An object of the present invention is to provide a horizontal control station for take-off and landing of an unmanned aerial vehicle, which can stably control horizontality during movement or in a curved terrain. According to an aspect of the present invention, the horizontal control station for take-off and landing of the unmanned aerial vehicle comprises: a take-off and landing platform supporting an unmanned aerial vehicle; a posture control member controlling a posture of an upper plate in a lower portion of the take-off and landing platform and including a plurality of bevel gears; a main base supporting the posture control member in a lower portion of the posture control member; and a buffer cylinder connecting and supporting the take-off and landing platform and the main base.

    본 발명은 이동 중 또는 굴곡된 지형에서 안정적으로 수평을 제어할 수 있는 무인 항공기 이착륙을 위한 수평 제어 스테이션을 제공하는 것을 목적으로 한다. 본 발명의 일 측면에 따른 무인 항공기 이착륙을 위한 수평 제어 스테이션은 무인 항공기를 지지하는 이착륙 플랫폼, 상기 이착륙 플랫폼의 하부에서 상기 상판의 자세를 제어하며 복수의 베벨기어를 포함하는 자세제어부재, 상기 자세제어부재의 하부에서 상기 자세제어부재를 지지하는 메인 베이스, 및 상기 이착륙 플랫폼과 상기 메인 베이스를 연결하여 지지하는 완충 실린더를 포함할 수 있다.


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    Title :

    HORIZONTAL CONTROL STATION FOR UNMANED AERIAL VEHICLE LANDING AND FLIGHT


    Additional title:

    무인 항공기 이착륙을 위한 수평 제어 스테이션


    Contributors:
    HAHM JE HUN (author) / PARK SANG HYUN (author) / LEE JAE YOUL (author) / KIM SANG HO (author) / JEONG MYEONG SU (author) / SEO KAP HO (author)

    Publication date :

    2024-03-06


    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 / B64C AEROPLANES , Flugzeuge / F16F SPRINGS , Federn / F16H Getriebe , GEARING




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