25:00: | thick_panels | 1 | 3.414587193246589 | 20 | float |
INFO - 17:25:00: +--------------+-------------+-------------------+-------------+-------+
INFO - 17:25:00: *** End MDOScenario execution (time: 0:00:00.028840) ***
INFO - 17:25:00: ... 43%|████▎ | 3/7 [00:00<00:00, 8.42 it/sec, obj=-3.82e+3]
INFO - 17:25:00:
INFO - 17:25:00: *** Start MDOScenario execution ***
INFO - 17:25:00: MDOScenario
INFO - 17:25:00: Disciplines: Aerodynamics Mission
INFO - 17:25:00: MDO formulation: DisciplinaryOpt
INFO - 17:25:00: Optimization problem:
INFO - 17:25:00: minimize -range(thick_airfoils)
INFO - 17:25:00: with respect to thick_airfoils
INFO - 17:25:00: subject to constraints:
INFO - 17:25:00: lift(thick_airfoils) == 0.5
INFO - 17:25:00: over the design space:
INFO - 17:25:00: +----------------+-------------+-------+-------------+-------+
INFO - 17:25:00: | name | lower_bound | value | upper_bound | type |
INFO - 17:25:00: +----------------+-------------+-------+-------------+-------+
INFO - 17:25:00: | thick_airfoils | 5 | 25 | 25 | float |
INFO - 17:25:00: +----------------+-------------+-------+-------------+-------+
INFO - 17:25:00: Solving optimization problem with algorithm NLOPT_SLSQP:
INFO - 17:25:00: ... 0%| | 0/5 [00:00<?, ?it]
INFO - 17:25:00:
INFO - 17:25:00: ... 20%|██ | 1/5 [00:00<00:00, 497.54 it/sec, obj=-3.82e+3]
INFO - 17:25:00:
WARNING - 17:25:00: Optimization found no feasible point ! The least infeasible point is selected.
INFO - 17:25:00: ... 40%|████ | 2/5 [00:00<00:00, 148.17 it/sec, obj=-4.49e+3]
INFO - 17:25:00:
INFO - 17:25:00:
INFO - 17:25:00: Optimization result:
INFO - 17:25:00: Optimizer info:
INFO - 17:25:00: Status: 5
INFO - 17:25:00: Message: NLOPT_MAXEVAL_REACHED: Optimization stopped because maxeval (above) was reached
INFO - 17:25:00: Number of calls to the objective function by the optimizer: 8
INFO - 17:25:00: Solution:
WARNING - 17:25:00: The solution is not feasible.
INFO - 17:25:00: Objective: -4490.540174198762
INFO - 17:25:00: Standardized constraints:
INFO - 17:25:00: lift - 0.5 = 0.009181047336995207
INFO - 17:25:00: Design space:
INFO - 17:25:00: +----------------+-------------+-------+-------------+-------+
INFO - 17:25:00: | name | lower_bound | value | upper_bound | type |
INFO - 17:25:00: +----------------+-------------+-------+-------------+-------+
INFO - 17:25:00: | thick_airfoils | 5 | 5 | 25 | float |
INFO - 17:25:00: +----------------+-------------+-------+-------------+-------+
INFO - 17:25:00: *** End MDOScenario execution (time: 0:00:00.019407) ***
INFO - 17:25:00:
INFO - 17:25:00: *** Start MDOScenario execution ***
INFO - 17:25:00: MDOScenario
INFO - 17:25:00: Disciplines: Mission Structure
INFO - 17:25:00: MDO formulation: DisciplinaryOpt
INFO - 17:25:00: Optimization problem:
INFO - 17:25:00: minimize -range(thick_panels)
INFO - 17:25:00: with respect to thick_panels
INFO - 17:25:00: subject to constraints:
INFO - 17:25:00: reserve_fact(thick_panels) <= 0.5
INFO - 17:25:00: over the design space:
INFO - 17:25:00: +--------------+-------------+-------------------+-------------+-------+
INFO - 17:25:00: | name | lower_bound | value | upper_bound | type |
INFO - 17:25:00: +--------------+-------------+-------------------+-------------+-------+
INFO - 17:25:00: | thick_panels | 1 | 3.414587193246589 | 20 | float |
INFO - 17:25:00: +--------------+-------------+-------------------+-------------+-------+
INFO - 17:25:00: Solving optimization problem with algorithm NLOPT_SLSQP:
INFO - 17:25:00: ... 0%| | 0/5 [00:00<?, ?it]
INFO - 17:25:00:
INFO - 17:25:00: ... 20%|██ | 1/5 [00:00<00:00, 444.55 it/sec, obj=-4.5e+3]
INFO - 17:25:00:
INFO - 17:25:00: ... 40%|████ | 2/5 [00:00<00:00, 132.33 it/sec, obj=-4.5e+3]
INFO - 17:25:00:
INFO - 17:25:00: ... 60%|██████ | 3/5 [00:00<00:00, 142.00 it/sec, obj=-4.5e+3]
INFO - 17:25:00:
INFO - 17:25:00: ... 80%|████████ | 4/5 [00:00<00:00, 184.53 it/sec, obj=-4.5e+3]
INFO - 17:25:00:
INFO - 17:25:00:
INFO - 17:25:00: Optimization result:
INFO - 17:25:00: Optimizer info:
INFO - 17:25:00: Status: None
INFO - 17:25:00: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO Stopped the driver
INFO - 17:25:00: Number of calls to the objective function by the optimizer: 5
INFO - 17:25:00: Solution:
INFO - 17:25:00: The solution is feasible.
INFO - 17:25:00: Objective: -4503.594568762557
INFO - 17:25:00: Standardized constraints:
INFO - 17:25:00: reserve_fact - 0.5 = 4.5724135588898207e-10
INFO - 17:25:00: Design space:
INFO - 17:25:00: +--------------+-------------+-------------------+-------------+-------+
INFO - 17:25:00: | name | lower_bound | value | upper_bound | type |
INFO - 17:25:00: +--------------+-------------+-------------------+-------------+-------+
INFO - 17:25:00: | thick_panels | 1 | 3.256301635443915 | 20 | float |
INFO - 17:25:00: +--------------+-------------+-------------------+-------------+-------+
INFO - 17:25:00: *** End MDOScenario execution (time: 0:00:00.028204) ***
INFO - 17:25:00: ... 57%|█████▋ | 4/7 [00:00<00:00, 9.17 it/sec, obj=-4.51e+3]
INFO - 17:25:00:
INFO - 17:25:00: *** Start MDOScenario execution ***
INFO - 17:25:00: MDOScenario
INFO - 17:25:00: Disciplines: Aerodynamics Mission
INFO - 17:25:00: MDO formulation: DisciplinaryOpt
INFO - 17:25:00: Optimization problem:
INFO - 17:25:00: minimize -range(thick_airfoils)
INFO - 17:25:00: with respect to thick_airfoils
INFO - 17:25:00: subject to constraints:
INFO - 17:25:00: lift(thick_airfoils) == 0.5
INFO - 17:25:00: over the design space:
INFO - 17:25:00: +----------------+-------------+-------+-------------+-------+
INFO - 17:25:00: | name | lower_bound | value | upper_bound | type |
INFO - 17:25:00: +----------------+-------------+-------+-------------+-------+
INFO - 17:25:00: | thick_airfoils | 5 | 5 | 25 | float |
INFO - 17:25:00: +----------------+-------------+-------+-------------+-------+
INFO - 17:25:00: Solving optimization problem with algorithm NLOPT_SLSQP:
INFO - 17:25:00: ... 0%| | 0/5 [00:00<?, ?it]
INFO - 17:25:00:
INFO - 17:25:00: ... 20%|██ | 1/5 [00:00<00:00, 488.39 it/sec, obj=-4.51e+3]
INFO - 17:25:00:
INFO - 17:25:00: ... 40%|████ | 2/5 [00:00<00:00, 144.75 it/sec, obj=-3.85e+3]
INFO - 17:25:00:
INFO - 17:25:00: ... 60%|██████ | 3/5 [00:00<00:00, 208.55 it/sec, obj=-4.48e+3]
INFO - 17:25:00:
INFO - 17:25:00: ... 80%|████████ | 4/5 [00:00<00:00, 214.33 it/sec, obj=-4.51e+3]
INFO - 17:25:00:
INFO - 17:25:00: ... 100%|██████████| 5/5 [00:00<00:00, 219.27 it/sec, obj=-4.51e+3]
INFO - 17:25:00:
INFO - 17:25:00:
INFO - 17:25:00: Optimization result:
INFO - 17:25:00: Optimizer info:
INFO - 17:25:00: Status: None
INFO - 17:25:00: Message: Maximum number of iterations reached. GEMSEO Stopped the driver
INFO - 17:25:00: Number of calls to the objective function by the optimizer: 7
INFO - 17:25:00: Solution:
INFO - 17:25:00: The solution is feasible.
INFO - 17:25:00: Objective: -3854.0818034962194
INFO - 17:25:00: Standardized constraints:
INFO - 17:25:00: lift - 0.5 = 0.0
INFO - 17:25:00: Design space:
INFO - 17:25:00: +----------------+-------------+-------------------+-------------+-------+
INFO - 17:25:00: | name | lower_bound | value | upper_bound | type |
INFO - 17:25:00: +----------------+-------------+-------------------+-------------+-------+
INFO - 17:25:00: | thick_airfoils | 5 | 24.35677419032555 | 25 | float |
INFO - 17:25:00: +----------------+-------------+-------------------+-------------+-------+
INFO - 17:25:00: *** End MDOScenario execution (time: 0:00:00.033071) ***
INFO - 17:25:00:
INFO - 17:25:00: *** Start MDOScenario execution ***
INFO - 17:25:00: MDOScenario
INFO - 17:25:00: Disciplines: Mission Structure
INFO - 17:25:00: MDO formulation: DisciplinaryOpt
INFO - 17:25:00: Optimization problem:
INFO - 17:25:00: minimize -range(thick_panels)
INFO - 17:25:00: with respect to thick_panels
INFO - 17:25:00: subject to constraints:
INFO - 17:25:00: reserve_fact(thick_panels) <= 0.5
INFO - 17:25:00: over the design space:
INFO - 17:25:00: +--------------+-------------+-------------------+-------------+-------+
INFO - 17:25:00: | name | lower_bound | value | upper_bound | type |
INFO - 17:25:00: +--------------+-------------+-------------------+-------------+-------+
INFO - 17:25:00: | thick_panels | 1 | 3.256301635443915 | 20 | float |
INFO - 17:25:00: +--------------+-------------+-------------------+-------------+-------+
INFO - 17:25:00: Solving optimization problem with algorithm NLOPT_SLSQP:
INFO - 17:25:00: ... 0%| | 0/5 [00:00<?, ?it]
INFO - 17:25:00:
INFO - 17:25:00: ... 20%|██ | 1/5 [00:00<00:00, 451.49 it/sec, obj=-3.84e+3]
INFO - 17:25:00:
INFO - 17:25:00: ... 40%|████ | 2/5 [00:00<00:00, 131.57 it/sec, obj=-3.84e+3]
INFO - 17:25:00:
INFO - 17:25:00: ... 60%|██████ | 3/5 [00:00<00:00, 135.11 it/sec, obj=-3.84e+3]
INFO - 17:25:00:
INFO - 17:25:00: ... 80%|████████ | 4/5 [00:00<00:00, 170.91 it/sec, obj=Not evaluated]
INFO - 17:25:00:
INFO - 17:25:00:
INFO - 17:25:00: Optimization result:
INFO - 17:25:00: Optimizer info:
INFO - 17:25:00: Status: None
INFO - 17:25:00: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO Stopped the driver
INFO - 17:25:00: Number of calls to the objective function by the optimizer: 4
INFO - 17:25:00: Solution:
INFO - 17:25:00: The solution is feasible.
INFO - 17:25:00: Objective: -3843.3818346286994
INFO - 17:25:00: Standardized constraints:
INFO - 17:25:00: reserve_fact - 0.5 = -1.0020073659688933e-10
INFO - 17:25:00: Design space:
INFO - 17:25:00: +--------------+-------------+-------------------+-------------+-------+
INFO - 17:25:00: | name | lower_bound | value | upper_bound | type |
INFO - 17:25:00: +--------------+-------------+-------------------+-------------+-------+
INFO - 17:25:00: | thick_panels | 1 | 3.303233602238194 | 20 | float |
INFO - 17:25:00: +--------------+-------------+-------------------+-------------+-------+
INFO - 17:25:00: *** End MDOScenario execution (time: 0:00:00.029409) ***
INFO - 17:25:00: ... 71%|███████▏ | 5/7 [00:00<00:00, 9.37 it/sec, obj=-3.85e+3]
INFO - 17:25:00:
INFO - 17:25:00: *** Start MDOScenario execution ***
INFO - 17:25:00: MDOScenario
INFO - 17:25:00: Disciplines: Aerodynamics Mission
INFO - 17:25:00: MDO formulation: DisciplinaryOpt
INFO - 17:25:00: Optimization problem:
INFO - 17:25:00: minimize -range(thick_airfoils)
INFO - 17:25:00: with respect to thick_airfoils
INFO - 17:25:00: subject to constraints:
INFO - 17:25:00: lift(thick_airfoils) == 0.5
INFO - 17:25:00: over the design space:
INFO - 17:25:00: +----------------+-------------+-------------------+-------------+-------+
INFO - 17:25:00: | name | lower_bound | value | upper_bound | type |
INFO - 17:25:00: +----------------+-------------+-------------------+-------------+-------+
INFO - 17:25:00: | thick_airfoils | 5 | 24.35677419032555 | 25 | float |
INFO - 17:25:00: +----------------+-------------+-------------------+-------------+-------+
INFO - 17:25:00: Solving optimization problem with algorithm NLOPT_SLSQP:
INFO - 17:25:00: ... 0%| | 0/5 [00:00<?, ?it]
INFO - 17:25:00:
INFO - 17:25:00: ... 20%|██ | 1/5 [00:00<00:00, 456.90 it/sec, obj=-3.85e+3]
INFO - 17:25:00:
WARNING - 17:25:00: Optimization found no feasible point ! The least infeasible point is selected.
INFO - 17:25:00: ... 40%|████ | 2/5 [00:00<00:00, 147.56 it/sec, obj=-4.49e+3]
INFO - 17:25:00:
INFO - 17:25:00:
INFO - 17:25:00: Optimization result:
INFO - 17:25:00: Optimizer info:
INFO - 17:25:00: Status: 5
INFO - 17:25:00: Message: NLOPT_MAXEVAL_REACHED: Optimization stopped because maxeval (above) was reached
INFO - 17:25:00: Number of calls to the objective function by the optimizer: 8
INFO - 17:25:00: Solution:
WARNING - 17:25:00: The solution is not feasible.
INFO - 17:25:00: Objective: -4492.389203686935
INFO - 17:25:00: Standardized constraints:
INFO - 17:25:00: lift - 0.5 = 0.008585874882770628
INFO - 17:25:00: Design space:
INFO - 17:25:00: +----------------+-------------+-------+-------------+-------+
INFO - 17:25:00: | name | lower_bound | value | upper_bound | type |
INFO - 17:25:00: +----------------+-------------+-------+-------------+-------+
INFO - 17:25:00: | thick_airfoils | 5 | 5 | 25 | float |
INFO - 17:25:00: +----------------+-------------+-------+-------------+-------+
INFO - 17:25:00: *** End MDOScenario execution (time: 0:00:00.019250) ***
INFO - 17:25:00:
INFO - 17:25:00: *** Start MDOScenario execution ***
INFO - 17:25:00: MDOScenario
INFO - 17:25:00: Disciplines: Mission Structure
INFO - 17:25:00: MDO formulation: DisciplinaryOpt
INFO - 17:25:00: Optimization problem:
INFO - 17:25:00: minimize -range(thick_panels)
INFO - 17:25:00: with respect to thick_panels
INFO - 17:25:00: subject to constraints:
INFO - 17:25:00: reserve_fact(thick_panels) <= 0.5
INFO - 17:25:00: over the design space:
INFO - 17:25:00: +--------------+-------------+-------------------+-------------+-------+
INFO - 17:25:00: | name | lower_bound | value | upper_bound | type |
INFO - 17:25:00: +--------------+-------------+-------------------+-------------+-------+
INFO - 17:25:00: | thick_panels | 1 | 3.303233602238194 | 20 | float |
INFO - 17:25:00: +--------------+-------------+-------------------+-------------+-------+
INFO - 17:25:00: Solving optimization problem with algorithm NLOPT_SLSQP:
INFO - 17:25:00: ... 0%| | 0/5 [00:00<?, ?it]
INFO - 17:25:00:
INFO - 17:25:00: ... 20%|██ | 1/5 [00:00<00:00, 474.15 it/sec, obj=-4.5e+3]
INFO - 17:25:00:
ERROR - 17:25:00: NLopt run failed: NLopt roundoff-limited, RoundoffLimited
INFO - 17:25:00: ... 40%|████ | 2/5 [00:00<00:00, 160.24 it/sec, obj=-4.5e+3]
INFO - 17:25:00:
INFO - 17:25:00:
INFO - 17:25:00: Optimization result:
INFO - 17:25:00: Optimizer info:
INFO - 17:25:00: Status: None
INFO - 17:25:00: Message: GEMSEO Stopped the driver
INFO - 17:25:00: Number of calls to the objective function by the optimizer: 3
INFO - 17:25:00: Solution:
INFO - 17:25:00: The solution is feasible.
INFO - 17:25:00: Objective: -4504.850157624369
INFO - 17:25:00: Standardized constraints:
INFO - 17:25:00: reserve_fact - 0.5 = -2.198845550083206e-10
INFO - 17:25:00: Design space:
INFO - 17:25:00: +--------------+-------------+------------------+-------------+-------+
INFO - 17:25:00: | name | lower_bound | value | upper_bound | type |
INFO - 17:25:00: +--------------+-------------+------------------+-------------+-------+
INFO - 17:25:00: | thick_panels | 1 | 3.26453684407339 | 20 | float |
INFO - 17:25:00: +--------------+-------------+------------------+-------------+-------+
INFO - 17:25:00: *** End MDOScenario execution (time: 0:00:00.018142) ***
INFO - 17:25:00: ... 86%|████████▌ | 6/7 [00:00<00:00, 9.97 it/sec, obj=-4.51e+3]
INFO - 17:25:00:
INFO - 17:25:00: *** Start MDOScenario execution ***
INFO - 17:25:00: MDOScenario
INFO - 17:25:00: Disciplines: Aerodynamics Mission
INFO - 17:25:00: MDO formulation: DisciplinaryOpt
INFO - 17:25:00: Optimization problem:
INFO - 17:25:00: minimize -range(thick_airfoils)
INFO - 17:25:00: with respect to thick_airfoils
INFO - 17:25:00: subject to constraints:
INFO - 17:25:00: lift(thick_airfoils) == 0.5
INFO - 17:25:00: over the design space:
INFO - 17:25:00: +----------------+-------------+-------+-------------+-------+
INFO - 17:25:00: | name | lower_bound | value | upper_bound | type |
INFO - 17:25:00: +----------------+-------------+-------+-------------+-------+
INFO - 17:25:00: | thick_airfoils | 5 | 5 | 25 | float |
INFO - 17:25:00: +----------------+-------------+-------+-------------+-------+
INFO - 17:25:00: Solving optimization problem with algorithm NLOPT_SLSQP:
INFO - 17:25:00: ... 0%| | 0/5 [00:00<?, ?it]
INFO - 17:25:00:
INFO - 17:25:00: ... 20%|██ | 1/5 [00:00<00:00, 467.12 it/sec, obj=-4.51e+3]
INFO - 17:25:00:
INFO - 17:25:00: ... 40%|████ | 2/5 [00:00<00:00, 145.82 it/sec, obj=-4.48e+3]
INFO - 17:25:00:
INFO - 17:25:00: ... 60%|██████ | 3/5 [00:00<00:00, 210.10 it/sec, obj=-4.51e+3]
INFO - 17:25:00:
INFO - 17:25:00: ... 80%|████████ | 4/5 [00:00<00:00, 216.94 it/sec, obj=-4.51e+3]
INFO - 17:25:00:
INFO - 17:25:00: ... 100%|██████████| 5/5 [00:00<00:00, 221.74 it/sec, obj=-4.51e+3]
INFO - 17:25:00:
INFO - 17:25:00:
INFO - 17:25:00: Optimization result:
INFO - 17:25:00: Optimizer info:
INFO - 17:25:00: Status: None
INFO - 17:25:00: Message: Maximum number of iterations reached. GEMSEO Stopped the driver
INFO - 17:25:00: Number of calls to the objective function by the optimizer: 7
INFO - 17:25:00: Solution:
INFO - 17:25:00: The solution is feasible.
INFO - 17:25:00: Objective: -4509.519641910823
INFO - 17:25:00: Standardized constraints:
INFO - 17:25:00: lift - 0.5 = -0.00013691255181019768
INFO - 17:25:00: Design space:
INFO - 17:25:00: +----------------+-------------+-------+-------------+-------+
INFO - 17:25:00: | name | lower_bound | value | upper_bound | type |
INFO - 17:25:00: +----------------+-------------+-------+-------------+-------+
INFO - 17:25:00: | thick_airfoils | 5 | 5 | 25 | float |
INFO - 17:25:00: +----------------+-------------+-------+-------------+-------+
INFO - 17:25:00: *** End MDOScenario execution (time: 0:00:00.033158) ***
INFO - 17:25:00:
INFO - 17:25:00: *** Start MDOScenario execution ***
INFO - 17:25:00: MDOScenario
INFO - 17:25:00: Disciplines: Mission Structure
INFO - 17:25:00: MDO formulation: DisciplinaryOpt
INFO - 17:25:00: Optimization problem:
INFO - 17:25:00: minimize -range(thick_panels)
INFO - 17:25:00: with respect to thick_panels
INFO - 17:25:00: subject to constraints:
INFO - 17:25:00: reserve_fact(thick_panels) <= 0.5
INFO - 17:25:00: over the design space:
INFO - 17:25:00: +--------------+-------------+------------------+-------------+-------+
INFO - 17:25:00: | name | lower_bound | value | upper_bound | type |
INFO - 17:25:00: +--------------+-------------+------------------+-------------+-------+
INFO - 17:25:00: | thick_panels | 1 | 3.26453684407339 | 20 | float |
INFO - 17:25:00: +--------------+-------------+------------------+-------------+-------+
INFO - 17:25:00: Solving optimization problem with algorithm NLOPT_SLSQP:
INFO - 17:25:00: ... 0%| | 0/5 [00:00<?, ?it]
INFO - 17:25:00:
INFO - 17:25:00: ... 20%|██ | 1/5 [00:00<00:00, 479.40 it/sec, obj=-4.51e+3]
INFO - 17:25:00:
INFO - 17:25:00: ... 40%|████ | 2/5 [00:00<00:00, 132.59 it/sec, obj=-4.51e+3]
INFO - 17:25:00:
INFO - 17:25:00: ... 60%|██████ | 3/5 [00:00<00:00, 142.64 it/sec, obj=-4.51e+3]
INFO - 17:25:00:
INFO - 17:25:00: ... 80%|████████ | 4/5 [00:00<00:00, 185.54 it/sec, obj=-4.51e+3]
INFO - 17:25:00:
INFO - 17:25:00:
INFO - 17:25:00: Optimization result:
INFO - 17:25:00: Optimizer info:
INFO - 17:25:00: Status: None
INFO - 17:25:00: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO Stopped the driver
INFO - 17:25:00: Number of calls to the objective function by the optimizer: 5
INFO - 17:25:00: Solution:
INFO - 17:25:00: The solution is feasible.
INFO - 17:25:00: Objective: -4509.583287367007
INFO - 17:25:00: Standardized constraints:
INFO - 17:25:00: reserve_fact - 0.5 = 2.2632107743447705e-08
INFO - 17:25:00: Design space:
INFO - 17:25:00: +--------------+-------------+-------------------+-------------+-------+
INFO - 17:25:00: | name | lower_bound | value | upper_bound | type |
INFO - 17:25:00: +--------------+-------------+-------------------+-------------+-------+
INFO - 17:25:00: | thick_panels | 1 | 3.225021422872048 | 20 | float |
INFO - 17:25:00: +--------------+-------------+-------------------+-------------+-------+
INFO - 17:25:00: *** End MDOScenario execution (time: 0:00:00.028096) ***
INFO - 17:25:00: ... 100%|██████████| 7/7 [00:00<00:00, 10.02 it/sec, obj=-4.51e+3]
INFO - 17:25:00: Optimization result:
INFO - 17:25:00: Optimizer info:
INFO - 17:25:00: Status: None
INFO - 17:25:00: Message: Maximum number of iterations reached. GEMSEO Stopped the driver
INFO - 17:25:00: Number of calls to the objective function by the optimizer: 9
INFO - 17:25:00: Solution:
INFO - 17:25:00: The solution is feasible.
INFO - 17:25:00: Objective: -4509.243436177998
INFO - 17:25:00: Standardized constraints:
INFO - 17:25:00: lift - 0.5 = 5.5555555820374636e-05
INFO - 17:25:00: reserve_fact - 0.5 = -0.1583333328503187
INFO - 17:25:00: Design space:
INFO - 17:25:00: +-------+-------------+-------+-------------+-------+
INFO - 17:25:00: | name | lower_bound | value | upper_bound | type |
INFO - 17:25:00: +-------+-------------+-------+-------------+-------+
INFO - 17:25:00: | sweep | 10 | 25 | 35 | float |
INFO - 17:25:00: +-------+-------------+-------+-------------+-------+
INFO - 17:25:00: *** End MDOScenario execution (time: 0:00:00.723821) ***
<gemseo.post.opt_history_view.OptHistoryView object at 0x7fcce877ce20>
Total running time of the script: ( 0 minutes 4.928 seconds)