FIELD: aviation.
SUBSTANCE: invention relates to landing systems for unmanned aerial vehicles of vertical take-off and landing. System consists of an air module fixed to the aircraft and a landing module. Air module comprises a housing, with an electronic control unit housed in the housing, a ball-shaped armature disposed on a rigid post. Electric contacts are made on the lower part of the armature. Landing module is made in the form of a gripper. Gripper consists of a dome with flaps installed in the lower part of the dome, which are designed to open into the dome. Each slot has a groove in such a way that in the closed position of the leaflets these grooves form a hole in which the anchor rod of the air module of the landing system is tightly placed. Leaflets are made with spring-loaded contacts. Hardware module is fixed in the landing module for the landing system and hovering in the air, in order to further charge the device through the anchor.
EFFECT: greater accuracy of the final position of the apparatus after landing is achieved.
18 cl, 8 dwg
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