A method determines the position of an actuating device of an element of an aircraft seat. The actuating device includes a calculating unit, an actuator movably mounted on an output shaft for actuating the element, the output shaft being connected to an angular position encoder so a position (X) of the actuator on the output shaft corresponds to a single angular position (θ) of the encoder. The method includes a preliminary submethod of automatically calibrating the actuating device including: placing the actuator at a predetermined position (Xref) corresponding to an expected angle value (θatt) of the encoder; measuring an initial positioning angle value (θini) of the encoder when the actuator shaft is in the predetermined position (Xref); comparing the initial positioning angle value (θini) and the expected angle value (θatt) calculating the angular offset of the encoder signal, with θdécal=(θini−θatt) [MODULO 360°], θdecal being between 0° and 359°.


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    Title :

    PROCEDE DE DETERMINATION DE LA POSITION D'UN DISPOSITIF D'ACTIONNEMENT, DISPOSITIF D'ACTIONNEMENT CORRESPONDANT


    Additional title:

    METHOD FOR DETERMINING THE POSITION OF AN ACTUATING DEVICE, CORRESPONDING ACTUATING DEVICE
    VERFAHREN ZUR BESTIMMUNG DER POSITION EINER BETÄTIGUNGSVORRICHTUNG, BETÄTIGUNGSVORRICHTUNG


    Contributors:

    Publication date :

    2025-04-23


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    French


    Classification :

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




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