Distributed flight control system implemented according to an integrated modular avionics architecture

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United States of America Patent

PATENT NO 9081372
APP PUB NO 20120101663A1
SERIAL NO

13255778

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Abstract

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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.

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Patent Owner(s)

  • AIRBUS OPERATIONS SAS

International Classification(s)

Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Aubert, Jean-Jacques Pibrac, FR 17 232
Fervel, Marc Toulouse, FR 10 143
Lecanu, Arnaud Blagnac, FR 4 76
Maussion, Antoine Toulouse, FR 5 107

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