The invention discloses a parachuting method and device of an unmanned aerial vehicle. The method comprises the steps of detecting the current wind speed and the current wind direction of the current environment of the unmanned aerial vehicle when the unmanned aerial vehicle enters a parachute opening zone; controlling the unmanned aerial vehicle to fly in the parachute opening zone according to the preset airline, flying height and flying speed, wherein the flying direction of the unmanned aerial vehicle in the airline is opposite to the current wind direction; determining the location of a parachuting point of the unmanned aerial vehicle, wherein the location of the parachuting point of the unmanned aerial vehicle is a preset landing location of the unmanned aerial vehicle; determining the parachute opening location of the unmanned aerial vehicle according to the current wind speed, the flying height, the flying speed and the location of the parachuting point; opening the parachute of the unmanned aerial vehicle when the unmanned aerial vehicle arrives at the parachute opening location. With the adoption of the method and the device, the problem that the unmanned aerial vehicle cannot accurately land in a preset zone can be solved, and the effect that the unmanned aerial vehicle accurately lands in the preset zone can be achieved.


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    Title :

    Parachuting method and device of unmanned aerial vehicle


    Contributors:
    YANG LUN (author) / XING RUI (author)

    Publication date :

    2016-02-03


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

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



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