FIRING METHOD OF SEPARATE CONTROLLABLE SEPARATELY-CHARGED PROJECTILE ROCKET AND PROJECTILE FOR IMPLEMENTATION THEREOF Russian patent published in 2019 - IPC F42B15/00 

FIELD: weapons.

SUBSTANCE: group of inventions relates to artillery equipment, in particular to tank controlled projectiles of separate loading with parts of projectile attached in barrel channel. According to the firing method separate missile of projectile parts is performed by rocket projectile of separate loading. These parts are coupled in the barrel bore with an arbitrary mutual angular position. Control commands are generated in executive coordinate system of tail control compartment. Permanent magnet is arranged on interface surface of head control compartment. Magnetoresistive transducer of angular position is arranged on tail surface of tail section. After projectile start-up, angle of mutual position of compartments is additionally measured and memorized. In the flight of the missile, control commands are sent from the ground control equipment or from the homing head to the coordinate converter of the head compartment for the onboard computer. Coordinates of the target are converted from the measuring system of coordinates of the head compartment to the executive coordinate system of the tail control compartment as per analytical dependencies.

EFFECT: technical result is higher accuracy of guidance of separate projectile with parts of projectile jointed in barrel with arbitrary angle of mutual orientation.

3 cl, 2 dwg