| GPS与弹道导弹INS组合制导方案初探 |
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| 引用本文： | 王永刚,袁建平,王明海. GPS与弹道导弹INS组合制导方案初探[J]. 航天控制, 1996, 0(2) |
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| 作者姓名： | 王永刚 袁建平 王明海 |
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| 作者单位： | 西北工业大学，二炮工程学院 |
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| 摘 要： | ＧＰＳ与弹道导弹ＩＮＳ组合制导方案初探王永刚，袁建平，王明海西北工业大学，二炮工程学院摘要＊针对弹道导弹的导航环境，提出了利用卡尔曼滤波构造的一种可用来提高弹道导弹射击精度的ＧＰＳ与惯导系统（ＩＮＳ）组合制导方案；并简要地阐述了利用该方案估计值对惯导...
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| 关 键 词： | 弹道导弹，组合制导，卡尔曼滤波 |
A Preliminary Investigation on GPS and INS of Ballistic Missile Integrated Guidance Scheme |
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| Wang Yonggang,Yuan Jianping,Wang Minghai. A Preliminary Investigation on GPS and INS of Ballistic Missile Integrated Guidance Scheme[J]. Aerospace Control, 1996, 0(2) |
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| Authors: | Wang Yonggang Yuan Jianping Wang Minghai |
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| Affiliation: | North West Industrial University The Second Artillery Engineering College |
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| Abstract: | In view of ballistic missile navigation environment,GPS and INS of ballistic missile integrated guidance scheme is studied in this paper,in which kalman filtering is used to raise ballistic missile impact accuracy and correction method of INS instrument error by estimated value of this scheme is stated briefly. The preliminary computation aimed at a certain ballistic missile shows that the integrated guidance scheme can make impact accuracy raise about an order of magnitude. |
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| Keywords: | Ballistic missile Integrated guidance Kalman filtering |
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