Note
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MDO formulations for a toy example in aerostructure¶
from __future__ import annotations
from copy import deepcopy
from gemseo import configure_logger
from gemseo import create_discipline
from gemseo import create_scenario
from gemseo 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/5.0.1/lib/python3.9/site-packages/gemseo/algos/design_space.py:426: ComplexWarning: Casting complex values to real discards the imaginary part
self.__current_value[name] = array_value.astype(
INFO - 08:37:25: Variable reserve_fact was removed from the Design Space, it is not an input of any discipline.
INFO - 08:37:25:
INFO - 08:37:25: *** Start MDOScenario execution ***
INFO - 08:37:25: MDOScenario
INFO - 08:37:25: Disciplines: Aerodynamics Mission Structure
INFO - 08:37:25: MDO formulation: MDF
INFO - 08:37:25: Optimization problem:
INFO - 08:37:25: minimize -range(thick_airfoils, thick_panels, sweep)
INFO - 08:37:25: with respect to sweep, thick_airfoils, thick_panels
INFO - 08:37:25: subject to constraints:
INFO - 08:37:25: reserve_fact(thick_airfoils, thick_panels, sweep) <= 0.5
INFO - 08:37:25: lift(thick_airfoils, thick_panels, sweep) == 0.5
INFO - 08:37:25: over the design space:
INFO - 08:37:25: +----------------+-------------+-------+-------------+-------+
INFO - 08:37:25: | name | lower_bound | value | upper_bound | type |
INFO - 08:37:25: +----------------+-------------+-------+-------------+-------+
INFO - 08:37:25: | thick_airfoils | 5 | 15 | 25 | float |
INFO - 08:37:25: | thick_panels | 1 | 3 | 20 | float |
INFO - 08:37:25: | sweep | 10 | 25 | 35 | float |
INFO - 08:37:25: +----------------+-------------+-------+-------------+-------+
INFO - 08:37:25: Solving optimization problem with algorithm NLOPT_SLSQP:
INFO - 08:37:25: ... 0%| | 0/10 [00:00<?, ?it]
INFO - 08:37:25: ... 10%|█ | 1/10 [00:00<00:00, 30.25 it/sec, obj=-4.25e+3]
INFO - 08:37:25: ... 20%|██ | 2/10 [00:00<00:00, 12.47 it/sec, obj=-4.51e+3]
INFO - 08:37:25: ... 30%|███ | 3/10 [00:00<00:00, 14.59 it/sec, obj=-4.51e+3]
INFO - 08:37:25: ... 40%|████ | 4/10 [00:00<00:00, 19.35 it/sec, obj=Not evaluated]
INFO - 08:37:25: Optimization result:
INFO - 08:37:25: Optimizer info:
INFO - 08:37:25: Status: None
INFO - 08:37:25: Message: Successive iterates of the design variables are closer than xtol_rel or xtol_abs. GEMSEO Stopped the driver
INFO - 08:37:25: Number of calls to the objective function by the optimizer: 4
INFO - 08:37:25: Solution:
INFO - 08:37:25: The solution is feasible.
INFO - 08:37:25: Objective: -4509.505446928907
INFO - 08:37:25: Standardized constraints:
INFO - 08:37:25: lift - 0.5 = 1.1963030566164434e-10
INFO - 08:37:25: reserve_fact - 0.5 = 2.204757620916098e-07
INFO - 08:37:25: Design space:
INFO - 08:37:25: +----------------+-------------+-------------------+-------------+-------+
INFO - 08:37:25: | name | lower_bound | value | upper_bound | type |
INFO - 08:37:25: +----------------+-------------+-------------------+-------------+-------+
INFO - 08:37:25: | thick_airfoils | 5 | 5 | 25 | float |
INFO - 08:37:25: | thick_panels | 1 | 3.225589189454885 | 20 | float |
INFO - 08:37:25: | sweep | 10 | 24.99326599322578 | 35 | float |
INFO - 08:37:25: +----------------+-------------+-------------------+-------------+-------+
INFO - 08:37:25: *** End MDOScenario execution (time: 0:00:00.220410) ***
/home/docs/checkouts/readthedocs.org/user_builds/gemseo/envs/5.0.1/lib/python3.9/site-packages/genson/schema/strategies/base.py:42: UserWarning: Schema incompatible. Keyword 'description' has conflicting values ('The width and height of the figure in inches, e.g. ``(w, h)``.\nIf ``None``, use the :attr:`.OptPostProcessor.DEFAULT_FIG_SIZE`\nof the post-processor.' vs. 'The width and height of the figure in inches, e.g. `(w, h)`.\nIf ``None``, use the :attr:`.OptPostProcessor.DEFAULT_FIG_SIZE`\nof the post-processor.'). Using 'The width and height of the figure in inches, e.g. ``(w, h)``.\nIf ``None``, use the :attr:`.OptPostProcessor.DEFAULT_FIG_SIZE`\nof the post-processor.'
warn(('Schema incompatible. Keyword {0!r} has conflicting '
/home/docs/checkouts/readthedocs.org/user_builds/gemseo/envs/5.0.1/lib/python3.9/site-packages/gemseo/post/opt_history_view.py:599: UserWarning: All values for SymLogScale are below linthresh, making it effectively linear. You likely should lower the value of linthresh.
col_bar = fig.colorbar(
<gemseo.post.opt_history_view.OptHistoryView object at 0x7f873bd0cdc0>
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()
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 - 08:37:26:
INFO - 08:37:26: *** Start MDOScenario execution ***
INFO - 08:37:26: MDOScenario
INFO - 08:37:26: Disciplines: MDOScenario MDOScenario Mission
INFO - 08:37:26: MDO formulation: BiLevel
INFO - 08:37:26: Optimization problem:
INFO - 08:37:26: minimize -range(sweep)
INFO - 08:37:26: with respect to sweep
INFO - 08:37:26: subject to constraints:
INFO - 08:37:26: reserve_fact(sweep) <= 0.5
INFO - 08:37:26: lift(sweep) == 0.5
INFO - 08:37:26: over the design space:
INFO - 08:37:26: +-------+-------------+-------+-------------+-------+
INFO - 08:37:26: | name | lower_bound | value | upper_bound | type |
INFO - 08:37:26: +-------+-------------+-------+-------------+-------+
INFO - 08:37:26: | sweep | 10 | 25 | 35 | float |
INFO - 08:37:26: +-------+-------------+-------+-------------+-------+
INFO - 08:37:26: Solving optimization problem with algorithm NLOPT_COBYLA:
INFO - 08:37:26: ... 0%| | 0/7 [00:00<?, ?it]
INFO - 08:37:26:
INFO - 08:37:26: *** Start MDOScenario execution ***
INFO - 08:37:26: MDOScenario
INFO - 08:37:26: Disciplines: Aerodynamics Mission
INFO - 08:37:26: MDO formulation: DisciplinaryOpt
INFO - 08:37:26: Optimization problem:
INFO - 08:37:26: minimize -range(thick_airfoils)
INFO - 08:37:26: with respect to thick_airfoils
INFO - 08:37:26: subject to constraints:
INFO - 08:37:26: lift(thick_airfoils) == 0.5
INFO - 08:37:26: over the design space:
INFO - 08:37:26: +----------------+-------------+-------+-------------+-------+
INFO - 08:37:26: | name | lower_bound | value | upper_bound | type |
INFO - 08:37:26: +----------------+-------------+-------+-------------+-------+
INFO - 08:37:26: | thick_airfoils | 5 | 15 | 25 | float |
INFO - 08:37:26: +----------------+-------------+-------+-------------+-------+
INFO - 08:37:26: Solving optimization problem with algorithm NLOPT_SLSQP:
INFO - 08:37:26: ... 0%| | 0/5 [00:00<?, ?it]
INFO - 08:37:26:
INFO - 08:37:26: ... 20%|██ | 1/5 [00:00<00:00, 193.29 it/sec, obj=-4.27e+3]
INFO - 08:37:26:
WARNING - 08:37:26: Optimization found no feasible point ! The least infeasible point is selected.
INFO - 08:37:26: ... 40%|████ | 2/5 [00:00<00:00, 166.93 it/sec, obj=-4.51e+3]
INFO - 08:37:26:
INFO - 08:37:26:
INFO - 08:37:26: Optimization result:
INFO - 08:37:26: Optimizer info:
INFO - 08:37:26: Status: 5
INFO - 08:37:26: Message: NLOPT_MAXEVAL_REACHED: Optimization stopped because maxeval (above) was reached
INFO - 08:37:26: Number of calls to the objective function by the optimizer: 8
INFO - 08:37:26: Solution:
WARNING - 08:37:26: The solution is not feasible.
INFO - 08:37:26: Objective: -4513.429203824652
INFO - 08:37:26: Standardized constraints:
INFO - 08:37:26: lift - 0.5 = 0.008666666666666822
INFO - 08:37:26: Design space:
INFO - 08:37:26: +----------------+-------------+-------+-------------+-------+
INFO - 08:37:26: | name | lower_bound | value | upper_bound | type |
INFO - 08:37:26: +----------------+-------------+-------+-------------+-------+
INFO - 08:37:26: | thick_airfoils | 5 | 5 | 25 | float |
INFO - 08:37:26: +----------------+-------------+-------+-------------+-------+
INFO - 08:37:26: *** End MDOScenario execution (time: 0:00:00.023816) ***
INFO - 08:37:26:
INFO - 08:37:26: *** Start MDOScenario execution ***
INFO - 08:37:26: MDOScenario
INFO - 08:37:26: Disciplines: Mission Structure
INFO - 08:37:26: MDO formulation: DisciplinaryOpt
INFO - 08:37:26: Optimization problem:
INFO - 08:37:26: minimize -range(thick_panels)
INFO - 08:37:26: with respect to thick_panels
INFO - 08:37:26: subject to constraints:
INFO - 08:37:26: reserve_fact(thick_panels) <= 0.5
INFO - 08:37:26: over the design space:
INFO - 08:37:26: +--------------+-------------+-------+-------------+-------+
INFO - 08:37:26: | name | lower_bound | value | upper_bound | type |
INFO - 08:37:26: +--------------+-------------+-------+-------------+-------+
INFO - 08:37:26: | thick_panels | 1 | 3 | 20 | float |
INFO - 08:37:26: +--------------+-------------+-------+-------------+-------+
INFO - 08:37:26: Solving optimization problem with algorithm NLOPT_SLSQP:
INFO - 08:37:26: ... 0%| | 0/5 [00:00<?, ?it]
INFO - 08:37:26:
INFO - 08:37:26: ... 20%|██ | 1/5 [00:00<00:00, 182.23 it/sec, obj=-4.51e+3]
INFO - 08:37:26:
ERROR - 08:37:26: NLopt run failed: NLopt roundoff-limited, RoundoffLimited
INFO - 08:37:26: ... 40%|████ | 2/5 [00:00<00:00, 173.99 it/sec, obj=-4.5e+3]
INFO - 08:37:26:
INFO - 08:37:26:
INFO - 08:37:26: Optimization result:
INFO - 08:37:26: Optimizer info:
INFO - 08:37:26: Status: None
INFO - 08:37:26: Message: GEMSEO Stopped the driver
INFO - 08:37:26: Number of calls to the objective function by the optimizer: 3
INFO - 08:37:26: Solution:
INFO - 08:37:26: The solution is feasible.
INFO - 08:37:26: Objective: -4504.955637332531
INFO - 08:37:26: Standardized constraints:
INFO - 08:37:26: reserve_fact - 0.5 = 1.062133492268913e-09
INFO - 08:37:26: Design space:
INFO - 08:37:26: +--------------+-------------+-------------------+-------------+-------+
INFO - 08:37:26: | name | lower_bound | value | upper_bound | type |
INFO - 08:37:26: +--------------+-------------+-------------------+-------------+-------+
INFO - 08:37:26: | thick_panels | 1 | 3.266666666489645 | 20 | float |
INFO - 08:37:26: +--------------+-------------+-------------------+-------------+-------+
INFO - 08:37:26: *** End MDOScenario execution (time: 0:00:00.023019) ***
INFO - 08:37:26: ... 14%|█▍ | 1/7 [00:00<00:00, 9.05 it/sec, obj=-4.51e+3]
INFO - 08:37:26:
INFO - 08:37:26: *** Start MDOScenario execution ***
INFO - 08:37:26: MDOScenario
INFO - 08:37:26: Disciplines: Aerodynamics Mission
INFO - 08:37:26: MDO formulation: DisciplinaryOpt
INFO - 08:37:26: Optimization problem:
INFO - 08:37:26: minimize -range(thick_airfoils)
INFO - 08:37:26: with respect to thick_airfoils
INFO - 08:37:26: subject to constraints:
INFO - 08:37:26: lift(thick_airfoils) == 0.5
INFO - 08:37:26: over the design space:
INFO - 08:37:26: +----------------+-------------+-------+-------------+-------+
INFO - 08:37:26: | name | lower_bound | value | upper_bound | type |
INFO - 08:37:26: +----------------+-------------+-------+-------------+-------+
INFO - 08:37:26: | thick_airfoils | 5 | 5 | 25 | float |
INFO - 08:37:26: +----------------+-------------+-------+-------------+-------+
INFO - 08:37:26: Solving optimization problem with algorithm NLOPT_SLSQP:
INFO - 08:37:26: ... 0%| | 0/5 [00:00<?, ?it]
INFO - 08:37:26:
INFO - 08:37:26: ... 20%|██ | 1/5 [00:00<00:00, 915.99 it/sec, obj=-4.27e+3]
INFO - 08:37:26:
WARNING - 08:37:26: Optimization found no feasible point ! The least infeasible point is selected.
INFO - 08:37:26:
INFO - 08:37:26: Optimization result:
INFO - 08:37:26: Optimizer info:
INFO - 08:37:26: Status: 5
INFO - 08:37:26: Message: NLOPT_MAXEVAL_REACHED: Optimization stopped because maxeval (above) was reached
INFO - 08:37:26: Number of calls to the objective function by the optimizer: 8
INFO - 08:37:26: Solution:
WARNING - 08:37:26: The solution is not feasible.
INFO - 08:37:26: Objective: -4267.910320106268
INFO - 08:37:26: Standardized constraints:
INFO - 08:37:26: lift - 0.5 = 0.12708333333392374
INFO - 08:37:26: Design space:
INFO - 08:37:26: +----------------+-------------+-------+-------------+-------+
INFO - 08:37:26: | name | lower_bound | value | upper_bound | type |
INFO - 08:37:26: +----------------+-------------+-------+-------------+-------+
INFO - 08:37:26: | thick_airfoils | 5 | 5 | 25 | float |
INFO - 08:37:26: +----------------+-------------+-------+-------------+-------+
INFO - 08:37:26: *** End MDOScenario execution (time: 0:00:00.015504) ***
INFO - 08:37:26:
INFO - 08:37:26: *** Start MDOScenario execution ***
INFO - 08:37:26: MDOScenario
INFO - 08:37:26: Disciplines: Mission Structure
INFO - 08:37:26: MDO formulation: DisciplinaryOpt
INFO - 08:37:26: Optimization problem:
INFO - 08:37:26: minimize -range(thick_panels)
INFO - 08:37:26: with respect to thick_panels
INFO - 08:37:26: subject to constraints:
INFO - 08:37:26: reserve_fact(thick_panels) <= 0.5
INFO - 08:37:26: over the design space:
INFO - 08:37:26: +--------------+-------------+-------------------+-------------+-------+
INFO - 08:37:26: | name | lower_bound | value | upper_bound | type |
INFO - 08:37:26: +--------------+-------------+-------------------+-------------+-------+
INFO - 08:37:26: | thick_panels | 1 | 3.266666666489645 | 20 | float |
INFO - 08:37:26: +--------------+-------------+-------------------+-------------+-------+
INFO - 08:37:26: Solving optimization problem with algorithm NLOPT_SLSQP:
INFO - 08:37:26: ... 0%| | 0/5 [00:00<?, ?it]
INFO - 08:37:26:
INFO - 08:37:26: ... 20%|██ | 1/5 [00:00<00:00, 998.41 it/sec, obj=-4.27e+3]
INFO - 08:37:26:
ERROR - 08:37:26: NLopt run failed: NLopt roundoff-limited, RoundoffLimited
INFO - 08:37:26: ... 40%|████ | 2/5 [00:00<00:00, 309.99 it/sec, obj=-4.27e+3]
INFO - 08:37:26:
INFO - 08:37:26:
INFO - 08:37:26: Optimization result:
INFO - 08:37:26: Optimizer info:
INFO - 08:37:26: Status: None
INFO - 08:37:26: Message: GEMSEO Stopped the driver
INFO - 08:37:26: Number of calls to the objective function by the optimizer: 3
INFO - 08:37:26: Solution:
INFO - 08:37:26: The solution is feasible.
INFO - 08:37:26: Objective: -4270.047650043281
INFO - 08:37:26: Standardized constraints:
INFO - 08:37:26: reserve_fact - 0.5 = 3.0379254667423083e-10
INFO - 08:37:26: Design space:
INFO - 08:37:26: +--------------+-------------+------------------+-------------+-------+
INFO - 08:37:26: | name | lower_bound | value | upper_bound | type |
INFO - 08:37:26: +--------------+-------------+------------------+-------------+-------+
INFO - 08:37:26: | thick_panels | 1 | 1.76499999995232 | 20 | float |
INFO - 08:37:26: +--------------+-------------+------------------+-------------+-------+
INFO - 08:37:26: *** End MDOScenario execution (time: 0:00:00.017453) ***
INFO - 08:37:26: ... 29%|██▊ | 2/7 [00:00<00:00, 12.43 it/sec, obj=-4.27e+3]
INFO - 08:37:26:
INFO - 08:37:26: *** Start MDOScenario execution ***
INFO - 08:37:26: MDOScenario
INFO - 08:37:26: Disciplines: Aerodynamics Mission
INFO - 08:37:26: MDO formulation: DisciplinaryOpt
INFO - 08:37:26: Optimization problem:
INFO - 08:37:26: minimize -range(thick_airfoils)
INFO - 08:37:26: with respect to thick_airfoils
INFO - 08:37:26: subject to constraints:
INFO - 08:37:26: lift(thick_airfoils) == 0.5
INFO - 08:37:26: over the design space:
INFO - 08:37:26: +----------------+-------------+-------+-------------+-------+
INFO - 08:37:26: | name | lower_bound | value | upper_bound | type |
INFO - 08:37:26: +----------------+-------------+-------+-------------+-------+
INFO - 08:37:26: | thick_airfoils | 5 | 5 | 25 | float |
INFO - 08:37:26: +----------------+-------------+-------+-------------+-------+
INFO - 08:37:26: Solving optimization problem with algorithm NLOPT_SLSQP:
INFO - 08:37:26: ... 0%| | 0/5 [00:00<?, ?it]
INFO - 08:37:26:
INFO - 08:37:26: ... 20%|██ | 1/5 [00:00<00:00, 796.64 it/sec, obj=-4.53e+3]
INFO - 08:37:26:
INFO - 08:37:26: ... 40%|████ | 2/5 [00:00<00:00, 265.29 it/sec, obj=-3.83e+3]
INFO - 08:37:26:
INFO - 08:37:26: ... 60%|██████ | 3/5 [00:00<00:00, 381.03 it/sec, obj=-4.43e+3]
INFO - 08:37:26:
INFO - 08:37:26: ... 80%|████████ | 4/5 [00:00<00:00, 401.46 it/sec, obj=-4.5e+3]
INFO - 08:37:26:
INFO - 08:37:26: ... 100%|██████████| 5/5 [00:00<00:00, 417.80 it/sec, obj=-4.51e+3]
INFO - 08:37:26:
WARNING - 08:37:26: Optimization found no feasible point ! The least infeasible point is selected.
INFO - 08:37:26:
INFO - 08:37:26: Optimization result:
INFO - 08:37:26: Optimizer info:
INFO - 08:37:26: Status: None
INFO - 08:37:26: Message: Maximum number of iterations reached. GEMSEO Stopped the driver
INFO - 08:37:26: Number of calls to the objective function by the optimizer: 7
INFO - 08:37:26: Solution:
WARNING - 08:37:26: The solution is not feasible.
INFO - 08:37:26: Objective: -3831.807218266315
INFO - 08:37:26: Standardized constraints:
INFO - 08:37:26: lift - 0.5 = -0.002337406467956049
INFO - 08:37:26: Design space:
INFO - 08:37:26: +----------------+-------------+-------+-------------+-------+
INFO - 08:37:26: | name | lower_bound | value | upper_bound | type |
INFO - 08:37:26: +----------------+-------------+-------+-------------+-------+
INFO - 08:37:26: | thick_airfoils | 5 | 25 | 25 | float |
INFO - 08:37:26: +----------------+-------------+-------+-------------+-------+
INFO - 08:37:26: *** End MDOScenario execution (time: 0:00:00.024183) ***
INFO - 08:37:26:
INFO - 08:37:26: *** Start MDOScenario execution ***
INFO - 08:37:26: MDOScenario
INFO - 08:37:26: Disciplines: Mission Structure
INFO - 08:37:26: MDO formulation: DisciplinaryOpt
INFO - 08:37:26: Optimization problem:
INFO - 08:37:26: minimize -range(thick_panels)
INFO - 08:37:26: with respect to thick_panels
INFO - 08:37:26: subject to constraints:
INFO - 08:37:26: reserve_fact(thick_panels) <= 0.5
INFO - 08:37:26: over the design space:
INFO - 08:37:26: +--------------+-------------+------------------+-------------+-------+
INFO - 08:37:26: | name | lower_bound | value | upper_bound | type |
INFO - 08:37:26: +--------------+-------------+------------------+-------------+-------+
INFO - 08:37:26: | thick_panels | 1 | 1.76499999995232 | 20 | float |
INFO - 08:37:26: +--------------+-------------+------------------+-------------+-------+
INFO - 08:37:26: Solving optimization problem with algorithm NLOPT_SLSQP:
INFO - 08:37:26: ... 0%| | 0/5 [00:00<?, ?it]
INFO - 08:37:26:
INFO - 08:37:26: ... 20%|██ | 1/5 [00:00<00:00, 755.32 it/sec, obj=-3.82e+3]
INFO - 08:37:26:
INFO - 08:37:26: ... 40%|████ | 2/5 [00:00<00:00, 246.87 it/sec, obj=-3.82e+3]
INFO - 08:37:26:
INFO - 08:37:26: ... 60%|██████ | 3/5 [00:00<00:00, 269.16 it/sec, obj=-3.82e+3]
INFO - 08:37:26:
INFO - 08:37:26: ... 80%|████████ | 4/5 [00:00<00:00, 348.52 it/sec, obj=-3.82e+3]
INFO - 08:37:26:
INFO - 08:37:26:
INFO - 08:37:26: Optimization result:
INFO - 08:37:26: Optimizer info:
INFO - 08:37:26: Status: None
INFO - 08:37:26: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO Stopped the driver
INFO - 08:37:26: Number of calls to the objective function by the optimizer: 5
INFO - 08:37:26: Solution:
INFO - 08:37:26: The solution is feasible.
INFO - 08:37:26: Objective: -3818.5902855979184
INFO - 08:37:26: Standardized constraints:
INFO - 08:37:26: reserve_fact - 0.5 = 3.0950531026974204e-09
INFO - 08:37:26: Design space:
INFO - 08:37:26: +--------------+-------------+-------------------+-------------+-------+
INFO - 08:37:26: | name | lower_bound | value | upper_bound | type |
INFO - 08:37:26: +--------------+-------------+-------------------+-------------+-------+
INFO - 08:37:26: | thick_panels | 1 | 3.414591822343108 | 20 | float |
INFO - 08:37:26: +--------------+-------------+-------------------+-------------+-------+
INFO - 08:37:26: *** End MDOScenario execution (time: 0:00:00.023024) ***
INFO - 08:37:26: ... 43%|████▎ | 3/7 [00:00<00:00, 13.14 it/sec, obj=-3.82e+3]
INFO - 08:37:26:
INFO - 08:37:26: *** Start MDOScenario execution ***
INFO - 08:37:26: MDOScenario
INFO - 08:37:26: Disciplines: Aerodynamics Mission
INFO - 08:37:26: MDO formulation: DisciplinaryOpt
INFO - 08:37:26: Optimization problem:
INFO - 08:37:26: minimize -range(thick_airfoils)
INFO - 08:37:26: with respect to thick_airfoils
INFO - 08:37:26: subject to constraints:
INFO - 08:37:26: lift(thick_airfoils) == 0.5
INFO - 08:37:26: over the design space:
INFO - 08:37:26: +----------------+-------------+-------+-------------+-------+
INFO - 08:37:26: | name | lower_bound | value | upper_bound | type |
INFO - 08:37:26: +----------------+-------------+-------+-------------+-------+
INFO - 08:37:26: | thick_airfoils | 5 | 25 | 25 | float |
INFO - 08:37:26: +----------------+-------------+-------+-------------+-------+
INFO - 08:37:26: Solving optimization problem with algorithm NLOPT_SLSQP:
INFO - 08:37:26: ... 0%| | 0/5 [00:00<?, ?it]
INFO - 08:37:26:
INFO - 08:37:26: ... 20%|██ | 1/5 [00:00<00:00, 779.76 it/sec, obj=-3.82e+3]
INFO - 08:37:26:
WARNING - 08:37:26: Optimization found no feasible point ! The least infeasible point is selected.
INFO - 08:37:26: ... 40%|████ | 2/5 [00:00<00:00, 267.31 it/sec, obj=-4.49e+3]
INFO - 08:37:26:
INFO - 08:37:26:
INFO - 08:37:26: Optimization result:
INFO - 08:37:26: Optimizer info:
INFO - 08:37:26: Status: 5
INFO - 08:37:26: Message: NLOPT_MAXEVAL_REACHED: Optimization stopped because maxeval (above) was reached
INFO - 08:37:26: Number of calls to the objective function by the optimizer: 8
INFO - 08:37:26: Solution:
WARNING - 08:37:26: The solution is not feasible.
INFO - 08:37:26: Objective: -4490.540174494245
INFO - 08:37:26: Standardized constraints:
INFO - 08:37:26: lift - 0.5 = 0.00918103190667352
INFO - 08:37:26: Design space:
INFO - 08:37:26: +----------------+-------------+-------+-------------+-------+
INFO - 08:37:26: | name | lower_bound | value | upper_bound | type |
INFO - 08:37:26: +----------------+-------------+-------+-------------+-------+
INFO - 08:37:26: | thick_airfoils | 5 | 5 | 25 | float |
INFO - 08:37:26: +----------------+-------------+-------+-------------+-------+
INFO - 08:37:26: *** End MDOScenario execution (time: 0:00:00.018435) ***
INFO - 08:37:26:
INFO - 08:37:26: *** Start MDOScenario execution ***
INFO - 08:37:26: MDOScenario
INFO - 08:37:26: Disciplines: Mission Structure
INFO - 08:37:26: MDO formulation: DisciplinaryOpt
INFO - 08:37:26: Optimization problem:
INFO - 08:37:26: minimize -range(thick_panels)
INFO - 08:37:26: with respect to thick_panels
INFO - 08:37:26: subject to constraints:
INFO - 08:37:26: reserve_fact(thick_panels) <= 0.5
INFO - 08:37:26: over the design space:
INFO - 08:37:26: +--------------+-------------+-------------------+-------------+-------+
INFO - 08:37:26: | name | lower_bound | value | upper_bound | type |
INFO - 08:37:26: +--------------+-------------+-------------------+-------------+-------+
INFO - 08:37:26: | thick_panels | 1 | 3.414591822343108 | 20 | float |
INFO - 08:37:26: +--------------+-------------+-------------------+-------------+-------+
INFO - 08:37:26: Solving optimization problem with algorithm NLOPT_SLSQP:
INFO - 08:37:26: ... 0%| | 0/5 [00:00<?, ?it]
INFO - 08:37:26:
INFO - 08:37:26: ... 20%|██ | 1/5 [00:00<00:00, 758.74 it/sec, obj=-4.5e+3]
INFO - 08:37:26:
INFO - 08:37:26: ... 40%|████ | 2/5 [00:00<00:00, 244.30 it/sec, obj=-4.5e+3]
INFO - 08:37:26:
INFO - 08:37:26: ... 60%|██████ | 3/5 [00:00<00:00, 268.94 it/sec, obj=-4.5e+3]
INFO - 08:37:26:
INFO - 08:37:26: ... 80%|████████ | 4/5 [00:00<00:00, 348.21 it/sec, obj=-4.5e+3]
INFO - 08:37:26:
INFO - 08:37:26:
INFO - 08:37:26: Optimization result:
INFO - 08:37:26: Optimizer info:
INFO - 08:37:26: Status: None
INFO - 08:37:26: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO Stopped the driver
INFO - 08:37:26: Number of calls to the objective function by the optimizer: 5
INFO - 08:37:26: Solution:
INFO - 08:37:26: The solution is feasible.
INFO - 08:37:26: Objective: -4503.594576639364
INFO - 08:37:26: Standardized constraints:
INFO - 08:37:26: reserve_fact - 0.5 = 2.4330390147042635e-08
INFO - 08:37:26: Design space:
INFO - 08:37:26: +--------------+-------------+-------------------+-------------+-------+
INFO - 08:37:26: | name | lower_bound | value | upper_bound | type |
INFO - 08:37:26: +--------------+-------------+-------------------+-------------+-------+
INFO - 08:37:26: | thick_panels | 1 | 3.256301554313449 | 20 | float |
INFO - 08:37:26: +--------------+-------------+-------------------+-------------+-------+
INFO - 08:37:26: *** End MDOScenario execution (time: 0:00:00.023404) ***
INFO - 08:37:26: ... 57%|█████▋ | 4/7 [00:00<00:00, 13.84 it/sec, obj=-4.51e+3]
INFO - 08:37:26:
INFO - 08:37:26: *** Start MDOScenario execution ***
INFO - 08:37:26: MDOScenario
INFO - 08:37:26: Disciplines: Aerodynamics Mission
INFO - 08:37:26: MDO formulation: DisciplinaryOpt
INFO - 08:37:26: Optimization problem:
INFO - 08:37:26: minimize -range(thick_airfoils)
INFO - 08:37:26: with respect to thick_airfoils
INFO - 08:37:26: subject to constraints:
INFO - 08:37:26: lift(thick_airfoils) == 0.5
INFO - 08:37:26: over the design space:
INFO - 08:37:26: +----------------+-------------+-------+-------------+-------+
INFO - 08:37:26: | name | lower_bound | value | upper_bound | type |
INFO - 08:37:26: +----------------+-------------+-------+-------------+-------+
INFO - 08:37:26: | thick_airfoils | 5 | 5 | 25 | float |
INFO - 08:37:26: +----------------+-------------+-------+-------------+-------+
INFO - 08:37:26: Solving optimization problem with algorithm NLOPT_SLSQP:
INFO - 08:37:26: ... 0%| | 0/5 [00:00<?, ?it]
INFO - 08:37:26:
INFO - 08:37:26: ... 20%|██ | 1/5 [00:00<00:00, 917.19 it/sec, obj=-4.51e+3]
INFO - 08:37:26:
INFO - 08:37:26: ... 40%|████ | 2/5 [00:00<00:00, 271.05 it/sec, obj=-3.85e+3]
INFO - 08:37:26:
INFO - 08:37:26: ... 60%|██████ | 3/5 [00:00<00:00, 388.78 it/sec, obj=-4.48e+3]
INFO - 08:37:26:
INFO - 08:37:26: ... 80%|████████ | 4/5 [00:00<00:00, 395.91 it/sec, obj=-4.51e+3]
INFO - 08:37:26:
INFO - 08:37:26: ... 100%|██████████| 5/5 [00:00<00:00, 400.04 it/sec, obj=-4.51e+3]
INFO - 08:37:26:
INFO - 08:37:26:
INFO - 08:37:26: Optimization result:
INFO - 08:37:26: Optimizer info:
INFO - 08:37:26: Status: None
INFO - 08:37:26: Message: Maximum number of iterations reached. GEMSEO Stopped the driver
INFO - 08:37:26: Number of calls to the objective function by the optimizer: 7
INFO - 08:37:26: Solution:
INFO - 08:37:26: The solution is feasible.
INFO - 08:37:26: Objective: -3854.0820028049116
INFO - 08:37:26: Standardized constraints:
INFO - 08:37:26: lift - 0.5 = 0.0
INFO - 08:37:26: Design space:
INFO - 08:37:26: +----------------+-------------+-------------------+-------------+-------+
INFO - 08:37:26: | name | lower_bound | value | upper_bound | type |
INFO - 08:37:26: +----------------+-------------+-------------------+-------------+-------+
INFO - 08:37:26: | thick_airfoils | 5 | 24.35677013380376 | 25 | float |
INFO - 08:37:26: +----------------+-------------+-------------------+-------------+-------+
INFO - 08:37:26: *** End MDOScenario execution (time: 0:00:00.026010) ***
INFO - 08:37:26:
INFO - 08:37:26: *** Start MDOScenario execution ***
INFO - 08:37:26: MDOScenario
INFO - 08:37:26: Disciplines: Mission Structure
INFO - 08:37:26: MDO formulation: DisciplinaryOpt
INFO - 08:37:26: Optimization problem:
INFO - 08:37:26: minimize -range(thick_panels)
INFO - 08:37:26: with respect to thick_panels
INFO - 08:37:26: subject to constraints:
INFO - 08:37:26: reserve_fact(thick_panels) <= 0.5
INFO - 08:37:26: over the design space:
INFO - 08:37:26: +--------------+-------------+-------------------+-------------+-------+
INFO - 08:37:26: | name | lower_bound | value | upper_bound | type |
INFO - 08:37:26: +--------------+-------------+-------------------+-------------+-------+
INFO - 08:37:26: | thick_panels | 1 | 3.256301554313449 | 20 | float |
INFO - 08:37:26: +--------------+-------------+-------------------+-------------+-------+
INFO - 08:37:26: Solving optimization problem with algorithm NLOPT_SLSQP:
INFO - 08:37:26: ... 0%| | 0/5 [00:00<?, ?it]
INFO - 08:37:26:
INFO - 08:37:26: ... 20%|██ | 1/5 [00:00<00:00, 765.66 it/sec, obj=-3.84e+3]
INFO - 08:37:26:
INFO - 08:37:26: ... 40%|████ | 2/5 [00:00<00:00, 244.07 it/sec, obj=-3.84e+3]
INFO - 08:37:26:
INFO - 08:37:26: ... 60%|██████ | 3/5 [00:00<00:00, 254.96 it/sec, obj=-3.84e+3]
INFO - 08:37:26:
INFO - 08:37:26: ... 80%|████████ | 4/5 [00:00<00:00, 317.29 it/sec, obj=Not evaluated]
INFO - 08:37:26:
INFO - 08:37:26:
INFO - 08:37:26: Optimization result:
INFO - 08:37:26: Optimizer info:
INFO - 08:37:26: Status: None
INFO - 08:37:26: Message: Successive iterates of the design variables are closer than xtol_rel or xtol_abs. GEMSEO Stopped the driver
INFO - 08:37:26: Number of calls to the objective function by the optimizer: 4
INFO - 08:37:26: Solution:
INFO - 08:37:26: The solution is feasible.
INFO - 08:37:26: Objective: -3843.382035512657
INFO - 08:37:26: Standardized constraints:
INFO - 08:37:26: reserve_fact - 0.5 = 3.418136884647538e-10
INFO - 08:37:26: Design space:
INFO - 08:37:26: +--------------+-------------+------------------+-------------+-------+
INFO - 08:37:26: | name | lower_bound | value | upper_bound | type |
INFO - 08:37:26: +--------------+-------------+------------------+-------------+-------+
INFO - 08:37:26: | thick_panels | 1 | 3.30323358999496 | 20 | float |
INFO - 08:37:26: +--------------+-------------+------------------+-------------+-------+
INFO - 08:37:26: *** End MDOScenario execution (time: 0:00:00.023852) ***
INFO - 08:37:26: ... 71%|███████▏ | 5/7 [00:00<00:00, 13.92 it/sec, obj=-3.85e+3]
INFO - 08:37:26:
INFO - 08:37:26: *** Start MDOScenario execution ***
INFO - 08:37:26: MDOScenario
INFO - 08:37:26: Disciplines: Aerodynamics Mission
INFO - 08:37:26: MDO formulation: DisciplinaryOpt
INFO - 08:37:26: Optimization problem:
INFO - 08:37:26: minimize -range(thick_airfoils)
INFO - 08:37:26: with respect to thick_airfoils
INFO - 08:37:26: subject to constraints:
INFO - 08:37:26: lift(thick_airfoils) == 0.5
INFO - 08:37:26: over the design space:
INFO - 08:37:26: +----------------+-------------+-------------------+-------------+-------+
INFO - 08:37:26: | name | lower_bound | value | upper_bound | type |
INFO - 08:37:26: +----------------+-------------+-------------------+-------------+-------+
INFO - 08:37:26: | thick_airfoils | 5 | 24.35677013380376 | 25 | float |
INFO - 08:37:26: +----------------+-------------+-------------------+-------------+-------+
INFO - 08:37:26: Solving optimization problem with algorithm NLOPT_SLSQP:
INFO - 08:37:26: ... 0%| | 0/5 [00:00<?, ?it]
INFO - 08:37:26:
INFO - 08:37:26: ... 20%|██ | 1/5 [00:00<00:00, 798.61 it/sec, obj=-3.85e+3]
INFO - 08:37:26:
WARNING - 08:37:26: Optimization found no feasible point ! The least infeasible point is selected.
INFO - 08:37:26: ... 40%|████ | 2/5 [00:00<00:00, 268.53 it/sec, obj=-4.49e+3]
INFO - 08:37:26:
INFO - 08:37:26:
INFO - 08:37:26: Optimization result:
INFO - 08:37:26: Optimizer info:
INFO - 08:37:26: Status: 5
INFO - 08:37:26: Message: NLOPT_MAXEVAL_REACHED: Optimization stopped because maxeval (above) was reached
INFO - 08:37:26: Number of calls to the objective function by the optimizer: 8
INFO - 08:37:26: Solution:
WARNING - 08:37:26: The solution is not feasible.
INFO - 08:37:26: Objective: -4492.389207173915
INFO - 08:37:26: Standardized constraints:
INFO - 08:37:26: lift - 0.5 = 0.00858587312068304
INFO - 08:37:26: Design space:
INFO - 08:37:26: +----------------+-------------+-------+-------------+-------+
INFO - 08:37:26: | name | lower_bound | value | upper_bound | type |
INFO - 08:37:26: +----------------+-------------+-------+-------------+-------+
INFO - 08:37:26: | thick_airfoils | 5 | 5 | 25 | float |
INFO - 08:37:26: +----------------+-------------+-------+-------------+-------+
INFO - 08:37:26: *** End MDOScenario execution (time: 0:00:00.019425) ***
INFO - 08:37:26:
INFO - 08:37:26: *** Start MDOScenario execution ***
INFO - 08:37:26: MDOScenario
INFO - 08:37:26: Disciplines: Mission Structure
INFO - 08:37:26: MDO formulation: DisciplinaryOpt
INFO - 08:37:26: Optimization problem:
INFO - 08:37:26: minimize -range(thick_panels)
INFO - 08:37:26: with respect to thick_panels
INFO - 08:37:26: subject to constraints:
INFO - 08:37:26: reserve_fact(thick_panels) <= 0.5
INFO - 08:37:26: over the design space:
INFO - 08:37:26: +--------------+-------------+------------------+-------------+-------+
INFO - 08:37:26: | name | lower_bound | value | upper_bound | type |
INFO - 08:37:26: +--------------+-------------+------------------+-------------+-------+
INFO - 08:37:26: | thick_panels | 1 | 3.30323358999496 | 20 | float |
INFO - 08:37:26: +--------------+-------------+------------------+-------------+-------+
INFO - 08:37:26: Solving optimization problem with algorithm NLOPT_SLSQP:
INFO - 08:37:26: ... 0%| | 0/5 [00:00<?, ?it]
INFO - 08:37:26:
INFO - 08:37:26: ... 20%|██ | 1/5 [00:00<00:00, 771.86 it/sec, obj=-4.5e+3]
INFO - 08:37:26:
ERROR - 08:37:26: NLopt run failed: NLopt roundoff-limited, RoundoffLimited
INFO - 08:37:26: ... 40%|████ | 2/5 [00:00<00:00, 284.54 it/sec, obj=-4.5e+3]
INFO - 08:37:26:
INFO - 08:37:26:
INFO - 08:37:26: Optimization result:
INFO - 08:37:26: Optimizer info:
INFO - 08:37:26: Status: None
INFO - 08:37:26: Message: GEMSEO Stopped the driver
INFO - 08:37:26: Number of calls to the objective function by the optimizer: 3
INFO - 08:37:26: Solution:
INFO - 08:37:26: The solution is feasible.
INFO - 08:37:26: Objective: -4504.850158522
INFO - 08:37:26: Standardized constraints:
INFO - 08:37:26: reserve_fact - 0.5 = 3.3662672649370506e-10
INFO - 08:37:26: Design space:
INFO - 08:37:26: +--------------+-------------+-------------------+-------------+-------+
INFO - 08:37:26: | name | lower_bound | value | upper_bound | type |
INFO - 08:37:26: +--------------+-------------+-------------------+-------------+-------+
INFO - 08:37:26: | thick_panels | 1 | 3.264536835170201 | 20 | float |
INFO - 08:37:26: +--------------+-------------+-------------------+-------------+-------+
INFO - 08:37:26: *** End MDOScenario execution (time: 0:00:00.017970) ***
INFO - 08:37:26: ... 86%|████████▌ | 6/7 [00:00<00:00, 14.44 it/sec, obj=-4.51e+3]
INFO - 08:37:26:
INFO - 08:37:26: *** Start MDOScenario execution ***
INFO - 08:37:26: MDOScenario
INFO - 08:37:26: Disciplines: Aerodynamics Mission
INFO - 08:37:26: MDO formulation: DisciplinaryOpt
INFO - 08:37:26: Optimization problem:
INFO - 08:37:26: minimize -range(thick_airfoils)
INFO - 08:37:26: with respect to thick_airfoils
INFO - 08:37:26: subject to constraints:
INFO - 08:37:26: lift(thick_airfoils) == 0.5
INFO - 08:37:26: over the design space:
INFO - 08:37:26: +----------------+-------------+-------+-------------+-------+
INFO - 08:37:26: | name | lower_bound | value | upper_bound | type |
INFO - 08:37:26: +----------------+-------------+-------+-------------+-------+
INFO - 08:37:26: | thick_airfoils | 5 | 5 | 25 | float |
INFO - 08:37:26: +----------------+-------------+-------+-------------+-------+
INFO - 08:37:26: Solving optimization problem with algorithm NLOPT_SLSQP:
INFO - 08:37:26: ... 0%| | 0/5 [00:00<?, ?it]
INFO - 08:37:26:
INFO - 08:37:26: ... 20%|██ | 1/5 [00:00<00:00, 852.85 it/sec, obj=-4.51e+3]
INFO - 08:37:26:
INFO - 08:37:26: ... 40%|████ | 2/5 [00:00<00:00, 255.88 it/sec, obj=-4.48e+3]
INFO - 08:37:26:
INFO - 08:37:26: ... 60%|██████ | 3/5 [00:00<00:00, 367.98 it/sec, obj=-4.51e+3]
INFO - 08:37:26:
INFO - 08:37:26: ... 80%|████████ | 4/5 [00:00<00:00, 380.31 it/sec, obj=-4.51e+3]
INFO - 08:37:26:
INFO - 08:37:26: ... 100%|██████████| 5/5 [00:00<00:00, 379.53 it/sec, obj=-4.51e+3]
INFO - 08:37:26:
INFO - 08:37:26:
INFO - 08:37:26: Optimization result:
INFO - 08:37:26: Optimizer info:
INFO - 08:37:26: Status: None
INFO - 08:37:26: Message: Maximum number of iterations reached. GEMSEO Stopped the driver
INFO - 08:37:26: Number of calls to the objective function by the optimizer: 7
INFO - 08:37:26: Solution:
INFO - 08:37:26: The solution is feasible.
INFO - 08:37:26: Objective: -4509.519641910688
INFO - 08:37:26: Standardized constraints:
INFO - 08:37:26: lift - 0.5 = -0.0001369125221327705
INFO - 08:37:26: Design space:
INFO - 08:37:26: +----------------+-------------+-------+-------------+-------+
INFO - 08:37:26: | name | lower_bound | value | upper_bound | type |
INFO - 08:37:26: +----------------+-------------+-------+-------------+-------+
INFO - 08:37:26: | thick_airfoils | 5 | 5 | 25 | float |
INFO - 08:37:26: +----------------+-------------+-------+-------------+-------+
INFO - 08:37:26: *** End MDOScenario execution (time: 0:00:00.027257) ***
INFO - 08:37:26:
INFO - 08:37:26: *** Start MDOScenario execution ***
INFO - 08:37:26: MDOScenario
INFO - 08:37:26: Disciplines: Mission Structure
INFO - 08:37:26: MDO formulation: DisciplinaryOpt
INFO - 08:37:26: Optimization problem:
INFO - 08:37:26: minimize -range(thick_panels)
INFO - 08:37:26: with respect to thick_panels
INFO - 08:37:26: subject to constraints:
INFO - 08:37:26: reserve_fact(thick_panels) <= 0.5
INFO - 08:37:26: over the design space:
INFO - 08:37:26: +--------------+-------------+-------------------+-------------+-------+
INFO - 08:37:26: | name | lower_bound | value | upper_bound | type |
INFO - 08:37:26: +--------------+-------------+-------------------+-------------+-------+
INFO - 08:37:26: | thick_panels | 1 | 3.264536835170201 | 20 | float |
INFO - 08:37:26: +--------------+-------------+-------------------+-------------+-------+
INFO - 08:37:26: Solving optimization problem with algorithm NLOPT_SLSQP:
INFO - 08:37:26: ... 0%| | 0/5 [00:00<?, ?it]
INFO - 08:37:26:
INFO - 08:37:26: ... 20%|██ | 1/5 [00:00<00:00, 1018.78 it/sec, obj=-4.51e+3]
INFO - 08:37:26:
INFO - 08:37:26: ... 40%|████ | 2/5 [00:00<00:00, 249.33 it/sec, obj=-4.51e+3]
INFO - 08:37:26:
INFO - 08:37:26: ... 60%|██████ | 3/5 [00:00<00:00, 271.67 it/sec, obj=-4.51e+3]
INFO - 08:37:26:
INFO - 08:37:26: ... 80%|████████ | 4/5 [00:00<00:00, 351.69 it/sec, obj=-4.51e+3]
INFO - 08:37:26:
INFO - 08:37:26:
INFO - 08:37:26: Optimization result:
INFO - 08:37:26: Optimizer info:
INFO - 08:37:26: Status: None
INFO - 08:37:26: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO Stopped the driver
INFO - 08:37:26: Number of calls to the objective function by the optimizer: 5
INFO - 08:37:26: Solution:
INFO - 08:37:26: The solution is feasible.
INFO - 08:37:26: Objective: -4509.583287354345
INFO - 08:37:26: Standardized constraints:
INFO - 08:37:26: reserve_fact - 0.5 = 3.0278073381850845e-08
INFO - 08:37:26: Design space:
INFO - 08:37:26: +--------------+-------------+-------------------+-------------+-------+
INFO - 08:37:26: | name | lower_bound | value | upper_bound | type |
INFO - 08:37:26: +--------------+-------------+-------------------+-------------+-------+
INFO - 08:37:26: | thick_panels | 1 | 3.225021421746108 | 20 | float |
INFO - 08:37:26: +--------------+-------------+-------------------+-------------+-------+
INFO - 08:37:26: *** End MDOScenario execution (time: 0:00:00.023639) ***
INFO - 08:37:26: ... 100%|██████████| 7/7 [00:00<00:00, 14.36 it/sec, obj=-4.51e+3]
INFO - 08:37:26: Optimization result:
INFO - 08:37:26: Optimizer info:
INFO - 08:37:26: Status: None
INFO - 08:37:26: Message: Maximum number of iterations reached. GEMSEO Stopped the driver
INFO - 08:37:26: Number of calls to the objective function by the optimizer: 9
INFO - 08:37:26: Solution:
INFO - 08:37:26: The solution is feasible.
INFO - 08:37:26: Objective: -4509.243708600623
INFO - 08:37:26: Standardized constraints:
INFO - 08:37:26: lift - 0.5 = 5.903055821931957e-13
INFO - 08:37:26: reserve_fact - 0.5 = -0.2599999989201578
INFO - 08:37:26: Design space:
INFO - 08:37:26: +-------+-------------+-------+-------------+-------+
INFO - 08:37:26: | name | lower_bound | value | upper_bound | type |
INFO - 08:37:26: +-------+-------------+-------+-------------+-------+
INFO - 08:37:26: | sweep | 10 | 25 | 35 | float |
INFO - 08:37:26: +-------+-------------+-------+-------------+-------+
INFO - 08:37:26: *** End MDOScenario execution (time: 0:00:00.501726) ***
WARNING - 08:37:27: Failed to create Hessian approximation.
Traceback (most recent call last):
File "/home/docs/checkouts/readthedocs.org/user_builds/gemseo/envs/5.0.1/lib/python3.9/site-packages/gemseo/post/opt_history_view.py", line 621, in _create_hessian_approx_plot
_, diag, _, _ = SR1Approx(history).build_approximation(
File "/home/docs/checkouts/readthedocs.org/user_builds/gemseo/envs/5.0.1/lib/python3.9/site-packages/gemseo/post/core/hessians.py", line 379, in build_approximation
x_hist, grad_hist, _, _ = self.get_x_grad_history(
File "/home/docs/checkouts/readthedocs.org/user_builds/gemseo/envs/5.0.1/lib/python3.9/site-packages/gemseo/post/core/hessians.py", line 170, in get_x_grad_history
raise ValueError(
ValueError: Cannot build approximation for function: -range because its gradient history is too small: 0.
<gemseo.post.opt_history_view.OptHistoryView object at 0x7f873b76c940>
Total running time of the script: ( 0 minutes 3.251 seconds)