The invention provides a three-rotor aircraft and a control method thereof, and belongs to the field of aircraft design. The aircraft comprises an aircraft body, three aircraft arms and three rotors.The three rotors are evenly distributed on the periphery of the fuselage, and the vehicle arms are connected between the fuselage and the rotors. When the three-rotor aircraft flies, the three vehiclearms can deform and twist under the action of force and moment, so that the rotor wings deflect in a self-adaptive mode, three horizontal component forces are generated, the reaction torque of the three rotor wings is counteracted through the effect of combining the three horizontal component forces, and the torque problem of the three-rotor aircraft is solved.

    本发明提供了一种三旋翼飞行器及其控制方法,属于飞行器设计领域。飞行器包括机体、三根机臂和三个旋翼。所述三个旋翼均匀分布于机身外围,所述机臂连接与机身于旋翼之间。该三旋翼飞行器在飞行时,三根机臂在力和力矩的作用下可以发生变形扭转,从而使旋翼发生自适应偏转,产生三个水平分力,三个水平分力合成的效果来抵消三个旋翼的反扭矩,从而解决三旋翼飞行器的扭矩问题。


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    Title :

    Three-rotor aircraft and control method thereof


    Additional title:

    一种三旋翼飞行器及其控制方法


    Contributors:
    LI ZEBO (author) / LI XIANBANG (author) / LI BOWEN (author) / QI LINXIAO (author) / SHE GONGCHENG (author) / QUAN HEYI (author) / WANG YIXUAN (author)

    Publication date :

    2021-02-12


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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