Note
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MDO formulations for a toy example in aerostructure¶
from __future__ import annotations
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,
"MDF",
"range",
design_space,
maximize_objective=True,
)
scenario.add_constraint("reserve_fact", constraint_type="ineq", value=0.5)
scenario.add_constraint("lift", 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/5.3.1/lib/python3.9/site-packages/gemseo/algos/design_space.py:468: ComplexWarning: Casting complex values to real discards the imaginary part
self.__current_value[name] = array_value.astype(
INFO - 08:59:23: Variable reserve_fact was removed from the Design Space, it is not an input of any discipline.
INFO - 08:59:23:
INFO - 08:59:23: *** Start MDOScenario execution ***
INFO - 08:59:23: MDOScenario
INFO - 08:59:23: Disciplines: Aerodynamics Mission Structure
INFO - 08:59:23: MDO formulation: MDF
INFO - 08:59:23: Optimization problem:
INFO - 08:59:23: minimize -range(thick_airfoils, thick_panels, sweep)
INFO - 08:59:23: with respect to sweep, thick_airfoils, thick_panels
INFO - 08:59:23: subject to constraints:
INFO - 08:59:23: reserve_fact(thick_airfoils, thick_panels, sweep) <= 0.5
INFO - 08:59:23: lift(thick_airfoils, thick_panels, sweep) == 0.5
INFO - 08:59:23: over the design space:
INFO - 08:59:23: +----------------+-------------+-------+-------------+-------+
INFO - 08:59:23: | Name | Lower bound | Value | Upper bound | Type |
INFO - 08:59:23: +----------------+-------------+-------+-------------+-------+
INFO - 08:59:23: | thick_airfoils | 5 | 15 | 25 | float |
INFO - 08:59:23: | thick_panels | 1 | 3 | 20 | float |
INFO - 08:59:23: | sweep | 10 | 25 | 35 | float |
INFO - 08:59:23: +----------------+-------------+-------+-------------+-------+
INFO - 08:59:23: Solving optimization problem with algorithm NLOPT_SLSQP:
INFO - 08:59:23: 10%|█ | 1/10 [00:00<00:00, 31.71 it/sec, obj=-4.25e+3]
INFO - 08:59:23: 20%|██ | 2/10 [00:00<00:00, 11.52 it/sec, obj=-4.51e+3]
INFO - 08:59:23: 30%|███ | 3/10 [00:00<00:00, 13.38 it/sec, obj=-4.51e+3]
INFO - 08:59:23: 40%|████ | 4/10 [00:00<00:00, 17.77 it/sec, obj=Not evaluated]
INFO - 08:59:23: Optimization result:
INFO - 08:59:23: Optimizer info:
INFO - 08:59:23: Status: None
INFO - 08:59:23: Message: Successive iterates of the design variables are closer than xtol_rel or xtol_abs. GEMSEO Stopped the driver
INFO - 08:59:23: Number of calls to the objective function by the optimizer: 4
INFO - 08:59:23: Solution:
INFO - 08:59:23: The solution is feasible.
INFO - 08:59:23: Objective: -4509.505446993421
INFO - 08:59:23: Standardized constraints:
INFO - 08:59:23: [lift-0.5] = 8.926193117986259e-14
INFO - 08:59:23: [reserve_fact-0.5] = 6.522076034798374e-08
INFO - 08:59:23: Design space:
INFO - 08:59:23: +----------------+-------------+-------------------+-------------+-------+
INFO - 08:59:23: | Name | Lower bound | Value | Upper bound | Type |
INFO - 08:59:23: +----------------+-------------+-------------------+-------------+-------+
INFO - 08:59:23: | thick_airfoils | 5 | 5 | 25 | float |
INFO - 08:59:23: | thick_panels | 1 | 3.22558921528402 | 20 | float |
INFO - 08:59:23: | sweep | 10 | 24.99326599158099 | 35 | float |
INFO - 08:59:23: +----------------+-------------+-------------------+-------------+-------+
INFO - 08:59:23: *** End MDOScenario execution (time: 0:00:00.241946) ***
<gemseo.post.opt_history_view.OptHistoryView object at 0x7f8ae8b30880>
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/5.3.1/lib/python3.9/site-packages/gemseo/algos/design_space.py:468: 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.
aero_scenario = create_scenario(
[aerodynamics, mission],
"DisciplinaryOpt",
"range",
design_space_ref.filter(["thick_airfoils"], copy=True),
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.
struct_scenario = create_scenario(
[structure, mission],
"DisciplinaryOpt",
"range",
design_space_ref.filter(["thick_panels"], copy=True),
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 = design_space_ref.filter(["sweep"], copy=True)
system_scenario = create_scenario(
[aero_scenario, struct_scenario, mission],
"BiLevel",
"range",
design_space_system,
maximize_objective=True,
inner_mda_name="MDAJacobi",
tolerance=1e-8,
)
system_scenario.add_constraint("reserve_fact", constraint_type="ineq", value=0.5)
system_scenario.add_constraint("lift", 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 - 08:59:25:
INFO - 08:59:25: *** Start MDOScenario execution ***
INFO - 08:59:25: MDOScenario
INFO - 08:59:25: Disciplines: MDOScenario MDOScenario Mission
INFO - 08:59:25: MDO formulation: BiLevel
INFO - 08:59:25: Optimization problem:
INFO - 08:59:25: minimize -range(sweep)
INFO - 08:59:25: with respect to sweep
INFO - 08:59:25: subject to constraints:
INFO - 08:59:25: reserve_fact(sweep) <= 0.5
INFO - 08:59:25: lift(sweep) == 0.5
INFO - 08:59:25: over the design space:
INFO - 08:59:25: +-------+-------------+-------+-------------+-------+
INFO - 08:59:25: | Name | Lower bound | Value | Upper bound | Type |
INFO - 08:59:25: +-------+-------------+-------+-------------+-------+
INFO - 08:59:25: | sweep | 10 | 25 | 35 | float |
INFO - 08:59:25: +-------+-------------+-------+-------------+-------+
INFO - 08:59:25: Solving optimization problem with algorithm NLOPT_COBYLA:
INFO - 08:59:25:
INFO - 08:59:25: *** Start MDOScenario execution ***
INFO - 08:59:25: MDOScenario
INFO - 08:59:25: Disciplines: Aerodynamics Mission
INFO - 08:59:25: MDO formulation: DisciplinaryOpt
INFO - 08:59:25: Optimization problem:
INFO - 08:59:25: minimize -range(thick_airfoils)
INFO - 08:59:25: with respect to thick_airfoils
INFO - 08:59:25: subject to constraints:
INFO - 08:59:25: lift(thick_airfoils) == 0.5
INFO - 08:59:25: over the design space:
INFO - 08:59:25: +----------------+-------------+-------+-------------+-------+
INFO - 08:59:25: | Name | Lower bound | Value | Upper bound | Type |
INFO - 08:59:25: +----------------+-------------+-------+-------------+-------+
INFO - 08:59:25: | thick_airfoils | 5 | 15 | 25 | float |
INFO - 08:59:25: +----------------+-------------+-------+-------------+-------+
INFO - 08:59:25: Solving optimization problem with algorithm NLOPT_SLSQP:
INFO - 08:59:25: 20%|██ | 1/5 [00:00<00:00, 142.18 it/sec, obj=-4.27e+3]
WARNING - 08:59:25: Optimization found no feasible point ! The least infeasible point is selected.
INFO - 08:59:25: 40%|████ | 2/5 [00:00<00:00, 144.70 it/sec, obj=-4.51e+3]
INFO - 08:59:25: Optimization result:
INFO - 08:59:25: Optimizer info:
INFO - 08:59:25: Status: 5
INFO - 08:59:25: Message: NLOPT_MAXEVAL_REACHED: Optimization stopped because maxeval (above) was reached
INFO - 08:59:25: Number of calls to the objective function by the optimizer: 8
INFO - 08:59:25: Solution:
WARNING - 08:59:25: The solution is not feasible.
INFO - 08:59:25: Objective: -4513.429203824652
INFO - 08:59:25: Standardized constraints:
INFO - 08:59:25: [lift-0.5] = 0.008666666666666822
INFO - 08:59:25: Design space:
INFO - 08:59:25: +----------------+-------------+-------+-------------+-------+
INFO - 08:59:25: | Name | Lower bound | Value | Upper bound | Type |
INFO - 08:59:25: +----------------+-------------+-------+-------------+-------+
INFO - 08:59:25: | thick_airfoils | 5 | 5 | 25 | float |
INFO - 08:59:25: +----------------+-------------+-------+-------------+-------+
INFO - 08:59:25: *** End MDOScenario execution (time: 0:00:00.029568) ***
INFO - 08:59:25:
INFO - 08:59:25: *** Start MDOScenario execution ***
INFO - 08:59:25: MDOScenario
INFO - 08:59:25: Disciplines: Mission Structure
INFO - 08:59:25: MDO formulation: DisciplinaryOpt
INFO - 08:59:25: Optimization problem:
INFO - 08:59:25: minimize -range(thick_panels)
INFO - 08:59:25: with respect to thick_panels
INFO - 08:59:25: subject to constraints:
INFO - 08:59:25: reserve_fact(thick_panels) <= 0.5
INFO - 08:59:25: over the design space:
INFO - 08:59:25: +--------------+-------------+-------+-------------+-------+
INFO - 08:59:25: | Name | Lower bound | Value | Upper bound | Type |
INFO - 08:59:25: +--------------+-------------+-------+-------------+-------+
INFO - 08:59:25: | thick_panels | 1 | 3 | 20 | float |
INFO - 08:59:25: +--------------+-------------+-------+-------------+-------+
INFO - 08:59:25: Solving optimization problem with algorithm NLOPT_SLSQP:
INFO - 08:59:25: 20%|██ | 1/5 [00:00<00:00, 166.12 it/sec, obj=-4.51e+3]
ERROR - 08:59:25: NLopt run failed: NLopt roundoff-limited, RoundoffLimited
Traceback (most recent call last):
File "/home/docs/checkouts/readthedocs.org/user_builds/gemseo/envs/5.3.1/lib/python3.9/site-packages/gemseo/algos/opt/lib_nlopt.py", line 498, in _run
nlopt_problem.optimize(x_0.real)
File "/home/docs/checkouts/readthedocs.org/user_builds/gemseo/envs/5.3.1/lib/python3.9/site-packages/nlopt/nlopt.py", line 335, in optimize
return _nlopt.opt_optimize(self, *args)
nlopt.RoundoffLimited: NLopt roundoff-limited
INFO - 08:59:25: 40%|████ | 2/5 [00:00<00:00, 161.47 it/sec, obj=-4.5e+3]
INFO - 08:59:25: Optimization result:
INFO - 08:59:25: Optimizer info:
INFO - 08:59:25: Status: None
INFO - 08:59:25: Message: GEMSEO Stopped the driver
INFO - 08:59:25: Number of calls to the objective function by the optimizer: 3
INFO - 08:59:25: Solution:
INFO - 08:59:25: The solution is feasible.
INFO - 08:59:25: Objective: -4504.955637332531
INFO - 08:59:25: Standardized constraints:
INFO - 08:59:25: [reserve_fact-0.5] = 1.062133492268913e-09
INFO - 08:59:25: Design space:
INFO - 08:59:25: +--------------+-------------+-------------------+-------------+-------+
INFO - 08:59:25: | Name | Lower bound | Value | Upper bound | Type |
INFO - 08:59:25: +--------------+-------------+-------------------+-------------+-------+
INFO - 08:59:25: | thick_panels | 1 | 3.266666666489645 | 20 | float |
INFO - 08:59:25: +--------------+-------------+-------------------+-------------+-------+
INFO - 08:59:25: *** End MDOScenario execution (time: 0:00:00.028562) ***
INFO - 08:59:25: 14%|█▍ | 1/7 [00:00<00:00, 8.01 it/sec, obj=-4.51e+3]
INFO - 08:59:25:
INFO - 08:59:25: *** Start MDOScenario execution ***
INFO - 08:59:25: MDOScenario
INFO - 08:59:25: Disciplines: Aerodynamics Mission
INFO - 08:59:25: MDO formulation: DisciplinaryOpt
INFO - 08:59:25: Optimization problem:
INFO - 08:59:25: minimize -range(thick_airfoils)
INFO - 08:59:25: with respect to thick_airfoils
INFO - 08:59:25: subject to constraints:
INFO - 08:59:25: lift(thick_airfoils) == 0.5
INFO - 08:59:25: over the design space:
INFO - 08:59:25: +----------------+-------------+-------+-------------+-------+
INFO - 08:59:25: | Name | Lower bound | Value | Upper bound | Type |
INFO - 08:59:25: +----------------+-------------+-------+-------------+-------+
INFO - 08:59:25: | thick_airfoils | 5 | 5 | 25 | float |
INFO - 08:59:25: +----------------+-------------+-------+-------------+-------+
INFO - 08:59:25: Solving optimization problem with algorithm NLOPT_SLSQP:
INFO - 08:59:25: 20%|██ | 1/5 [00:00<00:00, 804.74 it/sec, obj=-4.27e+3]
WARNING - 08:59:25: Optimization found no feasible point ! The least infeasible point is selected.
INFO - 08:59:25: Optimization result:
INFO - 08:59:25: Optimizer info:
INFO - 08:59:25: Status: 5
INFO - 08:59:25: Message: NLOPT_MAXEVAL_REACHED: Optimization stopped because maxeval (above) was reached
INFO - 08:59:25: Number of calls to the objective function by the optimizer: 8
INFO - 08:59:25: Solution:
WARNING - 08:59:25: The solution is not feasible.
INFO - 08:59:25: Objective: -4267.910320106268
INFO - 08:59:25: Standardized constraints:
INFO - 08:59:25: [lift-0.5] = 0.12708333333392374
INFO - 08:59:25: Design space:
INFO - 08:59:25: +----------------+-------------+-------+-------------+-------+
INFO - 08:59:25: | Name | Lower bound | Value | Upper bound | Type |
INFO - 08:59:25: +----------------+-------------+-------+-------------+-------+
INFO - 08:59:25: | thick_airfoils | 5 | 5 | 25 | float |
INFO - 08:59:25: +----------------+-------------+-------+-------------+-------+
INFO - 08:59:25: *** End MDOScenario execution (time: 0:00:00.017988) ***
INFO - 08:59:25:
INFO - 08:59:25: *** Start MDOScenario execution ***
INFO - 08:59:25: MDOScenario
INFO - 08:59:25: Disciplines: Mission Structure
INFO - 08:59:25: MDO formulation: DisciplinaryOpt
INFO - 08:59:25: Optimization problem:
INFO - 08:59:25: minimize -range(thick_panels)
INFO - 08:59:25: with respect to thick_panels
INFO - 08:59:25: subject to constraints:
INFO - 08:59:25: reserve_fact(thick_panels) <= 0.5
INFO - 08:59:25: over the design space:
INFO - 08:59:25: +--------------+-------------+-------------------+-------------+-------+
INFO - 08:59:25: | Name | Lower bound | Value | Upper bound | Type |
INFO - 08:59:25: +--------------+-------------+-------------------+-------------+-------+
INFO - 08:59:25: | thick_panels | 1 | 3.266666666489645 | 20 | float |
INFO - 08:59:25: +--------------+-------------+-------------------+-------------+-------+
INFO - 08:59:25: Solving optimization problem with algorithm NLOPT_SLSQP:
INFO - 08:59:25: 20%|██ | 1/5 [00:00<00:00, 883.94 it/sec, obj=-4.27e+3]
ERROR - 08:59:25: NLopt run failed: NLopt roundoff-limited, RoundoffLimited
Traceback (most recent call last):
File "/home/docs/checkouts/readthedocs.org/user_builds/gemseo/envs/5.3.1/lib/python3.9/site-packages/gemseo/algos/opt/lib_nlopt.py", line 498, in _run
nlopt_problem.optimize(x_0.real)
File "/home/docs/checkouts/readthedocs.org/user_builds/gemseo/envs/5.3.1/lib/python3.9/site-packages/nlopt/nlopt.py", line 335, in optimize
return _nlopt.opt_optimize(self, *args)
nlopt.RoundoffLimited: NLopt roundoff-limited
INFO - 08:59:25: 40%|████ | 2/5 [00:00<00:00, 298.23 it/sec, obj=-4.27e+3]
INFO - 08:59:25: Optimization result:
INFO - 08:59:25: Optimizer info:
INFO - 08:59:25: Status: None
INFO - 08:59:25: Message: GEMSEO Stopped the driver
INFO - 08:59:25: Number of calls to the objective function by the optimizer: 3
INFO - 08:59:25: Solution:
INFO - 08:59:25: The solution is feasible.
INFO - 08:59:25: Objective: -4270.047650043281
INFO - 08:59:25: Standardized constraints:
INFO - 08:59:25: [reserve_fact-0.5] = 3.0379254667423083e-10
INFO - 08:59:25: Design space:
INFO - 08:59:25: +--------------+-------------+------------------+-------------+-------+
INFO - 08:59:25: | Name | Lower bound | Value | Upper bound | Type |
INFO - 08:59:25: +--------------+-------------+------------------+-------------+-------+
INFO - 08:59:25: | thick_panels | 1 | 1.76499999995232 | 20 | float |
INFO - 08:59:25: +--------------+-------------+------------------+-------------+-------+
INFO - 08:59:25: *** End MDOScenario execution (time: 0:00:00.019800) ***
INFO - 08:59:25: 29%|██▊ | 2/7 [00:00<00:00, 11.01 it/sec, obj=-4.27e+3]
INFO - 08:59:25:
INFO - 08:59:25: *** Start MDOScenario execution ***
INFO - 08:59:25: MDOScenario
INFO - 08:59:25: Disciplines: Aerodynamics Mission
INFO - 08:59:25: MDO formulation: DisciplinaryOpt
INFO - 08:59:25: Optimization problem:
INFO - 08:59:25: minimize -range(thick_airfoils)
INFO - 08:59:25: with respect to thick_airfoils
INFO - 08:59:25: subject to constraints:
INFO - 08:59:25: lift(thick_airfoils) == 0.5
INFO - 08:59:25: over the design space:
INFO - 08:59:25: +----------------+-------------+-------+-------------+-------+
INFO - 08:59:25: | Name | Lower bound | Value | Upper bound | Type |
INFO - 08:59:25: +----------------+-------------+-------+-------------+-------+
INFO - 08:59:25: | thick_airfoils | 5 | 5 | 25 | float |
INFO - 08:59:25: +----------------+-------------+-------+-------------+-------+
INFO - 08:59:25: Solving optimization problem with algorithm NLOPT_SLSQP:
INFO - 08:59:25: 20%|██ | 1/5 [00:00<00:00, 678.03 it/sec, obj=-4.53e+3]
INFO - 08:59:25: 40%|████ | 2/5 [00:00<00:00, 266.87 it/sec, obj=-3.83e+3]
INFO - 08:59:25: 60%|██████ | 3/5 [00:00<00:00, 382.31 it/sec, obj=-4.43e+3]
INFO - 08:59:25: 80%|████████ | 4/5 [00:00<00:00, 415.34 it/sec, obj=-4.5e+3]
INFO - 08:59:25: 100%|██████████| 5/5 [00:00<00:00, 435.64 it/sec, obj=-4.51e+3]
WARNING - 08:59:25: Optimization found no feasible point ! The least infeasible point is selected.
INFO - 08:59:25: Optimization result:
INFO - 08:59:25: Optimizer info:
INFO - 08:59:25: Status: None
INFO - 08:59:25: Message: Maximum number of iterations reached. GEMSEO Stopped the driver
INFO - 08:59:25: Number of calls to the objective function by the optimizer: 7
INFO - 08:59:25: Solution:
WARNING - 08:59:25: The solution is not feasible.
INFO - 08:59:25: Objective: -3831.807218266315
INFO - 08:59:25: Standardized constraints:
INFO - 08:59:25: [lift-0.5] = -0.0023374064679561046
INFO - 08:59:25: Design space:
INFO - 08:59:25: +----------------+-------------+-------+-------------+-------+
INFO - 08:59:25: | Name | Lower bound | Value | Upper bound | Type |
INFO - 08:59:25: +----------------+-------------+-------+-------------+-------+
INFO - 08:59:25: | thick_airfoils | 5 | 25 | 25 | float |
INFO - 08:59:25: +----------------+-------------+-------+-------------+-------+
INFO - 08:59:25: *** End MDOScenario execution (time: 0:00:00.025873) ***
INFO - 08:59:25:
INFO - 08:59:25: *** Start MDOScenario execution ***
INFO - 08:59:25: MDOScenario
INFO - 08:59:25: Disciplines: Mission Structure
INFO - 08:59:25: MDO formulation: DisciplinaryOpt
INFO - 08:59:25: Optimization problem:
INFO - 08:59:25: minimize -range(thick_panels)
INFO - 08:59:25: with respect to thick_panels
INFO - 08:59:25: subject to constraints:
INFO - 08:59:25: reserve_fact(thick_panels) <= 0.5
INFO - 08:59:25: over the design space:
INFO - 08:59:25: +--------------+-------------+------------------+-------------+-------+
INFO - 08:59:25: | Name | Lower bound | Value | Upper bound | Type |
INFO - 08:59:25: +--------------+-------------+------------------+-------------+-------+
INFO - 08:59:25: | thick_panels | 1 | 1.76499999995232 | 20 | float |
INFO - 08:59:25: +--------------+-------------+------------------+-------------+-------+
INFO - 08:59:25: Solving optimization problem with algorithm NLOPT_SLSQP:
INFO - 08:59:25: 20%|██ | 1/5 [00:00<00:00, 677.05 it/sec, obj=-3.82e+3]
INFO - 08:59:25: 40%|████ | 2/5 [00:00<00:00, 254.22 it/sec, obj=-3.82e+3]
INFO - 08:59:25: 60%|██████ | 3/5 [00:00<00:00, 280.77 it/sec, obj=-3.82e+3]
INFO - 08:59:25: 80%|████████ | 4/5 [00:00<00:00, 363.65 it/sec, obj=-3.82e+3]
INFO - 08:59:25: Optimization result:
INFO - 08:59:25: Optimizer info:
INFO - 08:59:25: Status: None
INFO - 08:59:25: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO Stopped the driver
INFO - 08:59:25: Number of calls to the objective function by the optimizer: 5
INFO - 08:59:25: Solution:
INFO - 08:59:25: The solution is feasible.
INFO - 08:59:25: Objective: -3818.5902855979184
INFO - 08:59:25: Standardized constraints:
INFO - 08:59:25: [reserve_fact-0.5] = 3.0950531026974204e-09
INFO - 08:59:25: Design space:
INFO - 08:59:25: +--------------+-------------+-------------------+-------------+-------+
INFO - 08:59:25: | Name | Lower bound | Value | Upper bound | Type |
INFO - 08:59:25: +--------------+-------------+-------------------+-------------+-------+
INFO - 08:59:25: | thick_panels | 1 | 3.414591822343108 | 20 | float |
INFO - 08:59:25: +--------------+-------------+-------------------+-------------+-------+
INFO - 08:59:25: *** End MDOScenario execution (time: 0:00:00.024850) ***
INFO - 08:59:25: 43%|████▎ | 3/7 [00:00<00:00, 11.83 it/sec, obj=-3.82e+3]
INFO - 08:59:25:
INFO - 08:59:25: *** Start MDOScenario execution ***
INFO - 08:59:25: MDOScenario
INFO - 08:59:25: Disciplines: Aerodynamics Mission
INFO - 08:59:25: MDO formulation: DisciplinaryOpt
INFO - 08:59:25: Optimization problem:
INFO - 08:59:25: minimize -range(thick_airfoils)
INFO - 08:59:25: with respect to thick_airfoils
INFO - 08:59:25: subject to constraints:
INFO - 08:59:25: lift(thick_airfoils) == 0.5
INFO - 08:59:25: over the design space:
INFO - 08:59:25: +----------------+-------------+-------+-------------+-------+
INFO - 08:59:25: | Name | Lower bound | Value | Upper bound | Type |
INFO - 08:59:25: +----------------+-------------+-------+-------------+-------+
INFO - 08:59:25: | thick_airfoils | 5 | 25 | 25 | float |
INFO - 08:59:25: +----------------+-------------+-------+-------------+-------+
INFO - 08:59:25: Solving optimization problem with algorithm NLOPT_SLSQP:
INFO - 08:59:25: 20%|██ | 1/5 [00:00<00:00, 705.76 it/sec, obj=-3.82e+3]
WARNING - 08:59:25: Optimization found no feasible point ! The least infeasible point is selected.
INFO - 08:59:25: 40%|████ | 2/5 [00:00<00:00, 267.30 it/sec, obj=-4.49e+3]
INFO - 08:59:25: Optimization result:
INFO - 08:59:25: Optimizer info:
INFO - 08:59:25: Status: 5
INFO - 08:59:25: Message: NLOPT_MAXEVAL_REACHED: Optimization stopped because maxeval (above) was reached
INFO - 08:59:25: Number of calls to the objective function by the optimizer: 8
INFO - 08:59:25: Solution:
WARNING - 08:59:25: The solution is not feasible.
INFO - 08:59:25: Objective: -4490.540174494246
INFO - 08:59:25: Standardized constraints:
INFO - 08:59:25: [lift-0.5] = 0.00918103190667341
INFO - 08:59:25: Design space:
INFO - 08:59:25: +----------------+-------------+-------+-------------+-------+
INFO - 08:59:25: | Name | Lower bound | Value | Upper bound | Type |
INFO - 08:59:25: +----------------+-------------+-------+-------------+-------+
INFO - 08:59:25: | thick_airfoils | 5 | 5 | 25 | float |
INFO - 08:59:25: +----------------+-------------+-------+-------------+-------+
INFO - 08:59:25: *** End MDOScenario execution (time: 0:00:00.020886) ***
INFO - 08:59:25:
INFO - 08:59:25: *** Start MDOScenario execution ***
INFO - 08:59:25: MDOScenario
INFO - 08:59:25: Disciplines: Mission Structure
INFO - 08:59:25: MDO formulation: DisciplinaryOpt
INFO - 08:59:25: Optimization problem:
INFO - 08:59:25: minimize -range(thick_panels)
INFO - 08:59:25: with respect to thick_panels
INFO - 08:59:25: subject to constraints:
INFO - 08:59:25: reserve_fact(thick_panels) <= 0.5
INFO - 08:59:25: over the design space:
INFO - 08:59:25: +--------------+-------------+-------------------+-------------+-------+
INFO - 08:59:25: | Name | Lower bound | Value | Upper bound | Type |
INFO - 08:59:25: +--------------+-------------+-------------------+-------------+-------+
INFO - 08:59:25: | thick_panels | 1 | 3.414591822343108 | 20 | float |
INFO - 08:59:25: +--------------+-------------+-------------------+-------------+-------+
INFO - 08:59:25: Solving optimization problem with algorithm NLOPT_SLSQP:
INFO - 08:59:25: 20%|██ | 1/5 [00:00<00:00, 678.80 it/sec, obj=-4.5e+3]
INFO - 08:59:25: 40%|████ | 2/5 [00:00<00:00, 252.49 it/sec, obj=-4.5e+3]
INFO - 08:59:25: 60%|██████ | 3/5 [00:00<00:00, 279.96 it/sec, obj=-4.5e+3]
INFO - 08:59:25: 80%|████████ | 4/5 [00:00<00:00, 362.41 it/sec, obj=-4.5e+3]
INFO - 08:59:25: Optimization result:
INFO - 08:59:25: Optimizer info:
INFO - 08:59:25: Status: None
INFO - 08:59:25: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO Stopped the driver
INFO - 08:59:25: Number of calls to the objective function by the optimizer: 5
INFO - 08:59:25: Solution:
INFO - 08:59:25: The solution is feasible.
INFO - 08:59:25: Objective: -4503.594576639364
INFO - 08:59:25: Standardized constraints:
INFO - 08:59:25: [reserve_fact-0.5] = 2.4330390147042635e-08
INFO - 08:59:25: Design space:
INFO - 08:59:25: +--------------+-------------+-------------------+-------------+-------+
INFO - 08:59:25: | Name | Lower bound | Value | Upper bound | Type |
INFO - 08:59:25: +--------------+-------------+-------------------+-------------+-------+
INFO - 08:59:25: | thick_panels | 1 | 3.256301554313449 | 20 | float |
INFO - 08:59:25: +--------------+-------------+-------------------+-------------+-------+
INFO - 08:59:25: *** End MDOScenario execution (time: 0:00:00.025651) ***
INFO - 08:59:25: 57%|█████▋ | 4/7 [00:00<00:00, 12.50 it/sec, obj=-4.51e+3]
INFO - 08:59:25:
INFO - 08:59:25: *** Start MDOScenario execution ***
INFO - 08:59:25: MDOScenario
INFO - 08:59:25: Disciplines: Aerodynamics Mission
INFO - 08:59:25: MDO formulation: DisciplinaryOpt
INFO - 08:59:25: Optimization problem:
INFO - 08:59:25: minimize -range(thick_airfoils)
INFO - 08:59:25: with respect to thick_airfoils
INFO - 08:59:25: subject to constraints:
INFO - 08:59:25: lift(thick_airfoils) == 0.5
INFO - 08:59:25: over the design space:
INFO - 08:59:25: +----------------+-------------+-------+-------------+-------+
INFO - 08:59:25: | Name | Lower bound | Value | Upper bound | Type |
INFO - 08:59:25: +----------------+-------------+-------+-------------+-------+
INFO - 08:59:25: | thick_airfoils | 5 | 5 | 25 | float |
INFO - 08:59:25: +----------------+-------------+-------+-------------+-------+
INFO - 08:59:25: Solving optimization problem with algorithm NLOPT_SLSQP:
INFO - 08:59:25: 20%|██ | 1/5 [00:00<00:00, 670.55 it/sec, obj=-4.51e+3]
INFO - 08:59:25: 40%|████ | 2/5 [00:00<00:00, 269.80 it/sec, obj=-3.85e+3]
INFO - 08:59:25: 60%|██████ | 3/5 [00:00<00:00, 387.33 it/sec, obj=-4.48e+3]
INFO - 08:59:25: 80%|████████ | 4/5 [00:00<00:00, 401.52 it/sec, obj=-4.51e+3]
INFO - 08:59:25: 100%|██████████| 5/5 [00:00<00:00, 411.75 it/sec, obj=-4.51e+3]
INFO - 08:59:25: Optimization result:
INFO - 08:59:25: Optimizer info:
INFO - 08:59:25: Status: None
INFO - 08:59:25: Message: Maximum number of iterations reached. GEMSEO Stopped the driver
INFO - 08:59:25: Number of calls to the objective function by the optimizer: 7
INFO - 08:59:25: Solution:
INFO - 08:59:25: The solution is feasible.
INFO - 08:59:25: Objective: -3854.082002804953
INFO - 08:59:25: Standardized constraints:
INFO - 08:59:25: [lift-0.5] = 0.0
INFO - 08:59:25: Design space:
INFO - 08:59:25: +----------------+-------------+-------------------+-------------+-------+
INFO - 08:59:25: | Name | Lower bound | Value | Upper bound | Type |
INFO - 08:59:25: +----------------+-------------+-------------------+-------------+-------+
INFO - 08:59:25: | thick_airfoils | 5 | 24.35677013380293 | 25 | float |
INFO - 08:59:25: +----------------+-------------+-------------------+-------------+-------+
INFO - 08:59:25: *** End MDOScenario execution (time: 0:00:00.027642) ***
INFO - 08:59:25:
INFO - 08:59:25: *** Start MDOScenario execution ***
INFO - 08:59:25: MDOScenario
INFO - 08:59:25: Disciplines: Mission Structure
INFO - 08:59:25: MDO formulation: DisciplinaryOpt
INFO - 08:59:25: Optimization problem:
INFO - 08:59:25: minimize -range(thick_panels)
INFO - 08:59:25: with respect to thick_panels
INFO - 08:59:25: subject to constraints:
INFO - 08:59:25: reserve_fact(thick_panels) <= 0.5
INFO - 08:59:25: over the design space:
INFO - 08:59:25: +--------------+-------------+-------------------+-------------+-------+
INFO - 08:59:25: | Name | Lower bound | Value | Upper bound | Type |
INFO - 08:59:25: +--------------+-------------+-------------------+-------------+-------+
INFO - 08:59:25: | thick_panels | 1 | 3.256301554313449 | 20 | float |
INFO - 08:59:25: +--------------+-------------+-------------------+-------------+-------+
INFO - 08:59:25: Solving optimization problem with algorithm NLOPT_SLSQP:
INFO - 08:59:25: 20%|██ | 1/5 [00:00<00:00, 679.46 it/sec, obj=-3.84e+3]
INFO - 08:59:25: 40%|████ | 2/5 [00:00<00:00, 255.07 it/sec, obj=-3.84e+3]
INFO - 08:59:25: 60%|██████ | 3/5 [00:00<00:00, 278.83 it/sec, obj=-3.84e+3]
INFO - 08:59:25: 80%|████████ | 4/5 [00:00<00:00, 360.74 it/sec, obj=-3.84e+3]
INFO - 08:59:25: Optimization result:
INFO - 08:59:25: Optimizer info:
INFO - 08:59:25: Status: None
INFO - 08:59:25: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO Stopped the driver
INFO - 08:59:25: Number of calls to the objective function by the optimizer: 5
INFO - 08:59:25: Solution:
INFO - 08:59:25: The solution is feasible.
INFO - 08:59:25: Objective: -3843.3820355127323
INFO - 08:59:25: Standardized constraints:
INFO - 08:59:25: [reserve_fact-0.5] = 4.908429218630772e-10
INFO - 08:59:25: Design space:
INFO - 08:59:25: +--------------+-------------+-------------------+-------------+-------+
INFO - 08:59:25: | Name | Lower bound | Value | Upper bound | Type |
INFO - 08:59:25: +--------------+-------------+-------------------+-------------+-------+
INFO - 08:59:25: | thick_panels | 1 | 3.303233589970119 | 20 | float |
INFO - 08:59:25: +--------------+-------------+-------------------+-------------+-------+
INFO - 08:59:25: *** End MDOScenario execution (time: 0:00:00.024814) ***
INFO - 08:59:25: 71%|███████▏ | 5/7 [00:00<00:00, 12.68 it/sec, obj=-3.85e+3]
INFO - 08:59:25:
INFO - 08:59:25: *** Start MDOScenario execution ***
INFO - 08:59:25: MDOScenario
INFO - 08:59:25: Disciplines: Aerodynamics Mission
INFO - 08:59:25: MDO formulation: DisciplinaryOpt
INFO - 08:59:25: Optimization problem:
INFO - 08:59:25: minimize -range(thick_airfoils)
INFO - 08:59:25: with respect to thick_airfoils
INFO - 08:59:25: subject to constraints:
INFO - 08:59:25: lift(thick_airfoils) == 0.5
INFO - 08:59:25: over the design space:
INFO - 08:59:25: +----------------+-------------+-------------------+-------------+-------+
INFO - 08:59:25: | Name | Lower bound | Value | Upper bound | Type |
INFO - 08:59:25: +----------------+-------------+-------------------+-------------+-------+
INFO - 08:59:25: | thick_airfoils | 5 | 24.35677013380293 | 25 | float |
INFO - 08:59:25: +----------------+-------------+-------------------+-------------+-------+
INFO - 08:59:25: Solving optimization problem with algorithm NLOPT_SLSQP:
INFO - 08:59:25: 20%|██ | 1/5 [00:00<00:00, 694.54 it/sec, obj=-3.85e+3]
WARNING - 08:59:25: Optimization found no feasible point ! The least infeasible point is selected.
INFO - 08:59:25: 40%|████ | 2/5 [00:00<00:00, 268.52 it/sec, obj=-4.49e+3]
INFO - 08:59:25: Optimization result:
INFO - 08:59:25: Optimizer info:
INFO - 08:59:25: Status: 5
INFO - 08:59:25: Message: NLOPT_MAXEVAL_REACHED: Optimization stopped because maxeval (above) was reached
INFO - 08:59:25: Number of calls to the objective function by the optimizer: 8
INFO - 08:59:25: Solution:
WARNING - 08:59:25: The solution is not feasible.
INFO - 08:59:25: Objective: -4492.389207173914
INFO - 08:59:25: Standardized constraints:
INFO - 08:59:25: [lift-0.5] = 0.008585873120765197
INFO - 08:59:25: Design space:
INFO - 08:59:25: +----------------+-------------+-------+-------------+-------+
INFO - 08:59:25: | Name | Lower bound | Value | Upper bound | Type |
INFO - 08:59:25: +----------------+-------------+-------+-------------+-------+
INFO - 08:59:25: | thick_airfoils | 5 | 5 | 25 | float |
INFO - 08:59:25: +----------------+-------------+-------+-------------+-------+
INFO - 08:59:25: *** End MDOScenario execution (time: 0:00:00.020809) ***
INFO - 08:59:25:
INFO - 08:59:25: *** Start MDOScenario execution ***
INFO - 08:59:25: MDOScenario
INFO - 08:59:25: Disciplines: Mission Structure
INFO - 08:59:25: MDO formulation: DisciplinaryOpt
INFO - 08:59:25: Optimization problem:
INFO - 08:59:25: minimize -range(thick_panels)
INFO - 08:59:25: with respect to thick_panels
INFO - 08:59:25: subject to constraints:
INFO - 08:59:25: reserve_fact(thick_panels) <= 0.5
INFO - 08:59:25: over the design space:
INFO - 08:59:25: +--------------+-------------+-------------------+-------------+-------+
INFO - 08:59:25: | Name | Lower bound | Value | Upper bound | Type |
INFO - 08:59:25: +--------------+-------------+-------------------+-------------+-------+
INFO - 08:59:25: | thick_panels | 1 | 3.303233589970119 | 20 | float |
INFO - 08:59:25: +--------------+-------------+-------------------+-------------+-------+
INFO - 08:59:25: Solving optimization problem with algorithm NLOPT_SLSQP:
INFO - 08:59:25: 20%|██ | 1/5 [00:00<00:00, 705.64 it/sec, obj=-4.5e+3]
INFO - 08:59:25: 40%|████ | 2/5 [00:00<00:00, 243.36 it/sec, obj=-4.5e+3]
INFO - 08:59:25: 60%|██████ | 3/5 [00:00<00:00, 274.53 it/sec, obj=-4.5e+3]
INFO - 08:59:25: 80%|████████ | 4/5 [00:00<00:00, 356.26 it/sec, obj=-4.5e+3]
INFO - 08:59:25: Optimization result:
INFO - 08:59:25: Optimizer info:
INFO - 08:59:25: Status: None
INFO - 08:59:25: Message: Successive iterates of the objective function are closer than ftol_rel or ftol_abs. GEMSEO Stopped the driver
INFO - 08:59:25: Number of calls to the objective function by the optimizer: 5
INFO - 08:59:25: Solution:
INFO - 08:59:25: The solution is feasible.
INFO - 08:59:25: Objective: -4504.850158526424
INFO - 08:59:25: Standardized constraints:
INFO - 08:59:25: [reserve_fact-0.5] = 1.7025072907017602e-08
INFO - 08:59:25: Design space:
INFO - 08:59:25: +--------------+-------------+-------------------+-------------+-------+
INFO - 08:59:25: | Name | Lower bound | Value | Upper bound | Type |
INFO - 08:59:25: +--------------+-------------+-------------------+-------------+-------+
INFO - 08:59:25: | thick_panels | 1 | 3.264536832389204 | 20 | float |
INFO - 08:59:25: +--------------+-------------+-------------------+-------------+-------+
INFO - 08:59:25: *** End MDOScenario execution (time: 0:00:00.024595) ***
INFO - 08:59:25: 86%|████████▌ | 6/7 [00:00<00:00, 13.04 it/sec, obj=-4.51e+3]
INFO - 08:59:25:
INFO - 08:59:25: *** Start MDOScenario execution ***
INFO - 08:59:25: MDOScenario
INFO - 08:59:25: Disciplines: Aerodynamics Mission
INFO - 08:59:25: MDO formulation: DisciplinaryOpt
INFO - 08:59:25: Optimization problem:
INFO - 08:59:25: minimize -range(thick_airfoils)
INFO - 08:59:25: with respect to thick_airfoils
INFO - 08:59:25: subject to constraints:
INFO - 08:59:25: lift(thick_airfoils) == 0.5
INFO - 08:59:25: over the design space:
INFO - 08:59:25: +----------------+-------------+-------+-------------+-------+
INFO - 08:59:25: | Name | Lower bound | Value | Upper bound | Type |
INFO - 08:59:25: +----------------+-------------+-------+-------------+-------+
INFO - 08:59:25: | thick_airfoils | 5 | 5 | 25 | float |
INFO - 08:59:25: +----------------+-------------+-------+-------------+-------+
INFO - 08:59:25: Solving optimization problem with algorithm NLOPT_SLSQP:
INFO - 08:59:25: 20%|██ | 1/5 [00:00<00:00, 785.89 it/sec, obj=-4.51e+3]
INFO - 08:59:25: 40%|████ | 2/5 [00:00<00:00, 280.17 it/sec, obj=-4.48e+3]
INFO - 08:59:25: 60%|██████ | 3/5 [00:00<00:00, 401.52 it/sec, obj=-4.51e+3]
INFO - 08:59:25: 80%|████████ | 4/5 [00:00<00:00, 414.08 it/sec, obj=-4.51e+3]
INFO - 08:59:25: 100%|██████████| 5/5 [00:00<00:00, 423.65 it/sec, obj=-4.51e+3]
INFO - 08:59:25: Optimization result:
INFO - 08:59:25: Optimizer info:
INFO - 08:59:25: Status: None
INFO - 08:59:25: Message: Maximum number of iterations reached. GEMSEO Stopped the driver
INFO - 08:59:25: Number of calls to the objective function by the optimizer: 7
INFO - 08:59:25: Solution:
INFO - 08:59:25: The solution is feasible.
INFO - 08:59:25: Objective: -4509.519641910645
INFO - 08:59:25: Standardized constraints:
INFO - 08:59:25: [lift-0.5] = -0.0001369125128627413
INFO - 08:59:25: Design space:
INFO - 08:59:25: +----------------+-------------+-------+-------------+-------+
INFO - 08:59:25: | Name | Lower bound | Value | Upper bound | Type |
INFO - 08:59:25: +----------------+-------------+-------+-------------+-------+
INFO - 08:59:25: | thick_airfoils | 5 | 5 | 25 | float |
INFO - 08:59:25: +----------------+-------------+-------+-------------+-------+
INFO - 08:59:25: *** End MDOScenario execution (time: 0:00:00.027657) ***
INFO - 08:59:25:
INFO - 08:59:25: *** Start MDOScenario execution ***
INFO - 08:59:25: MDOScenario
INFO - 08:59:25: Disciplines: Mission Structure
INFO - 08:59:25: MDO formulation: DisciplinaryOpt
INFO - 08:59:25: Optimization problem:
INFO - 08:59:25: minimize -range(thick_panels)
INFO - 08:59:25: with respect to thick_panels
INFO - 08:59:25: subject to constraints:
INFO - 08:59:25: reserve_fact(thick_panels) <= 0.5
INFO - 08:59:25: over the design space:
INFO - 08:59:25: +--------------+-------------+-------------------+-------------+-------+
INFO - 08:59:25: | Name | Lower bound | Value | Upper bound | Type |
INFO - 08:59:25: +--------------+-------------+-------------------+-------------+-------+
INFO - 08:59:25: | thick_panels | 1 | 3.264536832389204 | 20 | float |
INFO - 08:59:25: +--------------+-------------+-------------------+-------------+-------+
INFO - 08:59:25: Solving optimization problem with algorithm NLOPT_SLSQP:
INFO - 08:59:25: 20%|██ | 1/5 [00:00<00:00, 920.81 it/sec, obj=-4.51e+3]
INFO - 08:59:25: 40%|████ | 2/5 [00:00<00:00, 262.05 it/sec, obj=-4.51e+3]
INFO - 08:59:25: 60%|██████ | 3/5 [00:00<00:00, 272.50 it/sec, obj=-4.51e+3]
INFO - 08:59:25: 80%|████████ | 4/5 [00:00<00:00, 335.28 it/sec, obj=Not evaluated]
INFO - 08:59:25: Optimization result:
INFO - 08:59:25: Optimizer info:
INFO - 08:59:25: Status: None
INFO - 08:59:25: Message: Successive iterates of the design variables are closer than xtol_rel or xtol_abs. GEMSEO Stopped the driver
INFO - 08:59:25: Number of calls to the objective function by the optimizer: 4
INFO - 08:59:25: Solution:
INFO - 08:59:25: The solution is feasible.
INFO - 08:59:25: Objective: -4509.583287341628
INFO - 08:59:25: Standardized constraints:
INFO - 08:59:25: [reserve_fact-0.5] = 3.397815362404799e-11
INFO - 08:59:25: Design space:
INFO - 08:59:25: +--------------+-------------+-------------------+-------------+-------+
INFO - 08:59:25: | Name | Lower bound | Value | Upper bound | Type |
INFO - 08:59:25: +--------------+-------------+-------------------+-------------+-------+
INFO - 08:59:25: | thick_panels | 1 | 3.225021426833141 | 20 | float |
INFO - 08:59:25: +--------------+-------------+-------------------+-------------+-------+
INFO - 08:59:25: *** End MDOScenario execution (time: 0:00:00.025106) ***
INFO - 08:59:25: 100%|██████████| 7/7 [00:00<00:00, 13.10 it/sec, obj=-4.51e+3]
INFO - 08:59:25: Optimization result:
INFO - 08:59:25: Optimizer info:
INFO - 08:59:25: Status: None
INFO - 08:59:25: Message: Maximum number of iterations reached. GEMSEO Stopped the driver
INFO - 08:59:25: Number of calls to the objective function by the optimizer: 9
INFO - 08:59:25: Solution:
INFO - 08:59:25: The solution is feasible.
INFO - 08:59:25: Objective: -4509.243708600623
INFO - 08:59:25: Standardized constraints:
INFO - 08:59:25: [lift-0.5] = 5.903055821931957e-13
INFO - 08:59:25: [reserve_fact-0.5] = -0.2599999989201578
INFO - 08:59:25: Design space:
INFO - 08:59:25: +-------+-------------+-------+-------------+-------+
INFO - 08:59:25: | Name | Lower bound | Value | Upper bound | Type |
INFO - 08:59:25: +-------+-------------+-------+-------------+-------+
INFO - 08:59:25: | sweep | 10 | 25 | 35 | float |
INFO - 08:59:25: +-------+-------------+-------+-------------+-------+
INFO - 08:59:25: *** End MDOScenario execution (time: 0:00:00.552597) ***
<gemseo.post.opt_history_view.OptHistoryView object at 0x7f8ae858b9d0>
Total running time of the script: (0 minutes 3.407 seconds)