# This file is part of FAST-OAD_CS23 : A framework for rapid Overall Aircraft Design
# Copyright (C) 2022 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 openmdao.api as om
import fastoad.api as oad
from fastoad.module_management.constants import ModelDomain
from fastga.models.performances.mission.takeoff import TakeOffPhase
from .mission_vector import MissionVector
[docs]@oad.RegisterOpenMDAOSystem("fastga.performances.mission_vector", domain=ModelDomain.OTHER)
class FullMission(om.Group):
"""Computes and potentially save mission and takeoff based on options."""
[docs] def initialize(self):
self.options.declare("propulsion_id", default=None, types=str, allow_none=True)
self.options.declare("out_file", default="", types=str)
[docs] def setup(self):
self.add_subsystem(
"takeoff", TakeOffPhase(propulsion_id=self.options["propulsion_id"]), promotes=["*"]
)
self.add_subsystem(
"solve_equilibrium",
MissionVector(
out_file=self.options["out_file"], propulsion_id=self.options["propulsion_id"]
),
promotes=["*"],
)