|
| 1 | +from copy import deepcopy |
| 2 | +import unittest |
| 3 | + |
| 4 | +import numpy as np |
| 5 | +import openmdao.api as om |
| 6 | +from openmdao.utils.testing_utils import use_tempdirs |
| 7 | + |
| 8 | +from aviary.core.aviary_problem import AviaryProblem |
| 9 | +from aviary.utils.develop_metadata import add_meta_data |
| 10 | +from aviary.models.external_subsystems.detailed_battery.battery_variables import Aircraft, Dynamic |
| 11 | +from aviary.models.missions.energy_state_default import phase_info as energy_phase_info |
| 12 | +from aviary.subsystems.subsystem_builder import SubsystemBuilder |
| 13 | +from aviary.variable_info.variable_meta_data import CoreMetaData |
| 14 | +from aviary.variable_info.variables import Aircraft |
| 15 | + |
| 16 | + |
| 17 | +@use_tempdirs |
| 18 | +class TestShapebyConn(unittest.TestCase): |
| 19 | + def test_shape_bug(self): |
| 20 | + # Verifies that shape_by_conn variables no longer raise an exception during |
| 21 | + # setup. |
| 22 | + |
| 23 | + class ExtendedAircraft(Aircraft): |
| 24 | + """Aircraft data hierarchy with one new var.""" |
| 25 | + |
| 26 | + class Wing(Aircraft.Wing): |
| 27 | + CG1 = 'aircraft:wing:cg1' |
| 28 | + CG2 = 'aircraft:wing:cg2' |
| 29 | + |
| 30 | + ExtendedMetaData = CoreMetaData |
| 31 | + add_meta_data( |
| 32 | + ExtendedAircraft.Wing.CG1, |
| 33 | + units='ft', |
| 34 | + desc='CG of the wing.', |
| 35 | + default_value=1.0, |
| 36 | + meta_data=CoreMetaData, |
| 37 | + ) |
| 38 | + |
| 39 | + add_meta_data( |
| 40 | + ExtendedAircraft.Wing.CG2, |
| 41 | + units='ft', |
| 42 | + desc='CG of the wing.', |
| 43 | + default_value=1.0, |
| 44 | + meta_data=CoreMetaData, |
| 45 | + ) |
| 46 | + |
| 47 | + class SBC(om.ExplicitComponent): |
| 48 | + """This component has an input with shape_by_conn.""" |
| 49 | + |
| 50 | + def setup(self): |
| 51 | + self.add_input(ExtendedAircraft.Wing.CG1, units='ft', shape_by_conn=True) |
| 52 | + self.add_input('cg_promote_me', units='ft', shape_by_conn=True) |
| 53 | + |
| 54 | + self.add_output('stuff', units='ft**2', copy_shape=ExtendedAircraft.Wing.CG1) |
| 55 | + |
| 56 | + def compute(self, inputs, outputs): |
| 57 | + pass |
| 58 | + |
| 59 | + class CGBuilder(SubsystemBuilder): |
| 60 | + _default_name = 'cg_sub' |
| 61 | + |
| 62 | + def build_post_mission( |
| 63 | + self, |
| 64 | + aviary_inputs=None, |
| 65 | + mission_info=None, |
| 66 | + subsystem_options=None, |
| 67 | + phase_mission_bus_lengths=None, |
| 68 | + ): |
| 69 | + grp = om.Group() |
| 70 | + grp.add_subsystem( |
| 71 | + 'sbc', |
| 72 | + SBC(), |
| 73 | + promotes_inputs=[ |
| 74 | + ExtendedAircraft.Wing.CG1, |
| 75 | + ('cg_promote_me', ExtendedAircraft.Wing.CG2), |
| 76 | + ], |
| 77 | + ) |
| 78 | + return grp |
| 79 | + |
| 80 | + local_phase_info = deepcopy(energy_phase_info) |
| 81 | + |
| 82 | + prob = AviaryProblem(meta_data=ExtendedMetaData) |
| 83 | + |
| 84 | + prob.load_inputs( |
| 85 | + 'subsystems/aerodynamics/flops_based/test/data/high_wing_single_aisle.csv', |
| 86 | + local_phase_info, |
| 87 | + ) |
| 88 | + prob.load_external_subsystems([CGBuilder()]) |
| 89 | + # Preprocess inputs |
| 90 | + prob.check_and_preprocess_inputs() |
| 91 | + |
| 92 | + prob.build_model() |
| 93 | + |
| 94 | + prob.setup() |
| 95 | + |
| 96 | + prob.set_val(ExtendedAircraft.Wing.CG1, np.ones((3, 4))) |
| 97 | + prob.set_val(ExtendedAircraft.Wing.CG2, np.ones((4, 2))) |
| 98 | + |
| 99 | + prob.final_setup() |
| 100 | + |
| 101 | + |
| 102 | +if __name__ == '__main__': |
| 103 | + unittest.main() |
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