# This file is part of FAST-OAD_CS23-HE : A framework for rapid Overall Aircraft Design of Hybrid
# Electric Aircraft.
# Copyright (C) 2025 ISAE-SUPAERO
import openmdao.api as om
import numpy as np
import fastoad.api as oad
from fastga_he.powertrain_builder.powertrain import FASTGAHEPowerTrainConfigurator
from .constants import SUBMODEL_POWER_TRAIN_DELTA_CM
DELTA_CM_FROM_PT_FILE = "fastga_he.submodel.propulsion.delta_cm.from_pt_file"
oad.RegisterSubmodel.active_models[SUBMODEL_POWER_TRAIN_DELTA_CM] = DELTA_CM_FROM_PT_FILE
[docs]
@oad.RegisterSubmodel(SUBMODEL_POWER_TRAIN_DELTA_CM, DELTA_CM_FROM_PT_FILE)
class PowerTrainDeltaCmFromFile(om.ExplicitComponent):
def __init__(self, **kwargs):
super().__init__(**kwargs)
self.configurator = FASTGAHEPowerTrainConfigurator()
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def initialize(self):
self.options.declare(
name="power_train_file_path",
default=None,
desc="Path to the file containing the description of the power",
allow_none=False,
)
self.options.declare(
"number_of_points", default=1, desc="number of equilibrium to be treated"
)
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def setup(self):
number_of_points = self.options["number_of_points"]
self.configurator.load(self.options["power_train_file_path"])
(
components_name,
_,
_,
_,
_,
_,
_,
) = self.configurator.get_slipstream_element_lists()
self.add_output("delta_Cm", val=0.0, shape=number_of_points)
for component_name in components_name:
component_delta_cm = component_name + "_delta_Cm"
self.add_input(component_delta_cm, val=np.full(number_of_points, np.nan))
self.declare_partials(
of="delta_Cm",
wrt=component_delta_cm,
rows=np.arange(number_of_points),
cols=np.arange(number_of_points),
val=np.ones(number_of_points),
)
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def compute(self, inputs, outputs, discrete_inputs=None, discrete_outputs=None):
(
components_name,
_,
_,
_,
_,
_,
_,
) = self.configurator.get_slipstream_element_lists()
total_cm = 0.0
for component_name in components_name:
component_delta_cm = component_name + "_delta_Cm"
total_cm += inputs[component_delta_cm]
outputs["delta_Cm"] = total_cm