The present invention relates to a multi-rotor type rotary wing unmanned aerial vehicle system, comprising: a first unmanned aerial vehicle; and at least one second unmanned aerial vehicle coupled/separated via a bridge with the first unmanned aerial vehicle. The at least one second unmanned aerial vehicle moves to a target point after separation through relative positioning of the first unmanned aerial vehicle and the at least one second unmanned aerial vehicle.

    본 발명은 멀티로터 타입의 회전익 무인비행체 시스템에 관한 것으로, 제1 무인비행체 및, 상기 제1 무인비행체와 브릿지를 통해 결합 및 분리되는 적어도 하나 이상의 제2 무인비행체를 포함하되, 상기 제1 무인비행체와 상기 적어도 하나 이상의 제2 무인비행체의 상대 측위를 통해, 상기 적어도 하나 이상의 제2 무인비행체가 분리 후 목표 지점으로 이동한다.


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    Title :

    Unmanned Aerial Vehicle System Having Rotary Wing of Multi-Rotor Type


    Additional title:

    멀티로터 타입의 회전익 무인비행체 시스템


    Contributors:
    LEE TAIK JIN (author) / YOON CHANG WON (author) / JHON YOUNG MIN (author) / BANG JAE WON (author) / NAM SUK WOO (author)

    Publication date :

    2018-04-09


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Korean


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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