An aircraft assembly, comprising: a reference component; a first component (106) and a first actuator (102), the first actuator arranged to move the first component relative to the reference component; a second component (108) and a second actuator (102), the second actuator (102) arranged to move the second component relative to the reference component; a position sensor (110) arranged to measure a position of the first component (106), and to output a position value, the sensor being capable of outputting a plurality of non-zero position values; and a controller (100) arranged to control the movement of the second component (108) by the second actuator (104) based at least partially on the position value output by the position sensor (110).


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    Title :

    AIRCRAFT LANDING GEAR ASSEMBLY ACTUATION SYSTEM


    Additional title:

    AKTUATORSYSTEM FÜR FLUGZEUGFAHRWERKSEINHEIT
    SYSTÈME D'ACTIONNEMENT D'ASSEMBLAGE DU TRAIN D'ATTERRISSAGE D'AÉRONEF


    Contributors:

    Publication date :

    2022-08-24


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

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



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