Source code for RCAIDE.Framework.Mission.Segments.Ground.Test_Stand
# RCAIDE/Framework/Analyses/Mission/Segments/Ground/Test_Stand.py
#
#
# Created: Jul 2023, M. Clarke
# ----------------------------------------------------------------------------------------------------------------------
# IMPORT
# ----------------------------------------------------------------------------------------------------------------------
# RCAIDE imports
from RCAIDE.Framework.Mission.Segments.Evaluate import Evaluate
from RCAIDE.Framework.Core import Units
from RCAIDE.Library.Mission.Segments import Ground
from RCAIDE.Library.Methods.skip import skip
# ----------------------------------------------------------------------------------------------------------------------
# Takeoff
# ----------------------------------------------------------------------------------------------------------------------
[docs]
class Test_Stand(Evaluate):
"""
"""
def __defaults__(self):
""" This sets the default solver flow. Anything in here can be modified after initializing a segment.
Assumptions:
None
Source:
N/A
Inputs:
None
Outputs:
None
Properties Used:
None
"""
# --------------------------------------------------------------------------------------------------------------
# User Inputs
# --------------------------------------------------------------------------------------------------------------
self.velocity = 150 * Units.knots
self.throttle = 1.0
self.altitude = 0.0
self.time = 0.0
self.true_course = 0.0 * Units.degrees
# --------------------------------------------------------------------------------------------------------------
# Mission Unknowns and Residuals
# --------------------------------------------------------------------------------------------------------------
ones_row = self.state.ones_row
self.state.residuals.final_velocity_error = ones_row(1) * 0
self.state.unknowns.ground_velocity = ones_row(1) * 0
# --------------------------------------------------------------------------------------------------------------
# Mission specific processes
# --------------------------------------------------------------------------------------------------------------
initialize = self.process.initialize
initialize.conditions = Ground.Test_Stand.initialize_conditions
converge = self.process.converge
converge.solver = skip
iterate = self.process.iterate
iterate.unknowns.mission = skip
iterate.conditions.aerodynamics = skip
iterate.conditions.stability = skip
post_process = self.process.post_process
post_process.aeroacoustics = skip
return
