RCAIDE.Library.Mission.Segments.Climb.Constant_Throttle_Constant_Speed.update_differentials_altitude

update_differentials_altitude(segment)

On each iteration creates the differentials and integration funcitons from knowns about the problem. Sets the time at each point. Must return in dimensional time, with t[0] = 0

Assumptions: Constant throttle setting, with a constant true airspeed.

Source: N/A

Inputs: segment.climb_angle [radians] state.conditions.frames.inertial.velocity_vector [meter/second] segment.altitude_start [meters] segment.altitude_end [meters]

Outputs: state.conditions.frames.inertial.time [seconds] conditions.frames.inertial.position_vector [meters] conditions.freestream.altitude [meters]

Properties Used: N/A