Source code for fastga.models.weight.mass_breakdown.c_systems.sum

"""
Python module for systems mass calculation,
part of the Operating Empty Weight (OEW) estimation.
"""
#  This file is part of FAST-OAD_CS23 : A framework for rapid Overall Aircraft Design
#  Copyright (C) 2025  ONERA & ISAE-SUPAERO
#  FAST is free software: you can redistribute it and/or modify
#  it under the terms of the GNU General Public License as published by
#  the Free Software Foundation, either version 3 of the License, or
#  (at your option) any later version.
#  This program is distributed in the hope that it will be useful,
#  but WITHOUT ANY WARRANTY; without even the implied warranty of
#  MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE.  See the
#  GNU General Public License for more details.
#  You should have received a copy of the GNU General Public License
#  along with this program.  If not, see <https://www.gnu.org/licenses/>.

import fastoad.api as oad
import openmdao.api as om

from .constants import (
    SERVICE_POWER_SYSTEM_MASS,
    SERVICE_LIFE_SUPPORT_SYSTEM_MASS,
    SERVICE_AVIONICS_SYSTEM_MASS,
    SERVICE_RECORDING_SYSTEM_MASS,
)
from ..constants import SERVICE_SYSTEMS_MASS, SUBMODEL_SYSTEMS_MASS_LEGACY


[docs]@oad.RegisterSubmodel(SERVICE_SYSTEMS_MASS, SUBMODEL_SYSTEMS_MASS_LEGACY) class SystemsWeight(om.Group): """Computes mass of systems."""
[docs] def setup(self): self.add_subsystem( "navigation_systems_weight", oad.RegisterSubmodel.get_submodel(SERVICE_AVIONICS_SYSTEM_MASS), promotes=["*"], ) self.add_subsystem( "power_systems_weight", oad.RegisterSubmodel.get_submodel(SERVICE_POWER_SYSTEM_MASS), promotes=["*"], ) self.add_subsystem( "life_support_systems_weight", oad.RegisterSubmodel.get_submodel(SERVICE_LIFE_SUPPORT_SYSTEM_MASS), promotes=["*"], ) self.add_subsystem( "recording_systems_weight", oad.RegisterSubmodel.get_submodel(SERVICE_RECORDING_SYSTEM_MASS), promotes=["*"], ) weight_sum = om.AddSubtractComp() weight_sum.add_equation( "data:weight:systems:mass", [ "data:weight:systems:power:electric_systems:mass", "data:weight:systems:power:hydraulic_systems:mass", "data:weight:systems:life_support:air_conditioning:mass", "data:weight:systems:life_support:insulation:mass", "data:weight:systems:life_support:de_icing:mass", "data:weight:systems:life_support:internal_lighting:mass", "data:weight:systems:life_support:seat_installation:mass", "data:weight:systems:life_support:fixed_oxygen:mass", "data:weight:systems:life_support:security_kits:mass", "data:weight:systems:avionics:mass", "data:weight:systems:recording:mass", ], units="kg", desc="Mass of aircraft systems", ) self.add_subsystem("systems_weight_sum", weight_sum, promotes=["*"])