FIELD: weapons and ammunition.
SUBSTANCE: in compliance with proposed invention, possible trajectory of guide missile in laser-beam guidance system raster is determined. Points of possible efficient suppression of controlled laser radiation are computed with due allowance for current interference conditions, terrain relief, season day time and weather in missile trajectory. Most suitable points of power suppression of controlled laser radiation are selected from possible alternatives. Laser radiation of interference laser generator is used to affect the points of most suitable suppression that ensures power SNR smaller than that of missile onboard photo receiver, thus, allowing killing the missile control system.
EFFECT: expanded combat performances, higher probability of laser guidance suppression.
3 dwg
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Authors
Dates
2010-05-27—Published
2008-11-24—Filed