留言板

尊敬的读者、作者、审稿人, 关于本刊的投稿、审稿、编辑和出版的任何问题, 您可以本页添加留言。我们将尽快给您答复。谢谢您的支持!

姓名
邮箱
手机号码
标题
留言内容
验证码

防空导弹动能杀伤多层弹道优化MDO算法应用

刘恒军 姜 欢 陈万春

刘恒军, 姜 欢, 陈万春等 . 防空导弹动能杀伤多层弹道优化MDO算法应用[J]. 北京航空航天大学学报, 2010, 36(2): 145-149.
引用本文: 刘恒军, 姜 欢, 陈万春等 . 防空导弹动能杀伤多层弹道优化MDO算法应用[J]. 北京航空航天大学学报, 2010, 36(2): 145-149.
Liu Hengjun, Jiang Huan, Chen Wanchunet al. Application of MDO algorithm to multi-tier trajectory optimization design for a surface-to-air missile kinetic kill[J]. Journal of Beijing University of Aeronautics and Astronautics, 2010, 36(2): 145-149. (in Chinese)
Citation: Liu Hengjun, Jiang Huan, Chen Wanchunet al. Application of MDO algorithm to multi-tier trajectory optimization design for a surface-to-air missile kinetic kill[J]. Journal of Beijing University of Aeronautics and Astronautics, 2010, 36(2): 145-149. (in Chinese)

防空导弹动能杀伤多层弹道优化MDO算法应用

详细信息
    作者简介:

    刘恒军(1971-),男,辽宁铁岭人,博士生,lhengjun@163.com.

  • 中图分类号: TJ 765

Application of MDO algorithm to multi-tier trajectory optimization design for a surface-to-air missile kinetic kill

  • 摘要: 为了有效的毁伤目标,依据多层次优化方法提出了以杀伤概率优化为目标的防空导弹多层弹道优化模型.整个模型分为3层:导弹中制导段、导弹末制导段以及钨动能杆杀伤增强器动能毁伤目标阶段.将一个层次视为一个子系统,多层次弹道优化问题实质上就是多学科设计优化问题.通过系统分析与学科分析,提出了基于多学科设计优化理论和方法的多层弹道优化解决方法,用基于全局灵敏度方程的优化方法和一体化方法求解了系统优化问题.结果表明:两种方法都能有效解决多层次弹道优化问题,一体化方法的结果要更好一些.

     

  • [1] Phillips C A,Drake J C.Trajectory optimization for a SAM using a multi-tier approach .AIAA-94-4404,1994 [2] Phillips C A,Drake J C.Trajectory optimization for a missile using a multitier approach[J].Journal of Spacecraft and Rockets,2000,37(5):653-662 [3] 姜欢,周浩,陈万春,等.多层次法防空导弹弹道优化设计[J].北京航空航天大学学报,2008,34(2):135-139 Jiang Huan,Zhou Hao,Chen Wanchun,et al.The research of trajectory optimization design for a surface-to-air missile using a multilayer approach[J].Journal of Beijing University of Aeronautics and Astronautics,2008,34(2):135-139 (in Chinese) [4] Sobieszczanki-Sobieski J.Sensitivity of complex,internally coupled systems[J].AIAA Journal,1990,28(1):153-160 [5] Grossman B,Gurdal Z,Stauch G J,et al.Integrated aerodynamic/structure design of a sailplane wing[J].Journal of Aircraft,1988,25(9):855-860 [6] Zarchan P.Tactical and strategic missile guidance[M].3rd Edition.Washington,DC:American Institute of Aeronautics and Astronautics Inc,1998 [7] 李廷杰.导弹武器系统的效能及其分析[M].北京:国防工业出版社,2000 Li Tingjie.Effectiveness analysis for missile weapon systems[M].Beijing:National Defense Industry Press,2000 (in Chinese) [8] 秦如雯.钨杆杀伤增强器动能拦截TBM杀伤概率计算与仿真研究 .北京:北京航空航天大学宇航学院,2003 Qin Ruwen.Calculation and simulation of hit-to-kill probability to TBM by LE terminal interception .Beijing:School of Astronautics,Beijing University of Aeronautics and Astronautics,2003 (in Chinese) [9] Lloyd R M.Conventional warhead systems physics and engineering design[M].Washington,DC:American Institute of Aeronautics and Astronautic Inc,1998
  • 加载中
计量
  • 文章访问数:  3910
  • HTML全文浏览量:  333
  • PDF下载量:  1110
  • 被引次数: 0
出版历程
  • 收稿日期:  2008-07-20
  • 网络出版日期:  2010-02-28

目录

    /

    返回文章
    返回
    常见问答