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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    Title :

    Control surface actuation synchronization system


    Contributors:
    WANG MENG (author) / MADSON RYAN (author) / SHAH JALPA (author)

    Publication date :

    2024-03-26


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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