A flight control system for an aircraft, intended for controlling a plurality of actuators adapted for actuating control surfaces of the aircraft from information supplied by piloting members and/or sensors of the aircraft. The system includes a primary control system adapted for controlling a first set of control surface actuators and a secondary control system adapted for controlling a second set of control surface actuators, the primary and secondary systems being respectively powered by independent energy sources of different types.
Distributed flight control system implemented according to an integrated modular avionics architecture
2015-07-14
Patent
Electronic Resource
English
Integrated Modular Avionics Architecture Concepts Demonstration
British Library Conference Proceedings | 1997
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