首页 | 本学科首页   官方微博 | 高级检索  
     检索      

高超声速巡航导弹攻防对抗仿真研究
引用本文:郑祥品.高超声速巡航导弹攻防对抗仿真研究[J].科学技术与工程,2012,12(24):6113-6116,6131.
作者姓名:郑祥品
作者单位:西北工业大学
摘    要:在当前复杂作战环境下,对导弹武器系统进行攻防对抗研究是很有必要的。针对攻防对抗这一复杂的动态过程,本文建立了高超声速巡航导弹攻防对抗仿真模型,并在此模型中,分别给出了结果评判模型、作战环境模型和对抗仿真模型。并根据所建立的仿真模型,计算出高超声速巡航导弹的突防概率。仿真算例结果表明,减小高超声速巡航导弹的雷达反射截面积RCS和增大高超声速巡航导弹的巡航速度是提高其突防效能的重要手段。

关 键 词:高超声速巡航导弹  攻防对抗  建模仿真
收稿时间:2012/4/18 0:00:00
修稿时间:5/18/2012 7:12:47 PM

Study About Hypersonic Cruise Missile Combat Engagement Simulation
zhengxiangpin.Study About Hypersonic Cruise Missile Combat Engagement Simulation[J].Science Technology and Engineering,2012,12(24):6113-6116,6131.
Authors:zhengxiangpin
Institution:(School of Astronautics,Northwestern Polytechnical Universiry,Xi′an 710072,P.R.China)
Abstract:During current complex combat conditions, investigation of combat engagement of a new technology missile weapon system is necessary. Aimed at the complex dynamic course of combat engagement, a framework for hypersonic cruise missile combat engagement simulation is established. The combat engagement models of offensive side and defensive side are established in this framework, as well as combat environment models and damage probability of the hypersonic cruise missile are computed. Finally, penetration effectiveness of the hypersonic cruise missile is given. The results shows that reducing the RCS and increasing the cruise velocity of the hypersonic cruise missile are two important approaches to improve the penetration effectiveness.
Keywords:hypersonic cruise missile combat engagement modeling and simulation
本文献已被 CNKI 等数据库收录!
点击此处可从《科学技术与工程》浏览原始摘要信息
点击此处可从《科学技术与工程》下载免费的PDF全文
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号