The present invention relates to an apparatus for simulating flight of an unmanned aerial vehicle, which includes: a frame part including a plurality of vertical posts arranged with an interval along a circumferential direction and a connecting frame connecting the plurality of vertical posts and forming an inner space which is surrounded by the plurality of vertical posts and in which the flight of the unmanned aerial vehicle is simulated; three or more moving bases branching to be extended so as to be coupled to three or more slide posts among the plurality of vertical posts in a vertical slidable manner; and a joint part rotationally connecting the unmanned aerial vehicle to the moving base in a three-axis rotation.

    무인비행체 비행 모의 시험 장치에 관한 것으로, 둘레 방향을 따라 간격을 두고 배치되는 복수의 연직 포스트 및 상기 복수의 연직 포스트를 연결하는 연결프레임을 포함하고, 상기 복수의 연직 포스트로 둘러싸인 내측에 무인비행체의 비행 모의 시험이 이루어지는 내측 공간을 형성하는 골조부; 상기 복수의 연직 포스트 중 셋 이상인 슬라이드 포스트에 상하 방향 슬라이드 이동 가능하게 결합되도록 셋 이상 분기하여 연장되는 무빙 베이스; 및 상기 무인비행체를 상기 무빙 베이스에 3축 회전 가능하게 연결하는 조인트부를 포함한다.


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    Title :

    UNMANNED AERIAL VEHICLE FLIGHT SIMULATOR FOR VERIFICATION OF FLIGHT CONTROL ALGORITHM


    Additional title:

    비행제어 알고리즘 검증을 위한 무인비행체 비행 모의 시험 장치


    Contributors:
    KO SANGHO (author) / LEE YEONGHO (author) / KIM GEUNHWAN (author) / SHIN SEUNGCHAN (author)

    Publication date :

    2020-05-28


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Korean


    Classification :

    IPC:    B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen / G01M TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES , Prüfen der statischen oder dynamischen Massenverteilung rotierender Teile von Maschinen oder Konstruktionen




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