| 大气层内拦截战术弹道导弹制导控制技术研究 |
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| 引用本文： | 汪朝群.大气层内拦截战术弹道导弹制导控制技术研究[J].航天控制,2002,20(4):46-50. |
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| 作者姓名： | 汪朝群 |
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| 作者单位： | 上海机电工程研究所,上海,200233 |
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| 摘 要： | 就国家导弹防御系统而言 ,在大气层内对来袭弹道导弹的拦截与在大气层外实行拦击目标具有同样的实际意义。因此 ,新一代的防空导弹必须有一定的反战术导弹的能力。本文主要讨论在高空 2 0km以下作为低层防御的拦截导弹制导控制系统设计的一些方法。提出了拦截命中点的预测方法和拦截交会可采用的制导规律
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| 关 键 词： | 反导弹 制导和控制 制导规律 |
| 修稿时间： | 2002年7月2日 |
Study of Guidance and Control Technigue for ATBM In-atmosphere |
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| Wang ChaoqunShanghai Electrical and Mechanical Engineering Research Institute,Shanghai.Study of Guidance and Control Technigue for ATBM In-atmosphere[J].Aerospace Control,2002,20(4):46-50. |
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| Authors: | Wang ChaoqunShanghai Electrical and Mechanical Engineering Research Institute Shanghai |
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| Institution: | Wang ChaoqunShanghai Electrical and Mechanical Engineering Research Institute,Shanghai 200233 |
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| Abstract: | For National Missile Defence system, the research to intercept \%TBM\% target in atmosphere are of importance as well as engagement target extraatmospheric. A Developing surface to air missile have to possess anti \%TBM\% capability. The principle guidance techniqueson intercepting re entry \%TBM\% target in atmosphere that are range under 20\%km\% altitude are discussed in this paper. A model of estimating intercept position and guidance law about engagement reentry target is studied. |
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| Keywords: | Antimissile\ Guidance and control\ Guidanc law |
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