The present invention relates to a vertical take-off and landing fixed-wing unmanned aerial vehicle. More specifically, in the vertical take-off and landing fixed-wing unmanned aerial vehicle including a main body and a thrust unit which generates thrust, the vertical take-off and landing fixed-wing unmanned aerial vehicle of the present invention can perform forward movement and vertical take-off and landing without changing the direction of the thrust unit by controlling an inclination of the main body through control of a thrust value. The vertical take-off and landing fixed-wing unmanned aerial vehicle comprises: a body (110); a main body (100); and the thrust unit (200).

    본 발명은 수직 이착륙 고정익 무인기에 관한 것으로서, 더욱 상세하게는 본체와 추력을 발생시키는 추력부를 포함하는 수직 이착륙 고정익 무인기에 있어서, 추력 값의 제어를 통한 본체의 기울기를 제어함으로써, 추력부의 방향 변경 없이 전진 방향으로의 이동 및 수직 이착륙을 수행할 수 있는 수직 이착륙 고정익 무인기에 관한 것이다.


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    Title :

    VERTICAL TAKEOFF AND LANDING FIXED WING URMANNED AERIAL VEHICLE


    Additional title:

    수직 이착륙 고정익 무인기


    Contributors:
    HEEWOO LEE (author) / SUNGYOUL PARK (author)

    Publication date :

    2021-07-09


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Korean


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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