FIELD: aircraft engineering.
SUBSTANCE: development and use of mobile small-sized unmanned aerial systems with aircraft-type UAVs with manual launch and parachute landing, intended for air surveillance, reconnaissance, detection and tracking of objects. The system consists of a mobile ground control station, ground means of radio communication, navigation and flight control. The UAV is made according to the flying-wing design and has a collapsible frame, the beams of which are inserted into the grooves of the elastic shell. A flexible solar battery is applied to the upper surface of the shell, connected to a flat battery located in a pocket on the lower surface. The frame beams in the forward part of the body are fastened with fixation to the payload unit containing the means of radio communication, navigation and control, television and infrared cameras mounted on a gyro-stabilized platform. The parachute system is also located there. In the aft part of the body, the carrier beam of the frame and the beam of the aft steering panel are fastened with fixation to the sockets on the cruise electric motors. Cruise electric motors are equipped with pusher screws.
EFFECT: efficiency increase.
1 cl, 2 dwg
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Authors
Dates
2023-04-04—Published
2022-08-08—Filed