FIELD: aviation.
SUBSTANCE: invention relates to a manoeuvring method for a high-speed unmanned aerial vehicle (HSUAV) in possible coverage area of anti-missile and air defence means. To implement the method, the trajectory of mandatory HSUAV manoeuvring, consisting of a sequence of individual manoeuvres with a certain duration, is selected stochastically in certain spatial boundaries of the plane of the individual manoeuvre vectors, calculated in a certain way, while the parameters of the acceleration vector of the next manoeuvre are limited by the design features of HSUAV.
EFFECT: poor predictability and low vulnerability of the trajectories of a high-speed unmanned aerial vehicle in the area of their possible damage.
1 dwg
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