Abstract
This article describes the design of the UAV of the convertible type. This type of UAV allows for vertical take-off and landing. Runway, parachute, catapult, etc. are not required for this vehicle.For the design of this UAV, the scheme tilt rotor, i.e., the scheme with rotary motors is applied. This scheme combines the vertical lift potential of a helicopter with the speed and range of a conventional aircraft.The calculation of aerodynamics, flight characteristics and durability calculation are carried out.Each element is designed with ease of use of this UAV.The project has a direct market advantage due to the transportation of the complex. The complex is transported in a backpack, the overall dimensions of which do not differ from the tourist backpack.
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