AIR LANDING METHOD AND SYSTEM OF AN UNMANNED AIR VEHICLE

The present invention relates to an aerial landing system for an unmanned aerial vehicle, comprising a daughter ship equipped with a first coupling device capable of projecting downward and a mother ship equipped with a second coupling device capable of projecting upward, wherein the daughter ship a...

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Bibliographische Detailangaben
Hauptverfasser:	MYENG HYUN SAM, LEE MIN SEOK, JEONG JUN HO, JUNG JAE HWI, LIM HEUNG SIK
Format:	Patent
Sprache:	eng ; kor
Schlagworte:	AEROPLANES AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION COSMONAUTICS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS HELICOPTERS PARACHUTES PERFORMING OPERATIONS TRANSPORTING
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Beschreibung
Zusammenfassung:	The present invention relates to an aerial landing system for an unmanned aerial vehicle, comprising a daughter ship equipped with a first coupling device capable of projecting downward and a mother ship equipped with a second coupling device capable of projecting upward, wherein the daughter ship approaches the mother ship using a rendez-vous algorithm so that the first coupling device and the second coupling device are coupled. According to the present invention, the unmanned aerial vehicle can land in the air rather than on a ground runway. 본 발명은 하방향으로 돌출 가능한 제1 결합장치가 장착된 자선(daughter ship) 및 상방향으로 돌출 가능한 제2 결합장치가 장착된 모선(mother ship)을 포함하고, 상기 자선은 랑데부(rendez-vous) 알고리즘을 이용하여 상기 모선에 접근하여, 상기 제1 결합장치와 상기 제2 결합장치가 결합하는 것을 특징으로 하는 무인기의 공중착륙 시스템으로서, 본 발명에 의하면, 무인기가 지상 활주로가 아닌 공중에서 착륙할 수 있게 한다.