FIELD: aviation; control methods.
SUBSTANCE: invention relates to UAV group control method. Method comprises, for each UAV in its inertial navigation system, measuring its current speed, calculating its flight direction, using sensors measuring the viewing angle of each potentially hazardous object, distance to it, approach speed with it, angular velocity of the line of sight of this object, based on these measured and calculated values, calculating coordinates and velocity vectors of each UAV and each object, possibility of turning an object on an UAV for each UAV, forming a flight trajectory and control signal values of each UAV, then formed trajectory and a control signal are transmitted to the control system.
EFFECT: provides for correction of movement of all UAVs to prevent possible collisions.
1 cl, 4 dwg
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