RCAIDE.Library.Mission.Common.Update

Update

RCAIDE Package Setup

Modules

acceleration(segment)	Differentiates the velocity vector to get accelerations
aerodynamics(segment)	Gets aerodynamics conditions
altitude(segment)	Updates freestream altitude from inertial position
angular_acceleration(segment)	Differentiates the angular velocity vector to get angular accelerations
atmosphere(segment)	Computes conditions of the atmosphere at given altitudes
curvilinear_inertial_horizontal_position(segment)	Determines how far the airplane has traveled and calculates position.
differentials_time(segment)	Updates the time descretization
emissions(segment)	Updates the emissions produced by the vehicle
energy(segment)	Updates battery age based on operating conditions, cell temperature and time of operation.
forces(segment)	Updates the total resultant force on the vehicle
freestream(segment)	Updates the freestream conditions
gravity(segment)	Sets the gravity for each part of the mission
ground_forces(segment)	Compute the rolling friction on the aircraft
kinematics(segment)	Updates the kinematics of the rigid body (aircraft)
linear_inertial_horizontal_position(segment)	Determines how far the airplane has traveled.
moments(segment)	Updates the total resultant moment on the vehicle
noise(segment)	Updates the noise produced by the vehicle
orientations(segment)	Updates the orientation of the vehicle throughout the mission for each relevant axis
planet_position(segment)	Updates the location of the vehicle relative to the Planet throughout the mission
stability(segment)	Updates the stability of the aircraft
thrust(segment)	Updates the thrust vector of the vehicle from the propulsors
weights(segment)	Updates the weight of the vehicle