An actuator control system can include a plurality of electro-mechanical actuators for operating one or more end effectors, a plurality of position sensors associated with the plurality of electro-mechanical actuators, each of the plurality of positions sensors providing an output indicating an actual position value, and a control system. The control system can be configured to receive an activation command signal and the position sensor outputs, and send a speed command for each of the plurality of electro-mechanical actuators and adjust the speed command of each of the plurality of electro-mechanical actuators using a mean position value based on the actual position values to synchronize movement of the plurality of electro-mechanical actuators together.


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    Titel :

    CONTROL SURFACE ACTUATION SYNCHRONIZATION SYSTEM


    Weitere Titelangaben:

    STEUERFLÄCHENBETÄTIGUNGSSYNCHRONISATIONSSYSTEM
    SYSTÈME DE SYNCHRONISATION D'ACTIONNEMENT DE SURFACE DE COMMANDE


    Beteiligte:
    WANG MENG (Autor:in) / MADSON RYAN (Autor:in) / SHAH JALPA (Autor:in)

    Erscheinungsdatum :

    19.07.2023


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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