The invention discloses a coaxial inverted rotary wing UAV and a control method thereof. Unmanned aerial vehicles (UAVs) that work in urban streets or in environments that are inaccessible to humans through wireless control, which consists of three parts: wing, fuselage and arm. (1) On both sides of the upper fuselage of the engine, on both sides of the lower wing of the main engine (2) the inside of the wing is filled with batteries (3) the coaxial inversion, the wing rotatory wing (4) the fuselage head is equipped with photoelectric system and navigation system (5) the landing gear can be retrieved (6) the engine extends to the tail of the fuselage, and there is a downward nozzle. (7) Rotating multi-functional manipulator for grasping objects under the fuselage. According to the characteristics of coaxial dual-propeller rotary-wing UAV and various control modes, the internal space of the aircraft can be utilized to the greatest extent, and the wireless charging module can be installed and charged conveniently. It also counteracts the moment. Figure 1


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    Title :

    Coaxial Reverse Rotary Wing Mini UAV


    Contributors:
    YANG FENGZE (author) / LIU BINGWEI (author) / MENG XIN (author) / WEI XINYUAN (author) / XU HAORAN (author)

    Publication date :

    2019-10-31


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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