FIELD: weapons.
SUBSTANCE: invention relates to corrected ammunition and can be used to guide jet projectiles at moving targets. Method of controlling the flight of jet projectiles (JP) involves numbering each projectile when installing the missile on a guide frame, guiding the launcher in the direction of a group of targets based on processing data from a radar station. Further, issuing a command to launch missiles from a command post when targets enter the firing zone, generating a computer for correction signals for each projectile and a target selected for it based on the difference in motion vectors of the projectile and the moving target, transmitting correcting signals to each numbered rocket projectile and control their trajectories due to release of blades. Additionally, the spectrum of signals reflected from the projectiles is processed and the angular velocities of rotation of the projectiles around the longitudinal axis are calculated, moment and direction of correcting action in horizontal and vertical plane are determined depending on angular velocity of shells rotation. Projectile flight control system consists of ground equipment consisting of a command post, a radio transmitter, a radar station, an electronic computer, a launcher, jet projectiles and on-board equipment of each projectile consisting of a receiver, a counter, AND logic elements, solenoids and blades.
EFFECT: expanded operating performances of the flight control system for rocket projectiles by taking into account the angular velocities of the projectiles when correcting their trajectories.
3 cl, 6 dwg
