| 末端导引律综述 |
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| 引用本文： | 孙胜,张华明,周荻.末端导引律综述[J].航天控制,2012,30(1):86-96. |
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| 作者姓名： | 孙胜 张华明 周荻 |
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| 作者单位： | 1. 北京航天自动控制研究所,北京,100854
2. 哈尔滨工业大学控制科学与工程系,哈尔滨,150001 |
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| 基金项目： | 国家自然科学基金，教育部新世纪优秀人才支撑计划 |
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| 摘 要： | 为了提高制导精度,在末制导过程中就必须采用性能更优良的导引律,本文针对各种末端导引方法的特点及其发展情况进行了研究分析与总结,包括各种经典导引律、各种基于现代控制理论设计的导引律以及针对各种特定工程应用背景的导引律等,可为今后导弹导引律的改进和设计提供参考.
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| 关 键 词： | 末端导引律 综述 制导性能 |
A Survey of Terminal Guidance Law |
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| SUN Sheng
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ZHANG Huaming
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ZHOU Di.A Survey of Terminal Guidance Law[J].Aerospace Control,2012,30(1):86-96. |
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| Authors: | SUN Sheng ZHANG Huaming ZHOU Di |
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| Institution: | 1.Beijing Aerospace Automatic Control Institute,Beijing 100854,China 2.Harbin Institute of Technology,Department of Control Science and Engineering,Harbin 150001,China |
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| Abstract: | In order to improve guidance precision,the guidance law that provides better performance has to be involved during the terminal guidance.All kinds of terminal guidance laws are investigated,including various guidance laws based on classical and modern control theory along with those designed for specific engineering application background.And a summary is given to serve as a reference for the improvement and design of missile in future. |
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| Keywords: | Terminal guidance law Survey Guidance performance |
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