METHOD FOR DESTROYING HYPERSONIC MANEUVERING TARGET BY ROCKET

摘要

FIELD: missile guidance systems.;SUBSTANCE: invention relates to missile guidance systems, namely to defensive-offensive systems. In a defensive-offensive system (DOS), a target is detected and tracked and its coordinates and speed are determined. In the DOS, the trajectory of the target is determined, relative to which it maneuvers, its continuation is predicted and the coordinates of the place where the missile enters the oncoming course are determined, as well as the missile and the control station are assigned to bring the missile to the oncoming course and destroy the target in the minimum time and transmit the missile data to the control station where the rocket is launched. On the rocket, its coordinates and speed are determined and transmitted, through the control station, to the DOS, where the trajectory and flight speed of the rocket to the point of entry into the oncoming course are calculated and transmitted to the control station, where commands are formed to guide the rocket to the place of entry into the oncoming course and transfer them to the rocket. The DOS determines the current coordinates of the aiming point for the missile, and also calculates the trajectory and speed of the missile to the target and transmits them to the control station, where commands are formed to aim the missile at the target and transmit them to the missile.;EFFECT: invention increases the probability of destroying the target.;1 cl, 1 dwg