Fly-by-wire static longitudinal stability compensation system

摘要

Static longitudinal stability (SLS) systems, the release without pilot clearly the mode selection, in response to a control input of the pilot to the flight control system and to the state of the measured aircraft and set smoothly to provide airspeed hold function that do not it is, in the way. Trim state, aircraft approaches the non-accelerating state, SLS sets the airspeed hold. This logic is the pilot, can also be set to SLS, to the trim state aircraft acceleration / deceleration maneuvers to fly near the airspeed desired also, the speed at longitudinal acceleration is small, is released and set in response without waiting SLS is a catch, and the status of the flight control system, how the aircraft, and whether it is steered.