AIRCRAFT CONTROL SYSTEM, SHEET ROTOR AIRCRAFT AND METHOD OF IMPROVING LANDING DOWN STOP RATE

摘要

SUMMARY AN AIRCRAFT CONTROL SYSTEM, SHADOW ROTOR AIRCRAFT AND METHOD OF IMPROVING LANDING DOWN STOP RATE A flight control system uses a governor configured to regulate the speed of an rotor in the aircraft through step control. a rotor blade, and a limiter configured to selectively remove the governor limit value when the collective pitch control exceeds a limit value to allow a full collective pilot command above the limit value. The threshold value is selectively removed and progressively returned to provide temporary pilot control to "cushion" the landing of an aircraft when an engine fails.