期刊文献+

导弹喷射碎片威胁下的飞机易损性评估方法 被引量:4

Method for Assessing the Vulnerability of Aircraft to Spray Fragments of Missile
原文传递
导出
摘要 提出了一种飞机在导弹喷射碎片威胁下的易损性计算方法.该方法采用飞机及部件的有限元模型作为输入,首先以‘射击线扫描法’对飞机在单枚碎片打击下的易损性进行计算,然后以马尔可夫链法计算喷射碎片打击下的易损性.算例给出了飞机周围典型爆炸点位置引爆导弹战斗部的杀伤概率分布,并对导弹与飞机的交会区域进行了分析,验证了所提出方法的可行性与正确性.应用中表明,所提出的方法通用性强,易于实现;方法中考虑了导弹飞行速度、引爆点位置、装药质量比、碎片形状、空气阻力、飞机飞行高度及速度等因素,易损性计算结果具有一定的客观性;导弹碎片威胁下的易损性评估对于飞机生存力增强设计、导弹杀伤效能评估与引信优化设计具有指导意义. A method is proposed for calculating the vulnerability of aircraft to spray fragments of a missile. The input dada of aircraft or components for vulnerability assessment is organized by the finite element models. Firstly, the ' shot line scanning method' is used to calculate the single hit vulnerability of aircraft by a fragment of missile. Then, utilizing Markov-Chain method, the vulnerability of aircraft is obtained at the threat of multiple hits by spray fragments. Example has given the distributions of probabihty of kill at the typical missile detonation locations around the aircraft. In this example, the interaction regions of aircraft with fragments of missile are analyzed and the correctness and feasibihty of the proposed method are demonstrated. Application shows that ( 1 ) the proposed method is generic and easy to be programmed; (2) in order to provide a realistic and effective aircraft vulnerability assessment, the method has taken into consideration the factors such as missile velocity, missile detonation location, missile charge ratio, fragment shape, air drag, aircraft altitude, and aircraft velocity; (3) the vulnerability assessment of aircraft to fragments of missile is useful for aircraft survivability enhancement design, missile effectiveness assessment and optimizing missile fuse design.
出处 《系统工程理论与实践》 EI CSCD 北大核心 2007年第2期161-166,共6页 Systems Engineering-Theory & Practice
基金 国家自然科学基金(10372082) 中国博士后基金(20060400301)
关键词 易损性 杀伤概率 碎片 马尔可夫链 生存力 vulnerabihty kill probability fragment Markov-Chain survivability
  • 相关文献

参考文献12

  • 1GJB/Z 202.2001.飞机非核生存力通用指南[S].北京:国防科工委军标出版发行部出版,2002.
  • 2MIL-HDBK-336-1.Survivability aircraft nonnuclear general criteria[S].Washington DC:Dept.of Defense,1988.
  • 3Robert E.Ball.The Fundamentals of Aircraft Combat Survivability Analysis and Design[M].2nd Edition,Reston:AIAA,2003.
  • 4Robert E.Ball.The Fundamentals of Aircraft Combat Survivability Analysis and Design[M].1st Edition,New Y0rk:AIAA,1985.
  • 5John P.Fielding,Otsin Nilubol.Integraton of survivability assessment into combat aircraft design for operational effectiveness[A]//CAS 2004 CD-ROM Proceedings.Edinburgh:Optimage Ltd.,2004.
  • 6Angelo J.Kangalos,The effect of component redundancy upon aircraft combat survivability[D].Montery:Naval Postgraduate School,1983.
  • 7张金钟,王宏臣.解决多重命中易损性评价的一种改进的马尔可夫链法[J].沈阳航空工业学院学报,2001,18(1):87-89. 被引量:5
  • 8孙家广.计算机图形学[M].第三版,北京:清华大学出版社,1995.
  • 9裴扬,宋笔锋,韩庆.基于有限元模型的飞机几何描述算法研究[J].西北工业大学学报,2004,22(5):567-571. 被引量:9
  • 10MIL-HDBK-336-2.Survivability aircraft nonnuclear airframe[S].Washington DC:Dept.of Defense,1983.

二级参考文献10

  • 1倪建刚 严世英.马尔可夫转移概率矩阵一种实用求解方法及证明.航空基金论文集(4)[M].北京:航空工业出版社,1998..
  • 2[1]Gyllenspetz I M, Zabel P H. Comparison of US and Swedish Aerial Target Vulnerability Assessment Methodologies.AD-A095906, 1980
  • 3[9]Levy R, Dixon-Hiester L. Interactive Vulnerability Assessment Model. AIAA-91-3163
  • 4[10]Leonard F. Application of Aircraft Survivability Methodology to Spacecraft. AIAA-2002-1601
  • 5宋笔锋 韩庆.飞行器易损性指标计算的基本理论与方法(Ⅱ).现代防御技术,1999,27(5):36-42.
  • 6R P Boas.Entire Functions[]..1954
  • 7D Sofronou et al.The use of Nonregular Nets for Solving Two-di-mensional Nonstationary Problems in Gas Dynamics[].NumericalMethods in Fluid Dynamics.1984
  • 8何光武,张金钟.飞机武器系统易损性评价中几何描述研究[J].沈阳航空工业学院学报,1998,15(2):31-37. 被引量:3
  • 9张宝琳.计算两凸多边形交集面积的计算机算法[J].计算机工程与应用,2001,37(9):128-128. 被引量:16
  • 10徐元铭,龙伟,王永庆.军机易损性分析中多重遮挡投影面积计算[J].北京航空航天大学学报,2002,28(2):245-248. 被引量:3

共引文献25

同被引文献21

引证文献4

二级引证文献4

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部