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| 大气层外动能拦截器顺轨拦截制导律设计 | |
| 引用本文： | 高乾,周林,王云鹏,刘杰,严道明.大气层外动能拦截器顺轨拦截制导律设计[J].导弹与航天运载技术,2011(6):1-5. |
| 作者姓名： | 高乾 周林 王云鹏 刘杰 严道明 |
| 作者单位： | 1. 空军大连通信士官学校,大连,116600;空军工程大学导弹学院,三原,713800 2. 空军工程大学导弹学院,三原,713800 3. 空军大连通信士官学校,大连,116600 |
| 摘 要： | 在分析中段拦截弹道导弹的优势和特点的基础上,提出顺轨拦截弹道导弹的方案.阐述顺轨拦截的概念,建立用于顺轨制导的弹道导弹和拦截器相对运动模型,基于二阶滑模控制理论设计二阶滑模非线性制导律.通过拦截器拦截弹道导弹的数字仿真验证了制导模型和制导律的正确性. |
| 关 键 词： | 动能拦截器 顺轨拦截 二阶滑模 制导律 |
A Guidance Law Design for Exoatmospheric Kinetic Interceptor |
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| Gao Qian,Zhou Lin,Wang Yunpeng,Liu Jie,Yan Daoming.A Guidance Law Design for Exoatmospheric Kinetic Interceptor[J].Missiles and Space Vehicles,2011(6):1-5. | |
| Authors: | Gao Qian Zhou Lin Wang Yunpeng Liu Jie Yan Daoming |
| Affiliation: | 1(1.Dalian Communication Sergeant School of Air Force,Dalian,116600; 2.Missile Institute,Air Force Engineering University,Sanyuan,713800) |
| Abstract: | This paper analyzed the predominance and peculiarity of midcourse intercept.The concept of intercepting along track is brought forward on basis of the relative analysis.Firstly,the concept of intercepting along track is introduced.Secondly,relative motion model of ballistic missile and interceptor is established for along track guide.Finally,it designed second-order sliding mode nonlinear guidance law based on the second-order sliding mode control theory.Numerical simulation results verified the guidance model and the effectiveness of the guidance law. |
| Keywords: | Kinetic kill vehicle Interception along track Second-order sliding mode Guidance law |
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