Source code for fastoad.models.weight.mass_breakdown.d_furniture.d4_security_kit_weight

"""
Estimation of security kit weight
"""
#  This file is part of FAST-OAD : A framework for rapid Overall Aircraft Design
#  Copyright (C) 2021 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 numpy as np
import openmdao.api as om


[docs]class SecurityKitWeight(om.ExplicitComponent): """ Weight estimation for security kit Based on :cite:`supaero:2014`, mass contribution D4 """ """ Passenger security kit weight estimation (D4) """
[docs] def setup(self): self.add_input("data:TLAR:NPAX", val=np.nan) self.add_input("tuning:weight:furniture:security_kit:mass:k", val=1.0) self.add_input("tuning:weight:furniture:security_kit:mass:offset", val=0.0, units="kg") self.add_output("data:weight:furniture:security_kit:mass", units="kg")
[docs] def setup_partials(self): self.declare_partials("*", "*", method="fd")
[docs] def compute(self, inputs, outputs, discrete_inputs=None, discrete_outputs=None): npax = inputs["data:TLAR:NPAX"] k_d4 = inputs["tuning:weight:furniture:security_kit:mass:k"] offset_d4 = inputs["tuning:weight:furniture:security_kit:mass:offset"] temp_d4 = 1.5 * npax outputs["data:weight:furniture:security_kit:mass"] = k_d4 * temp_d4 + offset_d4