期刊文献+

追踪法推广的数学建模与仿真 被引量:2

Generalized Mathematical Modelings and Simulations of Pursuit Guidance Method
下载PDF
导出
摘要 本文首先引入侧面拦截,扩大对追踪法的讨论;并从理论上给出了追踪法对弹道影响的分析证明;其次结合推广的比例导引法,构建了三维立体组合导引法,使导引方案更加灵活、有效。最后对拦截过程进行了相应的仿真,实验结果说明此方法形式简单、方便,具有实用价值。 The lateral intercept was proposed to extend a discussion on a pursuit navigation method;the analysis and proof of influence of the pursuit navigation method on the trajectory were theoretically given;3D solid combined navigation method was established by the generalized proportional navigation method and the pursuit navigation one to make the navigation scheme more flexible and effective.The intercept process was simulated by the combined navigation method.The simulated results show that the method is simple and convenietn to use and has practical value.
出处 《兵工学报》 EI CAS CSCD 北大核心 2009年第1期56-62,共7页 Acta Armamentarii
基金 国家自然科学基金资助项目(60604020)
关键词 飞行器控制 导航技术 追踪法 推广的比例导引法 复合导引法 过载 动能拦截器 control and navigation technology of aerocraft pursuer guidance generalized proportional navigation trajectory combined navigation guidance overload kinetic kill vehicle
  • 相关文献

参考文献7

二级参考文献20

  • 1欧建军,张斌,寇英信.寻的导弹导引规律研究[J].电光与控制,2005,12(2):31-33. 被引量:7
  • 2张中南,童幼堂,张卫峰.比例导引法导引弹道仿真研究[J].战术导弹技术,2005(2):56-59. 被引量:40
  • 3孙亚力,李宝.地空导弹拦截战术弹道导弹主要技术[J].地面防空武器,2005(1):6-16. 被引量:3
  • 4[1]李仲伯,张国友.制导武器[M].长沙:国防科技大学出版社,1993.70-89.
  • 5Yuan P J, et al.Solution of true proportional navigation for maneuvering and nonmaneuvering target.J of Guidance, Control and Dynamics, 1992, 15(1):268~271.
  • 6Yuan P J, et al.Solution of generalized proportional navigation for maneuvering and nonmaneuvering target.IEEE Transactions on AES, 1995, 31(1):469~474
  • 7Vathal S, et al.Analysis of generalized guidance law for homing missiles.IEEE Transactions on AES, 1995, 31(2):514~520
  • 8Shukla U S,Mahapatra P R.The proportional navigation dilemma-Pure or rrue.IEEE Transactions on AES, 1990, 26(2):382~392
  • 9Guelman M.A qualitative study of proportional navigation.IEEE Transactions on AES, 1971,7(4):637~643
  • 10Yang C D.Optimal pure proportional navigation for maneuvering targets.IEEE Transactions on AES, 1997,33(3):949~957

共引文献105

同被引文献18

  • 1吴开明,任云,吴立新,丁翠环,张仁和.海上战争中的动态海洋及动态海洋声学环境平台探讨[J].舰船电子工程,2008,28(7):178-182. 被引量:1
  • 2中国船舶重工重团公司.海军武器装备与海战场环 境概论[M].北京:海洋出版社,2007.
  • 3唐国金,罗亚中,雍恩米.航天器轨迹优化理论、方法及应用[M].北京:科学出版社,2012:44-47.
  • 4Tyan F,Shen J F. A shnple adaptive GIPN missile guidance law [ C ]//Proceedings of the 2006 American Control Conference. Minneapolis, Minnesota, USA : IEEE,2006:345 - 350.
  • 5Rusnak I. Optimal guidance laws with uncertain time-of-flight a- gainst maneuvering target and noisy measurements [ C ]//AIAA Guidance, Navigation, and Control Conference and Exhibit. Aus- tin, Texas : AIAA, 2003 : 5576-1 - 5576-8.
  • 6Ryoo C K,Cho H,Tahk M J. Time-to-go weighted optimal guid- ance with impact angle constraints [ J ]. IEEE Transactions on Control Systems Technology ,2006,14 ( 3 ) :483 - 492.
  • 7Wang Zhigang, Li Wei. Three dimensional optimal guidance law for micro missiles to attack maneuvering targets [ J ] Inforalatics in Control, Automation and Robotics,2012,133 (5) :283 - 286.
  • 8Menon P K A,Duke E L. Time-optimal aircraft pursuit evasion with a weapon envelope constraint [ J ]. Journal of Guidance Control and Dynamics, 1992,15 ( 2 ) :448 - 456.
  • 9Zhan Z H,Zhang J, Li Y. An efficient ant colony system based on receding horizon control for the aircraft arrival sequencing and scheduling problem[ J]. IEEE Transactions on Intelligent Transportation Systems, 2010,11 ( 2 ) : 399 - 412.
  • 10Huntington G T, Benson D, Anil V R. A comparison of accuracy and computational efficiency of three pseudospectral method [ J ]. AIAA Guidance, Navigation and Control Conference artd Exhibit South Carolina,2007 : 6405 - 6429.

引证文献2

二级引证文献3

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