METHOD FOR GUIDANCE OF GUIDED MISSILE Russian patent published in 2006 - IPC F41G3/22 

FIELD: military equipment, in particular, guidance of guided missiles.

SUBSTANCE: an additional feature of the aiming line is introduced at missile guidance, for example, of the circumference aligned with it. The motion of the guided missile along the aiming line is simulated, for example, by variation of the dimensions of the introduced circumference in proportion to the current distance between the guided missile and the target. The aiming of the aiming line is specified by means of use of the additional aiming mark whose position is balanced relative to the aiming point.

EFFECT: enhanced probability of hitting by guided missiles by 15-20%.

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