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

双机编队空空导弹协同发射区模拟仿真分析

刁兴华 方洋旺 伍友利 付小飞

刁兴华, 方洋旺, 伍友利, 等 . 双机编队空空导弹协同发射区模拟仿真分析[J]. 北京航空航天大学学报, 2014, 40(3): 370-376. doi: 10.13700/j.bh.1001-5965.2013.0237
引用本文: 刁兴华, 方洋旺, 伍友利, 等 . 双机编队空空导弹协同发射区模拟仿真分析[J]. 北京航空航天大学学报, 2014, 40(3): 370-376. doi: 10.13700/j.bh.1001-5965.2013.0237
Diao Xinghua, Fang Yangwang, Wu Youli, et al. Simulation analysis on air-to-air missile allowable launch envelope about cooperative air combat of multi-fighter formation[J]. Journal of Beijing University of Aeronautics and Astronautics, 2014, 40(3): 370-376. doi: 10.13700/j.bh.1001-5965.2013.0237(in Chinese)
Citation: Diao Xinghua, Fang Yangwang, Wu Youli, et al. Simulation analysis on air-to-air missile allowable launch envelope about cooperative air combat of multi-fighter formation[J]. Journal of Beijing University of Aeronautics and Astronautics, 2014, 40(3): 370-376. doi: 10.13700/j.bh.1001-5965.2013.0237(in Chinese)

双机编队空空导弹协同发射区模拟仿真分析

doi: 10.13700/j.bh.1001-5965.2013.0237
详细信息
  • 中图分类号: TJ762

Simulation analysis on air-to-air missile allowable launch envelope about cooperative air combat of multi-fighter formation

  • 摘要: 对双机编队协同作战条件下的空空导弹发射区进行了仿真研究.通过分析单机作战条件下空空导弹实际发射区的形成机理,结合协同作战条件下空空导弹发射/制导方式,得出协同发射区的定义;建立导弹、目标和载机的运动模型,分析了影响协同发射区的导弹、发射机及制导机约束条件,采用黄金分割的方法搜索协同发射区的远界和近界,对不同参数影响下的双机协同发射区进行了仿真实验.仿真结果证实双机协同能有效扩大导弹允许发射区且协同发射区受制导机及导弹参数的影响.

     

  • [1] 聂心东,姜文志,刘兵.空舰协同制导下舰空导弹杀伤区低界研究[J].电光与控制,2009,16(6):24-27 Nie Xindong,Jiang Wenzhi,Liu Bing.Study on low boundary of ship-to-air missile killing zone based on coordinated guidance[J].Electronics Optics & Control,2009,16(6):24-27(in Chinese)
    [2] 聂心东,帅鹏,姜文志.舰舰协同制导下舰空导弹水平杀伤区研究[J].指挥控制与仿真,2009,31(3):29-31 Nie Xindong,Shuai Peng,Jiang Wenzhi.Study of ship-to-air missile horizontal launch envelops guided by ship-by-ship[J].Command Control & Simulation,2009,31(3):29-31(in Chinese)
    [3] 张平,方洋旺,乔治军,等.超视距空空导弹协同允许发射区解算方法[J].电光与控制,2012,19(3):12-16 Zhang Ping,Fang Yangwang,Qiao Zhijun,et al.A method for calculating allowable launch envelope of over-the-horizon air-to-air missile[J].Electronics Optics & Control,2012,19(3):12-16(in Chinese)
    [4] 寇英信,付昭旺,冯国强,等.网络瞄准下空空导弹允许发射区模拟仿真分析[J].空军工程大学学报:自然科学版,2012,13(2):24-28 Kou Yingxin,Fu Zhaowang,Feng Guoqiang,et al.Simulation analysis on air-to-air missile allowable launch envelope in networked targeting[J].Journal of Air Force Engineering University:Natural Science Edition,2012,13(2):24-28(in Chinese)
    [5] Dhar A,Ghose D.Capture region for a realistic TPN guidance law[J].IEEE Transactions on Aerospace and Electronic Systems,1993,29(3):995-1003
    [6] Ghose D.Capture region for true proportional navigation guidance with nonzero miss-distance[J].Journal of Guidance,Control and Dynamics,1994,17(3):627-628
    [7] 周志刚.航空综合火力控制原理[M].北京:国防工业出版社,2008:252-259 Zhou Zhigang.Aviation integrated fire control system[M].Beijing:National Defense Industry Press,2008:252-259(in Chinese)
    [8] Kumar V,Leonard N,Morse A S.Cooperative control[M].New York:Springer-Verlag,2003
    [9] 肖冰松,方洋旺,胡诗国,等.多机空战协同制导决策方法[J].系统工程与电子技术,2009,31(3):610-612 Xiao Bingsong,Fang Yangwang,Hu Shiguo,et al.Decision methods of cooperative guidance for multi-aircraft air combat[J].Systems Engineering and Electronics,2009,31(3):610-612(in Chinese)
    [10] Fax J A,Murray R M.Information flow and cooperative control of vehicle formations[J].IEEE Trans on Automatic Control,2004,49(9):1465-1476
    [11] 张斌,黄俊,寇英信,等.双机合作下远程空空导弹攻击技术[J].火力与指挥控制,2009,34(5):92-94 Zhang Bin,Huang Jun,Kou Yingxin,et al.Research on technology of long-range air-to-air missile attacking by two cooperative fighters[J].Fire Control & Command Control,2009, 34(5):92-94(in Chinese)
    [12] Siouris G M.Missile guidance and control systems[M].New York:Springer-Verlag,2004
    [13] Fleeman E L.Tactical missile design[M].[S.l.]:American Institute of Aeronautics and Astronautics Inc,2001
    [14] Acevedo R A.Valued information at the right time (VIRT) and the navy's cooperative engagement capability (CEC) -a win/win proposition[D].Monterey:Naval Postgraduate School,2006
    [15] 刘志华,季海波.数据链技术在战术武器中的应用方案研究[J].航天控制,2009,27(3):61-64 Liu Zhihua,Ji Haibo.Study of application project of data link technologies in tactical weapons[J].Aerospace Control,2009,27(3):61-64(in Chinese)
    [16] 郑志伟.空空导弹系统概论[M].北京:兵器工业出版社,1997 Zheng Zhiwei.Air to air missile system[M].Beijing:Weapon Industry Press,1997(in Chinese)
    [17] 张平,方洋旺,金冲,等.空空导弹攻击区实时解算的新方法[J].弹道学报,2010,22(4):11-14 Zhang Ping,Fang Yangwang,Jin Chong,et al.A new method of real-time calculation about air-to-air missile launch envelopes[J].Journal of Ballistics,2010,22(4):11-14(in Chinese)
    [18] 陈宝林.最优化理论与算法[M].北京:清华大学出版社,2007 Chen Baolin.The theory and algorithms of optimization[M].Beijing:Tsinghua University Press,2007(in Chinese)
    [19] Karelahti J,Virtanen K,Raivio T.Near-optimal missile avoidance trajectories via receding horizon control[J].Journal of Guidance,Control and Dynamics,2007,30(5):1287-1298
  • 加载中
计量
  • 文章访问数:  1532
  • HTML全文浏览量:  197
  • PDF下载量:  685
  • 被引次数: 0
出版历程
  • 收稿日期:  2013-05-02
  • 网络出版日期:  2014-03-20

目录

    /

    返回文章
    返回
    常见问答