A method for adjusting the angular position of a wheel, in particular a wheel of a landing gear on an aircraft. The wheel being connected to at least one hydraulic cylinder controlled by a servo valve. The method comprising a step for determining an angular deviation between a measurement of the angular position and a setpoint angular position, a first proportional correction step, a second integral correction step and a step for adding the first current and the second current in order to determine a control current of the servo valve. The second integral control step comprising a sub-step for limiting the second current according to a parametric law imposing a second current of zero value when the angular deviation is less, in absolute value, than a first determined threshold.


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    Title :

    PROCÉDÉ DE RÉGULATION DE LA POSITION ANGULAIRE D'UNE ROUE, EN PARTICULIER, D'UN TRAIN D'ATTERRISSAGE D'UN AÉRONEF


    Additional title:

    METHOD FOR CONTROLLING THE ANGULAR POSITION OF A WHEEL, IN PARTICULAR A LANDING GEAR OF AN AIRCRAFT
    VERFAHREN ZUR STEUERUNG DER WINKELPOSITION EINES RADES, INSBESONDERE EINES FAHRWERKES EINES FLUGZEUGES


    Contributors:

    Publication date :

    2024-04-03


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    French


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge





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