FIELD: aviation.
SUBSTANCE: invention relates to a method of controlling an unmanned aerial vehicle (UAV) at a final drive section. To control UAV, measuring relative distance to destination object, angle of direction to object, pitch angle, height of UAV, true air speed, angle of attack, components of wind velocity are evaluated, a given angle of approach is maintained with minimization of final deviation according to control signals generated by means of quasi-optimal law of guidance in a certain way.
EFFECT: higher speed and accuracy of UAV control.
1 cl, 4 dwg
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