The invention discloses a light flexible flap unmanned aerial vehicle and a control method thereof.The overall structure of the light flexible flap unmanned aerial vehicle is composed of a vehicle body, a main control module, a flexible flap driving mechanism and a rotor wing, the rotor wing provides power, and the flexible flap is driven by the driving mechanism to achieve actions such as ascending, descending, left-right rotation and high-low-speed flight; the main control module determines the current action of the unmanned aerial vehicle based on the current road condition. In addition, a radar, a camera, an infrared sensing module and the like can be installed on the machine body to execute highly difficult tasks. Due to the fact that the integrated wing bodies, the flat and light fuselage and the flexible flaps are adopted, the unmanned aerial vehicle has the advantages of being low in cost, capable of rapidly rotating and flying at a high speed and the like.

    本发明公开了一种轻质柔性襟翼无人机及其控制方法,其整体结构由机身、主控制模块、柔性襟翼驱动机构和旋翼组成,旋翼提供动力,通过驱动机构驱动柔性襟翼实现上升、下降、左右回旋和高低速飞行等动作,主控制模块基于当前路况决定当前无人机的动作。除此之外,在机身处可安装雷达、摄像头、红外感应模块等执行高难度的任务。由于整体采用翼身融合和扁平轻质的机身以及柔性襟翼,可使无人机实现低成本、急速回旋、高速飞行等优点。


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    Title :

    Flexible flap unmanned aerial vehicle and control method thereof


    Additional title:

    一种柔性襟翼无人机及其控制方法


    Contributors:
    XIN LIBIAO (author) / WANG YANG (author) / LI ZHIQIANG (author) / PEI HANCHEN (author) / WANG SHUOCHAO (author)

    Publication date :

    2023-11-17


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / B64U



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