Systems and methods are provided for a roll attitude dependent roll rate limit that may limit an aircraft to a lower roll rate limit under normal flight conditions. The 5 systems and methods may detect situations where a higher roll rate limit may be desirable and allow the aircraft to exceed the lower roll rate limit, to either a higher roll rate limit or a roll rate between the lower and higher roll rate limit. - 31 - 420 | 430 | 440 Airplane State Sensors: Pilot Controls: Autopilot Roll Rate Control Wheel Bank Angle Pedal Flap Position Airspeed Altitude Pitch Attitude , F450 Flight Control Computer Vehicle Dynamic Characteristic Calculation Roll Rate Regulation and Surface Command Calculation Flight Control Actuators and Roll Control Surfaces: Ailerons Flaperons Spoilers Rudders
Roll attitude-dependent roll rate limit
2020-07-02
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |