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单破片对导弹舱段毁伤的易损性快速分析方法 被引量:4

Fast Vulnerability Analysis Method of Missile Sections Under the Attack of Fragment
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摘要 针对标仿真模型建立、破片射击线以及弹目交会等问题,结合破片对目标的穿透毁伤判据,提出了一种破片对导弹舱段毁伤的计算方法,实现了在单破片打击下导弹舱段易损性的快速分析,并开发采用该方法为破片对导弹舱段毁伤概率进行快速计算的程序。根据计算结果得到不同条件下导弹不同舱段在破片打击毁伤下的易损性曲线,为巡航导弹目标的毁伤评估奠定了基础。 Aiming at the problems of target simulation model establishment,fragment shot line and the intersection of fragment and target,and combining with the criteria of fragment penetrating target,a calculation method of fragment damaging cruise missile sections was obtained,and the vulnerability of cruise missile sections under the attack of fragment was realized quickly.The method was developed as a program to calculate the damage probability of missile sections quickly.The vulnerability curves of different sections of missile under different conditions were obtained according to the calculation results,laid the foundation for the damage assessment of cruise missile targets.
作者 于滨 李翔宇 卢芳云 YU Bin;LI Xiangyu;LU Fangyun(College of Arts and Science, National University of Defense Technology, Changsha 410073, China)
出处 《兵器装备工程学报》 CAS 北大核心 2020年第12期82-86,共5页 Journal of Ordnance Equipment Engineering
关键词 破片 导弹 目标易损性 蒙特卡洛方法 数值仿真 fragment missile vulnerability Monte Carlo method numerical simulation
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