期刊文献+

高超声速飞行器滑翔再入性能评估 被引量:5

Research on Performance Evaluation for Hypersonic Reentry Glide Vehicle
下载PDF
导出
摘要 对高超声速滑翔再入飞行器性能评估的理论和方法进行了研究,并根据高超声速滑翔再入飞行器的特点,给出了高超声速滑翔再入飞行器性能评估的基本流程;通过对滑翔再入飞行器的系统分析,构建了该类飞行器的性能评估指标体系和评估模型;完成了性能评估软件的开发;对3种不同设计方案的性能进行了评估比较,结果表明该指标体系能够很好地反应此类飞行器的总体性能。 In this paper,performance evaluation theory and method are studied.Based on the characteristics of hypersonic glide re-entry vehicle,performance evaluation index system and evaluation model are built.The development of performance evaluation software is completed;Finally,the performance of different design schemes for hypersonic glide re-entry vehicle are evaluated,and the results show that the index system can reflect the overall performance of such vehicle.
出处 《火力与指挥控制》 CSCD 北大核心 2012年第8期120-123,共4页 Fire Control & Command Control
关键词 高超声速飞行器 性能评估 滑翔再入 hypersonic vehicle performance evaluation re-entry glide
  • 相关文献

参考文献9

  • 1崔尔杰.近空间飞行器研究发展现状及关键技术问题[J].力学进展,2009,39(6):658-673. 被引量:119
  • 2朱斯髙.导弹武器系统作战效能评估指标体系设计 研究[D].武汉:华中科技大学,2005:9-11.
  • 3马其东,方立恭.中远程舰空导弹武器作战效能指标体系研究[J].国防技术基础,2008(10):41-45. 被引量:9
  • 4肖凡,刘忠,黄金才.作战方案效能评估指标研究[J].军事运筹与系统工程,2006,20(2):41-45. 被引量:28
  • 5Paul A F. Simulation Model Design and Execution [J]. Building Digital Worlds?1995(11) :128-131.
  • 6Tao B R. Mathematical Simulation of Using Decoying and Killing Missiles to Counter Anti-Radiation Missiles[R]. ADA320857,1997.
  • 7Paul K D. Analytic Architecture for Capabilities-based Planning,Mission-system Analysis, and Transformation [ C ]//USA . RAND National Defense Research Institute ?2002.
  • 8Alexandria. Capabilities-based Planning ; The Road Ahead [ C ]//USA: RAND National Defense Research Institute,2004.
  • 9Wu J H,Doong H S,Lee C C,et al. A Methodology for Designing Form-Based Decision Support Systems [J]. Decision Support System, 2004, 36: 313-335.

二级参考文献40

共引文献150

同被引文献23

引证文献5

二级引证文献9

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