Source code for fastga.models.geometry.geom_components.nacelle.compute_nacelle_position

"""
Python module for nacelle position calculations, part of the geometry component.
"""
#  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.
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#  along with this program.  If not, see <https://www.gnu.org/licenses/>.

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

from .components import ComputeNacelleXPosition, ComputeNacelleYPosition
from ...constants import SERVICE_NACELLE_POSITION, SUBMODEL_NACELLE_POSITION_LEGACY


# pylint: disable=too-few-public-methods
[docs]@oad.RegisterSubmodel(SERVICE_NACELLE_POSITION, SUBMODEL_NACELLE_POSITION_LEGACY) class ComputeNacellePosition(om.Group): """Nacelle and pylon geometry estimation, obtained from :cite:`supaero:2014`.""" # pylint: disable=missing-function-docstring # Overriding OpenMDAO setup
[docs] def setup(self): self.add_subsystem( "nacelle_x_position", ComputeNacelleXPosition(), promotes=["*"], ) self.add_subsystem( "nacelle_y_position", ComputeNacelleYPosition(), promotes=["*"], )