发明名称 MISSILE GUIDANCE METHOD AND DEVICE FOR ITS IMPLEMENTATION
摘要 FIELD: weapons and ammunition. ^ SUBSTANCE: according to missile guidance level and device for its implementation at irradiation of radiation detector with control beam there determined with coordinates in control field at the moments of beginning and end of irradiation. Average value of coordinates of control moments at the moments of beginning and end of irradiation. Missile coordinates are formed as per average value of coordinates of control beam. In missile guidance system to the missile there additionally introduced is unit for shaping strobe pulses, register of code record of the irradiation beginning, irradiation end code record and averaging unit. ^ EFFECT: improving accuracy of determination of missile coordinates on control field, accuracy of missile guidance and probability of target killing. ^ 2 cl, 1 dwg
申请公布号 RU2431107(C1) 申请公布日期 2011.10.10
申请号 RU20100112078 申请日期 2010.03.29
申请人 GOSUDARSTVENNOE UNITARNOE PREDPRIJATIE "KONSTRUKTORSKOE BJURO PRIBOROSTROENIJA" 发明人 GUSEV ANDREJ VIKTOROVICH;KUZNETSOV VLADIMIR MARKOVICH;OVSENEV SERGEJ SERGEEVICH;TARASOV VIKTOR IVANOVICH;SEMASHKINA RAISA MIKHAJLOVNA;KUSHNIKOV DMITRIJ VJACHESLAVOVICH
分类号 F41G7/24 主分类号 F41G7/24
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