The invention provides a deformable water-air dual-purpose unmanned aerial vehicle and a control method thereof. The unmanned aerial vehicle comprises a vehicle body, a rotatable vehicle arm, a stand column, a landing buoy and a connecting supporting rod. The machine body is rectangular, each side edge is rotationally provided with one rotatable machine arm, one end of each rotatable machine arm is connected to the machine body through a driving motor, and the other end of each rotatable machine arm is provided with a three-blade propeller; the two rising and falling buoys and the two connecting supporting rods are all located below the aircraft body. The two rising and falling pontoons and the two connecting supporting rods are in one-to-one correspondence with the four side edges of the aircraft body respectively, the rising and falling pontoons and the connecting supporting rods are each provided with a groove structure II, and when the rotatable aircraft arm rotates to the vertical position, the rotatable aircraft arm falls into the groove structures II. According to the technical scheme, the problem that an existing traditional four-rotor or multi-rotor unmanned aerial vehicle cannot sail on the water surface or is positioned on the basis of sailing on the water surface is solved.

    本发明提供一种可变形水空两用的无人机及其控制方法,所述无人机包括机体、可旋转机臂、立柱、起落浮筒和连接撑杆;所述机体为矩形,每一条侧边均转动安装有一个所述可旋转机臂,所述可旋转机臂一端通过驱动马达连接于所述机体,所述可旋转机臂另一端安装有三叶桨;两个所述起落浮筒和两个连接撑杆均位于所述机体下方;两个所述起落浮筒和两个所述连接撑杆分别与所述机体的四条侧边一一对应,所述起落浮筒和所述连接撑杆均设置有凹槽结构Ⅱ,当所述可旋转机臂转动至竖直位置时,落入所述凹槽结构Ⅱ内。本发明的技术方案解决了现有传统四旋翼或多旋翼无人机无法进行水面航行或基于水面航行定位的问题。


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    Titel :

    Deformable water-air dual-purpose unmanned aerial vehicle and control method thereof


    Weitere Titelangaben:

    一种可变形水空两用的无人机及其控制方法


    Beteiligte:
    GUO YUNLONG (Autor:in)

    Erscheinungsdatum :

    2022-07-15


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

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



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