The invention relates to a fly-by-wire system which comprises: three-stage piloting control, each stage including a control computer suitable for determining the positions of the stick, and a monitoring computer capable of verifying all the pre-determined positions of the stick; three-stage control-surface position calculation, each stage including a control computer suitable for calculating the control-surface positions from encoded positions of the stick, and a monitoring computer capable of verifying all the calculated control-surface positions; a single unidirectional communication link connecting the control computer of the first piloting control stage to the control computer of the first control-surface position calculation stage; a single unidirectional communication link connecting the control computer of the second piloting control stage to the control computer of the second control-surface position calculation stage; and a single unidirectional communication link connecting the control computer of the third piloting control stage to the control computer of the third control-surface position calculation stage.


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    Titel :

    SYSTÈME DE COMMANDE DE VOL ÉLECTRIQUE POUR AÉRONEF


    Weitere Titelangaben:

    FLY-BY-WIRE SYSTEM FOR AN AIRCRAFT
    FLY-BY-WIRE-SYSTEM FÜR EIN FLUGZEUG


    Beteiligte:
    BARA CÉDRIC (Autor:in) / TUZI CHRISTOPHE (Autor:in) / BOURGOGNE ERIC (Autor:in) / COPPEE PASCAL (Autor:in) / VANDENBAVIERE YANN (Autor:in)

    Erscheinungsdatum :

    17.02.2021


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Französisch


    Klassifikation :

    IPC:    G05D SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES , Systeme zum Steuern oder Regeln nichtelektrischer veränderlicher Größen / B64C AEROPLANES , Flugzeuge



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