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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    Titel :

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


    Beteiligte:
    FERVEL MARC (Autor:in) / LECANU ARNAUD (Autor:in) / MAUSSION ANTOINE (Autor:in) / AUBERT JEAN-JACQUES (Autor:in)

    Erscheinungsdatum :

    2015-07-14


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    G01C Messen von Entfernungen, Höhen, Neigungen oder Richtungen , MEASURING DISTANCES, LEVELS OR BEARINGS / B64C AEROPLANES , Flugzeuge / G05B Steuer- oder Regelsysteme allgemein , CONTROL OR REGULATING SYSTEMS IN GENERAL




    Integrated Modular Avionics Architecture Concepts Demonstration

    Potthaus, J. / Kloeckner, W. / Sprang, I. et al. | British Library Conference Proceedings | 1997




    MODULAR ARCHITECTURE AVIONICS

    BAIN HAROLD MARK / RENAULT YANN / LAZBIN JENNIFER LYNN et al. | Europäisches Patentamt | 2023

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