GUIDED MISSILE CONTROL METHOD Russian patent published in 2013 - IPC F41G3/00 

FIELD: weapons and ammunition.

SUBSTANCE: invention includes formation of stabilised vision line and its alignment with the target, launching of controllable missile and its catching by guidance system, measurement of vertical deviation and deviation in direction by guidance system of controllable missile from vision line in the course of its flight, automatic formation and transition of control commands to missile corresponding to these deviations, automatic generation and supply of signals corresponding to these commands to missile control means. In case of sighting device of several targets in sight the alignment of sighting vision line is done sequentially with each target, the range and angular coordinates of targets are defined and recorded relatively the shooting object, there defined is a reasonable sequence of re-targeting in case of possible near misses, this information is input into sighting device vision range, after controllable missile launching in direction of the first target and its catching by guidance system there measured is the time of its movement along flight trajectory, the information about missile missing this target is defined and transmitted to sighting device vision range, after that the sighting line is shifted to the second target according to the expressions (1) and (2), and in case of missing, to the following targets with defining and transmitting the information about missing the corresponding targets to sighting device vision range. After controllable missile catching there reduced are the stopped sizes of sighting device vision range to the value of one and a half maximum size of visible part of target image.

EFFECT: invention allows improving the efficiency of firing by controllable missiles.