FIELD: aviation.
SUBSTANCE: invention relates to aircraft engineering. Unmanned aerial vehicle comprises wing, made in aerodynamic scheme "flying wing", control elements made in the form of vertical empennage and arranged on the support of the front horizontal empennage, power plant equipped with a motor and a propeller. Wing is disc-shaped, front horizontal empennage is made in form of two identical disks, located above axis of rotation of propeller at a distance exceeding half diameter of propeller. Vertical empennage is arranged in tail part of disc-shaped wing, in which additional horizontal empennage is installed with possibility of air blowing from side of upper surface of wing and from side of lower surface of wing.
EFFECT: invention is aimed at maintenance of stable conditions of air flow around the wing at high angles of attack and under action of strong side wind.
1 cl, 3 dwg
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