FIELD: aviation.
SUBSTANCE: unmanned aerial vehicle comprises an asymmetric body, a radar nose cone, a propulsion system and a flight control system with a flat active phased antenna array, maximum aperture of which is provided due to the angle of inclination of the radiating surface to the longitudinal axis of the housing, which provides its direction towards the upper part of the surface of the nose radiotranspar fairing. Propulsion system and flight control system are configured to operate in turned by 180° by roll position.
EFFECT: invention is aimed at improvement of accuracy of guidance on final section of flight trajectory.
1 cl, 3 dwg
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