According to an embodiment of the present invention, an autonomous precision landing verification system of an unmanned aerial vehicle may comprise: a landing target state estimation performance verification unit which verifies the performance of estimating a landing target of the unmanned aerial vehicle; a vertical landing performance verification unit for verifying the performance of the unmanned aerial vehicle landing on the landing target moving in the vertical direction; a horizontal landing performance verification unit for verifying the performance of the unmanned aerial vehicle landing on the landing target moving in the horizontal direction; and a precision landing reliability securing unit for using the verification results obtained by the landing target state estimation performance verification unit, the vertical landing performance verification unit, and the horizontal landing performance verification unit to calculate and store information necessary for the autonomous precision landing of the unmanned aerial vehicle.
본 발명의 일 실시예에 따른 무인비행체의 자율 정밀 착륙 검증 시스템은, 무인비행체가 착륙목표를 추정하는 성능을 검증하는 착륙목표 상태추정성능 검증부; 상기 무인비행체가 수직방향으로 움직이는 상기 착륙목표에 착륙하는 성능을 검증하는 수직방향 착륙성능 검증부; 상기 무인비행체가 수평방향으로 움직이는 상기 착륙목표에 착륙하는 성능을 검증하는 수평방향 착륙성능 검증부; 및 상기 착륙목표 상태추정성능 검증부, 상기 수직방향 착륙성능 검증부 및 상기 수평방향 착륙성능 검증부에서 얻은 검증 결과를 이용하여 상기 무인비행체가 상기 착륙목표에 자율 정밀 착륙하는데 필요한 정보를 산출 및 저장하는 정밀 착륙 신뢰성 확보부;를 포함할 수 있다.
SYSTEM FOR VERIFYING AUTONOMOUS PRECISE LANDING OF UNMANNED AERIAL VEHICLE
무인비행체의 자율 정밀 착륙 검증 시스템
30.09.2021
Patent
Elektronische Ressource
Koreanisch
IPC: | G01M TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES , Prüfen der statischen oder dynamischen Massenverteilung rotierender Teile von Maschinen oder Konstruktionen / B64C AEROPLANES , Flugzeuge / 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 |
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