FIELD: aviation.
SUBSTANCE: invention relates to the aviation equipment. Unmanned aerial vehicle (UAV) landing system consists of fixed on the aircraft mobile part (MP) and a fixed on the stationary or mobile object landing element (LE). MP is mounted on the UAV fuselage bottom container. Container is divided into front, central and rear parts. In front of the container strictly along the course guidance system camera is placed. In the container central part flaps are made with possibility of opening and a cable with an anchor is placed. In the container rear part a braking parachute is arranged and secured with the cable and the UAV elements with slings. Base part represents the landing element, made in the form of the horizontal yard, made with possibility of rotation around its own axis and with marks for the MP camera determination. UAV landing is carried out by the UAV and the anchor twisting around the landing element towards each other, lowered from the container before landing.
EFFECT: invention is aimed at increase in the landing accuracy.
13 cl, 9 dwg
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Authors
Dates
2019-01-28—Published
2017-12-28—Filed