The present invention relates to a launchpad aided GNSS relative positioning apparatus and method for unmanned aerial vehicles and, specifically, to an apparatus and method for determining the GNSS relative position of an unmanned aerial vehicle. Two launchpads are spaced apart by a set distance and allows an aircraft to take off and land. A master GNSS receiver and a follower GNSS receiver are placed on the launchpads. The GNSS relative position of the aircraft is determined in a state in which the origin of the local coordinate system is located at the position of the master GNSS receiver.
본 발명은 항공기의 런치 패드 보조 GNSS 상대 위치 결정 장치 및 방법에 관한 것으로, 특히 설정 거리 만큼 이격되어 있으며 항공기가 이착륙할 수 있는 두 개의 런치 패드(launchpad)를 마련하여 그 위에 마스터 GNSS 수신기와 팔로워 GNSS 수신기를 배치하고 로컬 좌표계의 원점은 마스터 GNSS 수신기의 위치에 위치한 상태에서 항공기의 GNSS 상대 위치를 결정하는, 항공기의 런치 패드 보조 GNSS 상대 위치 결정 장치 및 방법에 관한 것이다.
GNSS LAUNCHPAD AIDED GNSS RELATIVE POSITIONING APPARATUS FOR UNMANNED AERIAL VEHICLE AND ITS METHOD
항공기의 런치 패드 보조 GNSS 상대 위치 결정 장치 및 방법
2023-01-31
Patent
Electronic Resource
Korean
IPC: | G01S RADIO DIRECTION-FINDING , Funkpeilung / 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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