| 弹翼展开机构可靠性分析 |
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| 引用本文： | 刘英卫,郑冬青,侯俊平,张虹.弹翼展开机构可靠性分析[J].洪都科技,2001(1):1-5. |
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| 作者姓名： | 刘英卫 郑冬青 侯俊平 张虹 |
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| 作者单位： | 1. 洪都航空工业集团650所
2. 航天工业总公司三院三部,北京,100074 |
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| 摘 要： | 提出了一种折迭弹翼机构在指定时间内展开到位的可靠性分析方法，文中采用序列响应面法和全概率定理解决了涉及机构动力学随机参数及发射攻角随机参数的双重随机性问题，基于本方法所研制的RSMM程序应用效果良好。
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| 关 键 词： | 翼展 发射 攻角 响应面法 开机 机构 定时 程序 随机性 序列 |
| 修稿时间： | 2001年2月7日 |
Relibility Analysis for the Deploying Machanism of Missile Wing |
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| LiuYingwei and Zheng Dongqing.Relibility Analysis for the Deploying Machanism of Missile Wing[J].Hongdu Science and Technology,2001(1):1-5. |
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| Authors: | LiuYingwei and Zheng Dongqing |
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| Abstract: | This article provides a reliability analysis method for a kind of fold missile wing mechanism to be deployed to expected position within given time.The dual random problem that concern with the mechanism dynamics random data and launching AOA random data is solved by sequence response surface method and total probability theorem.The application effect of RSMM program developed based on the reliability analysis method is good. |
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| Keywords: | Mechanism reliability Response surface method Total probability theorem |
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