| 空间拦截的末制导律设计 |
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| 引用本文： | 马克茂,史小平,王子才.空间拦截的末制导律设计[J].航天控制,1998,16(1):39-42,27. |
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| 作者姓名： | 马克茂 史小平 王子才 |
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| 作者单位： | 哈尔滨工业大学,150001 |
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| 摘 要： | 针对空间拦截问题的非线性模型及发动机的实际工作特性，基于变结构控制的思想，设计了易于工程实现的末制导律，并进行了数值仿真，得到了满意的结果。
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| 关 键 词： | 非线性系统 末制导 导引规律 截击机 |
| 修稿时间： | 1997年8月4日 |
Terminal Guidance Law Design in Space Interception |
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| Ma Kemao,Shi Xiaoping,Wang Zicai.Terminal Guidance Law Design in Space Interception[J].Aerospace Control,1998,16(1):39-42,27. |
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| Authors: | Ma Kemao Shi Xiaoping Wang Zicai |
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| Institution: | Ma Kemao Shi Xiaoping Wang Zicai Harbin Institute of Technology 150001 |
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| Abstract: | For the nonlinear models of the space interception and the operating characteristics of the engines, terminal guidance laws are proposed based on variable structure control (VSC) theory. The VSC based guidance law is easy to be realized in engineering. Numerical simulation is carried out with satisfactory results. |
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| Keywords: | Nonlinear system Terminal guidance Guidance law Interceptor |
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