摘要
介绍了飞机易损性评估的基本方法,包括威胁分析、致命性部件辨识、目标几何描述、杀伤概率及易损面积计算、易损性降低措施及权衡方法。给出了碎片对部件的杀伤概率及爆炸冲击波对结构的杀伤概率计算方法。所提出的方法对于飞机生存力设计以及提高与优化战斗部的杀伤效能有指导意义。
This paper presents the basic aircraft vulnerability assessment method. It includes the analysis of the threat environment,the process of identification of critical components, the target geometrical description method, the calculation methods of aircraft kill probability and vulnerable area, the vulnerability reduction concepts and method of vulnerability trade study. Also, It gives the calculation methods of component kill probability by a fragment and the kill probability of aircraft structure by burst wave. The proposed assessment method is useful for aircraft survivability design and optimizing warhead effectiveness.
出处
《弹箭与制导学报》
CSCD
北大核心
2004年第2期70-74,共5页
Journal of Projectiles,Rockets,Missiles and Guidance
基金
国家自然科学基金(19972056
10372082)
西北工业大学博士论文创新基金
关键词
易损性
生存力
致命性部件
易损面积
杀伤概率
vulnerability
survivability
critical component
vulnerable area
kill probability