| 引用本文: | 郭振云,赵汉元.地基拦截弹对真目标进行拦截时的制导方案分析.[J].国防科技大学学报,1996,18(3):40-43.[点击复制] |
| Guo Zhenyun,Zhao Hanyuan.Analysis of the Guidance Scheme to Intercept the Actual Target[J].Journal of National University of Defense Technology,1996,18(3):40-43[点击复制] |
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| 地基拦截弹对真目标进行拦截时的制导方案分析 |
| 郭振云, 赵汉元 |
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(国防科技大学 自动控制系 湖南 长沙 410073)
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| 摘要: |
| 讨论了地基拦截弹对真目标(中近程弹道式导弹)进行拦截时的制导方案。根据拦截弹的飞行特点，将拦截过程分为初始段、中间段和拦截段，并采取了相应的制导方案。仿真结果表明，拦截具有较高的精度和良好的弹道特性，此方案是可行的。 |
| 关键词: 制导，拦截，真目标 |
| DOI： |
| 投稿日期：1996-01-20 |
| 基金项目: |
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| Analysis of the Guidance Scheme to Intercept the Actual Target |
| Guo Zhenyun, Zhao Hanyuan |
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(Department of Automatic Control，NUDT，Changsha，410073)
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| Abstract: |
| This paper studies the guidance scheme of the interception missile to intercept the actual target which is an intermediate or short range ballistic missile. According to the interception missile's flight characteristics, the trajectory is divided into three phases: primary，middle and interception phase，With variant guidance schemes. The simulation has proved that the schemes are feasible and the result is satisfactory. |
| Keywords: guidance,intercept,actual target |
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