A flight control system includes a first and second operator input means configured to receive a mechanical input from an operator and are connected to an artificial feel system and at least one sensor. The system includes a flight control computer (FCC) in data communication with the sensor, wherein the FCC receives a signal from the sensor in response to an input by the operator. The flight control system has first and second servo controllers in data communication with first and second servos, respectively, and the FCC. The servos are connected to control surfaces that, when moved, cause the aircraft to change attitude. The flight control system also includes a third and a fourth servo controller, the third and fourth servo controllers being in communication with the FCC and a dual-lane servo operably connected to a third control surface that, when moved, causes the aircraft to change attitude.
Fly by Wire Flight Control System
2024-12-12
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
FLY-BY-WIRE FLIGHT CONTROL SYSTEM WITH BACKUP MECHANICAL FLIGHT CONTROL SYSTEM
European Patent Office | 2018
FLY-BY-WIRE FLIGHT CONTROL SYSTEM WITH BACKUP MECHANICAL FLIGHT CONTROL SYSTEM
European Patent Office | 2018
|FBW Fly-By-Wire Flight control system capable of emergency flight control
European Patent Office | 2017
|