A control system for an aircraft allowing a pilot of the aircraft to control aerodynamic means, the control system comprising a processing unit for generating control commands, the control commands being transmitted to control devices to modify a position of the aerodynamic means and to pilot the aircraft according to four control axes having a pitch control axis, a roll control axis, a yaw movement control axis and a lift control axis, the control system comprising a control member generating control setpoints, the control setpoints being transmitted to the processing unit generating the control commands under the dependency of the control setpoints, the control member being mechanically disconnected from the control devices.


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    Title :

    SYSTEME DE COMMANDE D'UN AERONEF ET AERONEF ASSOCIE


    Additional title:

    AIRCRAFT CONTROL SYSTEM AND ASSOCIATED AIRCRAFT
    STEUERUNGSSYSTEM EINES LUFTFAHRZEUGS UND ZUGEHÖRIGES LUFTFAHRZEUG


    Contributors:

    Publication date :

    2024-03-06


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    French


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



    Système de commande d’un aéronef et aéronef associé

    QUEIRAS NICOLAS / HELLIO PATRICK | European Patent Office | 2022

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    SYSTEME DE COMMANDE D'UN AERONEF ET AERONEF ASSOCIE

    QUEIRAS NICOLAS / HELLIO PATRICK | European Patent Office | 2023

    Free access