| 姿控发动机点火逻辑研究 |
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| 引用本文： | 朱京. 姿控发动机点火逻辑研究[J]. 现代防御技术, 2007, 35(3): 42-45 |
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| 作者姓名： | 朱京 |
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| 作者单位： | 中国航天科工集团公司,二院二部,北京,100854 |
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| 摘 要： | 跟踪与分析国外先进防空导弹的姿控发动机控制技术,以美国PAC-3导弹为例,对姿控发动机组建立离散模型,然后采用一定的优化方法,对其点火方法作了研究,并提供仿真结果。
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| 关 键 词： | 姿控发动机 点火逻辑 离散模型 仿真 |
| 文章编号： | 1009-086X(2007)-03-0042-04 |
| 修稿时间： | 2007-03-10 |
Research on Ignition Logic of Attitude Control Engine |
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| ZHU Jing. Research on Ignition Logic of Attitude Control Engine[J]. Modern Defence Technology, 2007, 35(3): 42-45 |
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| Authors: | ZHU Jing |
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| Abstract: | The side jet technology of foreign advanced surface-to-air missiles is analyzed,disperse thrust models of 180 attitude control engines of patriot-III missile is built,and some optimized methods of ignite technology is studied,then the result of the simulation is presented. |
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| Keywords: | attitude control engine ignition logic disperse model simulation |
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