A control device for unmanned aircraft comprising: a rotary-wing control signal generation circuit for generating a rotary wing control signal for causing a driving device to drive a plurality of rotary wings for flying the unmanned aircraft; a measuring device for measuring a physical amount relating to an operation of at least one of the plurality of rotary wings; and a fault detection circuit for detecting a fault in the operation of at least one of the plurality of rotary wings by using the physical amount measured by the measuring device, wherein the rotary-wing control signal generation circuit is configured to generate a rotary wing control signal depending on the fault detected by the fault detection circuit in the operation of at least one of the plurality of rotary wings, is provided.


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    Title :

    Unmanned Aircraft, Device for Controlling Unmanned Aircraft, Method for Controlling Unmanned Aircraft, and Device for Detecting Failure of Unmanned Aircraft


    Contributors:
    NONAMI KENZO (author) / YANG YI (author)

    Publication date :

    2020-04-02


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    G05D SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES , Systeme zum Steuern oder Regeln nichtelektrischer veränderlicher Größen / B64C AEROPLANES , Flugzeuge / G06F ELECTRIC DIGITAL DATA PROCESSING , Elektrische digitale Datenverarbeitung






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