Aircraft, fly-by-wire systems, and controllers are provided. An aircraft includes a trim control system and a fly-by-wire system. The trim control system is configured for controlling surfaces of the aircraft. The fly-by-wire system is communicatively coupled with the trim control system and includes an input device and a controller. The input device is configured to receive a re-trim input from a user. The controller is communicatively coupled with the input device and is configured to control the trim control system, to obtain the re-trim input from the user, and to set a pitch trim of the aircraft based on a stable flight condition at a present airspeed of the aircraft in response to the re-trim input from the input device.
AIRCRAFT, SYSTEMS, AND METHODS FOR TRIM CONTROL IN FLY-BY-WIRE AIRCRAFT SYSTEMS
2016-06-02
Patent
Elektronische Ressource
Englisch
AIRCRAFT, SYSTEMS, AND METHODS FOR TRIM CONTROL IN FLY-BY-WIRE AIRCRAFT SYSTEMS
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