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| 战略导弹制导精度分析途径的探讨 | |
| 引用本文： | 徐延万.战略导弹制导精度分析途径的探讨[J].航天控制,1991(Z1). |
| 作者姓名： | 徐延万 |
| 作者单位： | 北京航天自动控制研究所 |
| 摘 要： | 本文扼要介绍了制导精度分析的方法及其有关问题和工具误差模型系数分离的意义。为保证制导精度指标,进行制导误差分析和提高制导精度,探讨在我国国情下实现误差系数分离的途径是必要的。 |
| 关 键 词： | 洲际导弹 制导误差 工具误差 惯性测量装置 制导误差系数分离 误差补偿 环境函数 远程导弹 |
SEARCH FOR WAY OF GUIDANCE ACCURACY EVALUATION OF STRATEGIC MISSILE |
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| Xu yan wan Beijing Aerospoace Automatic Control Institute.SEARCH FOR WAY OF GUIDANCE ACCURACY EVALUATION OF STRATEGIC MISSILE[J].Aerospace Control,1991(Z1). | |
| Authors: | Xu yan wan Beijing Aerospoace Automatic Control Institute |
| Institution: | Xu yan wan Beijing Aerospoace Automatic Control Institute |
| Abstract: | This paper briefly introduced the method of guidance accuracy evaluation and its associated problems and the necessity of separationing the instrumental error model coefficients. It also describes problems about main ways for enhancing guidance accuracy, model recognition of guidance errors and guidance accuracy evaluation in our country. |
| Keywords: | Intercontinental missile Guidance error compensation Instrumental error Intertial measurement unit ~+Guidance error coefficient separation ~+Error compensation ~+Environmental function Long-range missile |
| 本文献已被 CNKI 等数据库收录！ | |