| 引用本文: | 陈克俊.耗尽关机制导方法研究.[J].国防科技大学学报,1996,18(3):35-39.[点击复制] |
| Chen Kejun.An Approach to Depleted Shutdown Guidance[J].Journal of National University of Defense Technology,1996,18(3):35-39[点击复制] |
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| 耗尽关机制导方法研究 |
| 陈克俊 |
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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: |
| 本文研究了固体弹道导弹耗尽关机制导方法，提出了一种适用于无推力终止系统工作的固体弹道导弹，在要求能量随机耗尽条件下的混合制导模型，并进行仿真分析，论证了方案的可行性。 |
| 关键词: 固体弹道导弹，耗尽关机，制导 |
| DOI： |
| 投稿日期：1996-01-15 |
| 基金项目: |
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| An Approach to Depleted Shutdown Guidance |
| Chen Kejun |
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(Department of Automatic Control，NUDT，Changsha，410073)
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| Abstract: |
| In this paper，an approach to depleted shutdown guidance for solid ballistic missile is described. The complex guidance mathematical model applying to solid ballistic missile without thrust ending system is given under the condition that the fuel is depleted randomly. And then，it's correctness is proved by simulation. |
| Keywords: solid ballistic missile,depleted shutdown,guidance |
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