An actuating system for an aircraft having an electromechanical actuator (25) comprising a non-volatile memory (60) wherein stored data (61) including configuration data (62) specific to the electromechanical actuator is stored. The system also includes a control unit (22) using the configuration data to implement a servo-control loop, the output signal of which is a digital signal controlling the electric motor of the electromechanical actuator and at least one digital transmission channel (50) connecting the control unit and the electromechanical actuator.


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    Title :

    SYSTEME D'ACTIONNEMENT POUR AERONEF


    Additional title:

    ACTUATING SYSTEM FOR AN AIRCRAFT
    BETÄTIGUNGSSYSTEM FÜR LUFTFAHRZEUG


    Contributors:

    Publication date :

    2020-09-09


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    French


    Classification :

    IPC:    G05B Steuer- oder Regelsysteme allgemein , CONTROL OR REGULATING SYSTEMS IN GENERAL / B64C AEROPLANES , Flugzeuge



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