| 火箭弹末段脉冲修正方法研究 |
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| 引用本文： | 和黎伟,曹林平,胡杰. 火箭弹末段脉冲修正方法研究[J]. 弹箭与制导学报, 2007, 27(1): 154-156 |
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| 作者姓名： | 和黎伟 曹林平 胡杰 |
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| 作者单位： | 空军工程大学工程学院,西安,710038 |
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| 摘 要： | 立足实际,对火箭弹末制导技术进行了初步研究,提出了一种利用脉冲发动机实现火箭弹末段修正的方法,建立了脉冲修正的控制方程,并对其关键问题进行了探讨和分析。
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| 关 键 词： | 火箭弹 脉冲发动机 侧向偏差 脉冲修正 |
| 收稿时间： | 2006-05-23 |
| 修稿时间： | 2006-05-232006-08-05 |
A Study on Terminal Impulse Correction Means of Rockets |
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| HE Li-wei,CAO Lin-ping,HU Jie. A Study on Terminal Impulse Correction Means of Rockets[J]. Journal of Projectiles Rockets Missiles and Guidance, 2007, 27(1): 154-156 |
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| Authors: | HE Li-wei CAO Lin-ping HU Jie |
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| Abstract: | Based on practice, the airborne rockets guidance techniques have been studied elementarily, a terminal correction means of rockets using impulse engine has been put forward, the control equations of the impulse correction have been built, and the key problems have been studied and analyzed. |
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| Keywords: | rocket pulse engine side windage impulse correction |
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