FIELD: missile guidance, applicable in complexes of tank and antitank armament, as well as in small-sized antiaircraft complexes.
SUBSTANCE: the method consists in orientation of the launcher with the missile in the direction of the control field at preset angles θ0, φ0 respectively in the vertical and horizontal planes, missile movement in the control field by means of shooting from the launcher, deployment of the missile controls and subsequent their deflection proportionally to the missile co-ordinates in the control field. The controls are deployed after time moment tp of the missile entry to the control field read off from the moment of launching, and determined according to the mathematical dependence.
EFFECT: enhanced accuracy of missile guidance.
3 dwg
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