| 高精度偏置比例导引末制导律研究 |
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| 引用本文： | 王辉,章虹虹.高精度偏置比例导引末制导律研究[J].航天控制,2009,27(6). |
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| 作者姓名： | 王辉 章虹虹 |
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| 作者单位： | 北京航天自动控制研究所,北京,100854 |
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| 摘 要： | 针对微型拦截器高精度制导控制要求,研究了偏置比例导引末制导控制技术,设计了偏置比例导引律,开发了偏航/滚动优化姿态控制系统,进行了六自由度数学仿真,结果表明:偏置比例导引末制导系统能够实现微型拦截器的高精度直接碰撞.
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| 关 键 词： | 微型拦截器 直接碰撞 偏置比例导引 姿态控制 |
The Development of High-precision Biased Proportional Navigation Terminal Guidance Control |
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| WANG Hui,ZHANG Honghong.The Development of High-precision Biased Proportional Navigation Terminal Guidance Control[J].Aerospace Control,2009,27(6). |
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| Authors: | WANG Hui ZHANG Honghong |
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| Institution: | WANG Hui ZHANG HonghongBeijing Aerospace Automatic Control Institute,Beijing 100854,China |
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| Abstract: | To meet the high-precision requirements of miniature kill vehicle, the technology of biased proportional navigation terminal guide control is developed and presented in this paper. Subsequently, the biased proportional navigation guidance system is designed and the yaw-roll optimized attitude control system is developed. Finally, the six-degree mathematical simulation is implemented. The results show that the biased proportional navigation terminal guidance control system can meet the high-precision requirements of central collision between the miniature kill vehicle and targeted object. |
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| Keywords: | Miniature kill vehicle Central collision Biased proportional navigation Attitude control |
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