The invention relates to a multi-rotor aircraft and a control method thereof. The multi-rotor aircraft comprises a plurality of propellers and a plurality of motors. Each motor drives the corresponding propeller to rotate. The multi-rotor aircraft further comprises a plurality of adjustable devices and micro-control motors for controlling the adjustable devices. The adjustable devices are arranged within the range of downward flushing air flow generated by the propellers and interact with the downward flushing air flow to generate new torque in the specific direction. The micro-control motors are used for controlling the adjustable devices to control the torque formed by the adjustable devices. According to the multi-rotor aircraft, the adjustable devices are introduced to interact with the air flow of the propellers so as to generate extra acting force, the new torque generated in this way and the torque formed by the propellers act at the same time, and therefore the maximum load, the controllability, the stability, the maneuverability, the runtime, the safety performance and other performance of the aircraft are synchronously improved.


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    Title :

    Multi-rotor aircraft and control method thereof


    Contributors:

    Publication date :

    2015-10-28


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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