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 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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