RCAIDE.Framework.Mission.Segments.Cruise.Constant_Pitch_Rate_Constant_Altitude

Constant_Pitch_Rate_Constant_Altitude

class Constant_Pitch_Rate_Constant_Altitude(*args, **kwarg)

Bases: Evaluate

Vehicle flies at a constant pitch rate at a set altitude. This is maneuvering flight. This is used in VTOL aircraft which need to transition from one pitch attitude to another.

Assumptions: None

Source: None