FIELD: aviation.
SUBSTANCE: invention relates to unmanned aerial vehicles. Unmanned aerial vehicle landing system consists of located in fuselage (3) winch (7) with cable (4) and anchor (5), equipped with cable tension force sensor. Fuselage accommodates gastight vessel (1) accommodating heat exchanger (11) with heating element. Cylinder (6) filled with compressed lifting gas is connected to heat exchanger (11) through air valve (2). Operation of all devices of the unmanned aerial vehicle is provided by control system (8) and coordinated by an operator via a radio channel. Lanyard (10) with rigidly fixed ends suspended on supports (9) is used as a landing element.
EFFECT: reduced dependence on limited landing area.
1 cl, 2 dwg
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