Transition

Transition mission methods containing the functions for setting up and solving a mission. More...

Functions
def	SUAVE.Methods.Missions.Segments.Transition.Constant_Acceleration_Constant_Angle_Linear_Climb.initialize_conditions (segment)
def	SUAVE.Methods.Missions.Segments.Transition.Constant_Acceleration_Constant_Pitchrate_Constant_Altitude.initialize_conditions (segment)
	Constant_Acceleration_Constant_Pitchrate_Constant_Altitude.py. More...

Detailed Description

Transition mission methods containing the functions for setting up and solving a mission.

Function Documentation

initialize_conditions() [1/2]

def SUAVE.Methods.Missions.Segments.Transition.Constant_Acceleration_Constant_Angle_Linear_Climb.initialize_conditions

(

segment

)

Sets the specified conditions which are given for the segment type.

Assumptions:
Constant acceleration and constant altitude

Source:
N/A

Inputs:
segment.altitude                [meters]
segment.air_speed_start         [meters/second]
segment.air_speed_end           [meters/second]
segment.acceleration            [meters/second^2]
conditions.frames.inertial.time [seconds]

Outputs:
conditions.frames.inertial.velocity_vector  [meters/second]
conditions.frames.inertial.position_vector  [meters]
conditions.freestream.altitude              [meters]
conditions.frames.inertial.time             [seconds]

Properties Used:
N/A

initialize_conditions() [2/2]

def SUAVE.Methods.Missions.Segments.Transition.Constant_Acceleration_Constant_Pitchrate_Constant_Altitude.initialize_conditions

(

segment

)

Constant_Acceleration_Constant_Pitchrate_Constant_Altitude.py.

Created: Jul 2014, SUAVE Team Modified: Jan 2016, E. Botero

Sets the specified conditions which are given for the segment type.

Assumptions:
Constant acceleration and constant altitude

Source:
N/A

Inputs:
segment.altitude                [meters]
segment.air_speed_start         [meters/second]
segment.air_speed_end           [meters/second]
segment.acceleration            [meters/second^2]
conditions.frames.inertial.time [seconds]

Outputs:
conditions.frames.inertial.velocity_vector  [meters/second]
conditions.frames.inertial.position_vector  [meters]
conditions.freestream.altitude              [meters]
conditions.frames.inertial.time             [seconds]

Properties Used:
N/A