The invention discloses an inverse compensation stable-attitude quadrotor unmanned aerial vehicle. The inverse compensation stable-attitude quadrotor unmanned aerial vehicle comprises a vehicle body, wherein four arms are fixedly connected to the vehicle body, a rotor wing is installed at the tail end of each arm, the arms are arranged in a pairwise opposite mode, every two opposite arms are located on the same straight line, and the positions where two opposite arms are connected with the vehicle body are higher than the positions where the other two opposite arms are connected with the vehicle body; a chamber channel is formed in each arm, the chamber channels of every two opposite arms are communicated through a pipeline arranged in the vehicle body to form parallel channels, and balancing blocks are arranged in the parallel channels and driven by driving devices arranged on the parallel channels. By the adoption of the inverse compensation stable-attitude quadrotor unmanned aerial vehicle, the problem that the vehicle shakes under continuous strong wind high in the sky is effectively solved, and the quality of an aerial photo is more stable.


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    Titel :

    Inverse compensation stable-attitude quadrotor unmanned aerial vehicle


    Beteiligte:
    ZHU LIFEN (Autor:in) / GUO GUANGZHUANG (Autor:in)

    Erscheinungsdatum :

    2015-12-09


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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