发明名称 |
METHOD FOR NORMALIZATION OF SIGNAL OF COMPENSATION OF AXIAL ACCELERATION INFLUENCE |
摘要 |
FIELD: guided missile guidance systems. ^ SUBSTANCE: before normalization of missile control signals the engine operation time is preset, a priory evaluation of the projections of the missile axial acceleration onto the input axes of the antenna co-ordinate system of the homing head is preset. On completion of engine operation the present flight time is measured, the time before impact with the target is determined, and the evaluation of miss caused by missile axial acceleration is determined. The axial acceleration compensation signal is proportional to the evaluation of miss caused by missile axial acceleration. The obtained compensation signal is summed up with the signal of missile control according to the method of proportional navigation or its modifications. ^ EFFECT: enhanced accuracy of guidance. ^ 2 dwg |
申请公布号 |
RU2285886(C1) |
申请公布日期 |
2006.10.20 |
申请号 |
RU20050109894 |
申请日期 |
2005.04.05 |
申请人 |
OTKRYTOE AKTSIONERNOE OBSHCHESTVO "DOLGOPRUDNENSKOE NAUCHNO-PROIZVODSTVENNOE PREDPRIJATIE" |
发明人 |
AKIMOV VLADIMIR NIKOLAEVICH;ATASOV VLADIMIR ALEKSANDROVICH |
分类号 |
F41G7/22 |
主分类号 |
F41G7/22 |
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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