| 基于变系数的变前置角导引律设计 |
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| 引用本文： | 刘惠明,薛林,黄玲雅.基于变系数的变前置角导引律设计[J].现代防御技术,2005,33(5):16-18. |
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| 作者姓名： | 刘惠明 薛林 黄玲雅 |
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| 作者单位： | 中国航天科工集团公司,二院二部,北京,100854 |
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| 摘 要： | 对基于变系数的变前置角导引律进行了分析与研究,并从理论上给出了该导引规律的推导过程,然后对整个弹道系统建立仿真模型,并对理论设计的导引方法进行数学仿真计算。将所得到的仿真结果与经典的前置角法进行比较分析,得出最终结论。从而验证该方法的有效性。
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| 关 键 词： | 导引规律 前置角导引 变系数 |
| 文章编号： | 1009-086X(2005)05-0016-03 |
| 修稿时间： | 2004年9月28日 |
Study of the varying heading angle navigation law on the basis of varying coefficient method |
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| LIU Hui-ming,XUE Lin,HUANG Ling-ya.Study of the varying heading angle navigation law on the basis of varying coefficient method[J].Modern Defence Technology,2005,33(5):16-18. |
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| Authors: | LIU Hui-ming XUE Lin HUANG Ling-ya |
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| Abstract: | On the basis of varying coefficient method,varying heading angle navigation law is studied.Firstly,this navigation law is putted forward theoretically.Secondly,the simulation model is built for a whole ballistic system.And mathematical simulation calculation is performed for this theoretical navigation law.Finally,making a comparison between simulated data and classical heading angle method,an conclusion is given.The result shows the method is efficiency. |
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| Keywords: | Guidance law Heading angle navigation law Varying coefficient |
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