| 多击中条件下军用飞机二次效应评估方法研究 |
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| 引用本文： | 侯志强,孟维杰.多击中条件下军用飞机二次效应评估方法研究[J].兵工学报,2007,28(1):78-82. |
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| 作者姓名： | 侯志强 孟维杰 |
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| 作者单位： | 海军航空工程学院,山东,烟台,264001;92913部队,海南,加来,571820 |
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| 摘 要： | 用毁伤树和状态转换矩阵法，分非余度部件对非余度部件、非余度部件对余度部件、余度部件对非余度部件，余度部件对余度部件4种情况，对多击中条件下计入飞机部件二次效应的飞机易损性计算方法进行了讨论，并对毁伤树法和状态转换矩阵法在飞机二次效应计算中的应用进行了研究。
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| 关 键 词： | 概率论 飞机 多击中 易损性评估 二次效应 |
| 文章编号： | 1000-1093（2007）01-0078-05 |
| 修稿时间： | 07 8 2005 12:00AM |
A Study on Quadratic Effect Assessment Method of Military Aircraft Under Multiple Hit |
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| HOU Zhi-qiang,MENG Wei-jie.A Study on Quadratic Effect Assessment Method of Military Aircraft Under Multiple Hit[J].Acta Armamentarii,2007,28(1):78-82. |
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| Authors: | HOU Zhi-qiang MENG Wei-jie |
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| Affiliation: | 1. Naval Aeronautical Engineering Institute, Yantai 2o4001, Shandong,China;
2.No. 92913 Unit of PLA, Jialai 571820, Hainan, China |
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| Abstract: | The aircraft vulnerability assessment method was proposed by means of kill tree diagram and state transition matrix, under the conditions of multiple hit and counting quadratic effect, in four in- stances of the quadratic effects between components of nonredundant to nonredundant, nonredundant to redundant, the redundant to nonredundant, redundant to redundant. And the application of above mentioned methods to the c.alculation of the quadratic effect was studied. |
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| Keywords: | probability aircraft multiple hit vulnerability assessment quadratic effect |
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