An aircraft movable control system comprises a movable component configured to be movably connected to a support component, a time of flight sensor arrangement comprising at least one transponder configured to be attached to the movable component and a corresponding transceiver configured to be attached to the support component wherein the movable sensor arrangement is configured such that one or more range values between the transceiver and the at least one transponder is determinable by the transceiver, and a movable controller configured to process the one or more range values from the transceiver and compute position values of the movable component relative to the support component.


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    Title :

    AIRCRAFT MOVABLE CONTROL SYSTEM


    Contributors:

    Publication date :

    2020-03-05


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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