Disclosed is an aircraft control system (100) configured to be operably connected to at least one landing gear and at least one landing gear bay door of an aircraft (400). The system comprises: a user interface (10) operable by a user to manually input first and second requests; and a landing gear controller (20) communicatively coupled to the user interface. The controller is configured, in use, to: receive, from the user interface, a first indication indicative of user-operation of the user interface to input the first request, and to initiate movement of the landing gear bay door from a closed position to an open position on the basis of the first indication without initiating movement of the landing gear between an extended position and a retracted position; and receive, from the user interface, a second indication indicative of user-operation of the user interface to input the second request, and to initiate movement of the landing gear between the extended position and the retracted position on the basis of the second indication.


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    Title :

    LANDING GEAR CONTROL


    Additional title:

    FAHRWERKSSTEUERUNG
    COMMANDE DE TRAIN D'ATTERRISSAGE


    Contributors:
    KERR SEAN (author) / MARLES DAVID (author)

    Publication date :

    2020-09-02


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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