The present invention provides a precision landing guidance system for unmanned aerial vehicles. Provided is the precision landing guidance system of the unmanned aerial vehicle, which includes: an image acquisition unit which acquires an attitude image of a flying unmanned aerial vehicle; a posture information calculation unit which processes the acquired posture image to calculate posture information; and a landing control unit which receives the calculated attitude information, remotely corrects the attitude of the unmanned aerial vehicle to match the landing attitude information in the landing area, and lands the unmanned aerial vehicle in the landing area. Additionally, the present invention provides the method for guiding precision landing of the unmanned aerial vehicle.

    본 발명은 무인항공기의 정밀 착륙 유도 시스템을 제공한다. 상기 무인항공기의 정밀 착륙 유도 시스템은 비행 중인 무인 항공기에 대한 자세 영상을 취득하는 영상 취득부; 상기 취득된 자세 영상을 이미지 처리하여 자세 정보를 산출하는 자세 정보 산출부; 및, 상기 산출된 자세 정보를 전송 받아 착륙 영역부에서의 착륙 자세 정보에 부합되도록 상기 무인 항공기의 자세를 원격으로 보정하여 상기 무인 항공기를 상기 착륙 영역부에 착륙시키는 착륙 제어부;를 포함한다. 또한 본 발명은 무인항공기의 정밀 착륙 유도 방법을 제공한다.


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    Title :

    Unmaned aerial vehicle accuracy landing system and Unmaned aerial vehicle accuracy landing method using the same


    Additional title:

    무인항공기의 정밀 착륙 유도 시스템 및 이를 사용한 무인항공기의 정밀 착륙 유도 방법


    Contributors:
    KIM NAM SIC (author) / NAM HYUN YU (author) / JIN SANG JUNG (author)

    Publication date :

    2023-09-26


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Korean


    Classification :

    IPC:    G08G Anlagen zur Steuerung, Regelung oder Überwachung des Verkehrs , TRAFFIC CONTROL SYSTEMS / B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / G05D SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES , Systeme zum Steuern oder Regeln nichtelektrischer veränderlicher Größen



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