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。
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.
出处
《航天控制》
CSCD
北大核心
1991年第S1期1-8,共8页
Aerospace Control
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
Intercontinental missile Guidance error compensation Instrumental error Intertial measurement unit ^+Guidance error coefficient separation ^+Error compensation ^+Environmental function Long-range missile.
