PROBLEM TO BE SOLVED: To prevent impact caused by fall of an unmanned aircraft; to prevent damage of the unmanned aircraft; and to protect an object or an organism existing on a fall point.SOLUTION: An unmanned aircraft 100 including a rotary vane 10 also includes a buffer module 111 for mitigating impact of an airframe upon collision. Further, a battery residual quantity or a distance to an object is measured by a battery residual quantity measurement module 122 or a distance measurement module 123, and a measured value is compared with a threshold, and when the measured value is lower than the threshold, the buffer module 111 is activated by an activation module 121.SELECTED DRAWING: Figure 6

    【課題】無人航空機の落下による衝撃を防ぎ、無人航空機の破損を防ぐとともに、落下地点にある物体や生物を保護する。【解決手段】回転翼10を備える無人航空機100に、衝突時に機体の衝撃を和らげる緩衝モジュール111を備える。また、バッテリー残量計測モジュール122や距離計測モジュール123によりバッテリー残量や物体との距離を計測し、計測値と閾値を比較して計測値が閾値を下回る場合には、発動モジュール121により緩衝モジュール111を発動する。【選択図】図6


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    Titel :

    UNMANNED AIRCRAFT, UNMANNED AIRCRAFT CONTROL METHOD AND UNMANNED AIRCRAFT CONTROL PROGRAM


    Weitere Titelangaben:

    無人航空機、無人航空機制御方法、及び無人航空機制御プログラム


    Beteiligte:
    SUGAYA SHUNJI (Autor:in)

    Erscheinungsdatum :

    01.06.2017


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Japanisch


    Klassifikation :

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



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