METHOD FOR GUIDANCE OF GUIDED MISSILE Russian patent published in 2007 - IPC F41G3/22 

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

SUBSTANCE: the method consists in the fact that additional symptoms of maximum probable and effective ranges of guidance of guided missiles of the used types are introduced, the positions of the aiming lines and the distance between the guided missile and the target in the form of a respectively adjusted one with the aiming line of the circumference and its dimension. The most suitable type and mode of guided missile guidance for destruction of the target is selected. The motion of the intercepted missile along the aiming line is simulated by varying the dimension of the introduced circumference proportionally to the current distance between the guided missile and the target. The aiming of the aiming line is specified by using the additional indication of the positioned of the aiming line as an indicator of the distance between the guided missile and the target and an additional aiming mark; whose position is symmetrized relative to the point of aiming and the brightness of the aiming marks is periodically changed.

EFFECT: enhanced noise immunity and accuracy of guidance of the guided missiles, which enhances the efficiency of fire in the conditions of action of interference.

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