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Terminal Guidance Law Design in Space Interception
Author(s): 
Pages: 39-42,27
Year: Issue:  1
Journal: AEROSPACE CONTROL

Keyword:  非线性系统末制导导引规律截击机;
Abstract: 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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