Calculation model of military aircraft suryiyability to a missile

作     者：杨哲 Li Shulin Li Shouan Zhou Li Zhang Jun 

作者机构：The Engineering InstituteAir Force Engineering University Aviation University of Air Force Air Force Equipment Research Academy 

出 版 物：《High Technology Letters》 (高技术通讯（英文版）)

年 卷 期：2014年第20卷第2期

页      面：117-123页

核心收录：

学科分类：082601[工学-武器系统与运用工程] 08[工学] 082501[工学-飞行器设计] 0826[工学-兵器科学与技术] 082503[工学-航空宇航制造工程] 082602[工学-兵器发射理论与技术] 0825[工学-航空宇航科学与技术] 

基　　金：Supported by the National High Technology Research and Development Programme of China(No.2009AA04Z406) the National NaturalScience Foundation of China(No.61172083) 

主　　题：survivability missile miss distance Monte Carlo kill probability 

摘      要：Since missiles are main threat against aircrafts in air war,a model is proposed for calculating the aircraft survivability to a *** hit characteristic of aircraft to a missile is analyzed,and then Monte Carlo method is applied to generate missile detonation location according to its distribution *** addition,based on the analysis of fragment trajectory and critical components,the intersection point of these two is *** the kill probability of critical component to a fragment can be calculated,and the aircraft survivability to a missile is obtained ***,the feasibility of the proposed method is *** results show that this method captures the basic effects of missile detonation locations on aircraft survivability,which may provide an effective reference to aircraft survivability research.