GUIDED MISSILE CONTROL METHOD Russian patent published in 2011 - IPC F41G3/00 

FIELD: weapons and ammunition.

SUBSTANCE: at simultaneous missile capture there performed is periodic change of brightness of laying mark with the appropriate guidance system. Availability and time of joint capture of guided missile is determined simultaneously in both guidance systems; brightness change frequency of both laying marks is doubled by this time; guidance is stopped at target damage or lapse of flight time of guided missile to it. The proposed invention provides improvement of guidance efficiency of guided missiles by 5-10%, protection of firing weapon system, security of their use, as well as optimises time characteristics of guidance process by saving 1-2 seconds when each target is fired.

EFFECT: possibility of simultaneous target capture, as well as alternate or joint capture of guided missile with possibility of its further guidance with any system.