FIELD: aviation.
SUBSTANCE: invention relates to a maneuvering method for a high-speed unmanned aerial vehicle (HSUAV) in coverage area of anti-missile and air defense. To implement the method, the trajectory of mandatory maneuvering is set, consisting of a sequence of individual sections corresponding to a certain duration, certain distance and direction of HSUAV escape from the lesion, calculated in a certain way.
EFFECT: poor predictability and low vulnerability of the trajectories of a high-speed unmanned aerial vehicle in the area of their possible damage by anti-missile and air defense means is ensured.
1 dwg
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