期刊文献+

子母拦截器集群拦截策略研究 被引量:2

Research on group interception strategy of multiple kill vehicle
下载PDF
导出
摘要 针对采用机动突防技术的弹道导弹弹头,提出了子母拦截器的拦截策略。通过使子母拦截器的每个子拦截器的初始拦截速度矢量相互偏置一个角度,从而在预计拦截距离上形成多个基准拦截点,这样可以有效地降低目标提前机动对子母拦截器命中概率造成的影响。建立子母重拦截器6自由度模型,模拟子母拦截器攻击过程,仿真结果表明这种拦截策略有助于提高子母拦截器对机动再入弹头的拦截命中概率。 An interception strategy is presented for intercepting ballistic missile bullet,which realized penetration by maneuvering trajectory.The interception strategy,which is different from traditional interception strategy,works by making the initial velocity vector of every kinetic energy interceptor(KEI) of multiple kill vehicle(MKV) offset an angle with each other,which ensures every KEI of MKV to aim at one interception point.So several interception points are preset.Compared with interception strategy which has only one presetting interception point,this interception strategy could decrease the influence resulting from a maneuver of bullet maked to the hit probability of MKV.A 6DOF MKV model is made for digital simulation.The result of digital simulation shows that the new interception strategy is effective.
出处 《系统工程与电子技术》 EI CSCD 北大核心 2010年第8期1700-1702,1710,共4页 Systems Engineering and Electronics
关键词 子母拦截器 拦截策略 数字仿真 机动域 multiple kill vehicle(MKV) interception strategy digital simulation maneuvering range
  • 相关文献

参考文献14

二级参考文献41

  • 1尚安利,于德海,顾文锦.基于动态二阶滑模控制算法的导弹自动驾驶仪设计[J].兵工学报,2006,27(1):50-53. 被引量:4
  • 2Golan O M, Rom H, Yehezkely O. System for destroying ballistic missiles[R]. US patent No. 6, 209, 820 B1, April 3,2001. 被引量:1
  • 3Golan O M, Shima T. Head pursuit guidance for hypervelocity interception[C] //Navigation and Control Conference, CP- 4885, AIAA, Washington, DC, 2004 : 1 - 12. 被引量:1
  • 4Golan O M, Shima T Precursor interceptor Guidance using the sliding mode approach [C]//Navigation and Control Conference, CP-4885, AIAA, Washington, DC, 2005:1- 15. 被引量:1
  • 5Adler F P. Missile guidance by three-dimensional proportional navigation[J]. Journal of Applied Physics,1956,27(5) : 500 - 507. 被引量:1
  • 6Lin C L, Chen Y Y. Design of fuzzy logic guidance law against high-speed target[J]. Journal of Guidance, Control and Dynamics ,2000,23(1) : 17 - 25. 被引量:1
  • 7Moon J, Kim K. Design of missile guidance law via variable structure control[J]. Journal of Guidance, Control and Dynamics, 2001, 24(4): 659-664. 被引量:1
  • 8Shkolnikov I. Shtessel Y, Lianos D. Robust missile autopilot design via high-order sliding mode control. [C]//Proceedings of AIAA guidance, navigation and control conference, AIAA paper 2000:2000- 3968. 被引量:1
  • 9Davila J, Fridman L. Second-order sliding mode observer for mechanical systems[J]. IEEE Trans. on Automatic Control , 2005,50(11) :1785- 1789. 被引量:1
  • 10[1]曾颍超,陆毓峰,霍秀芳,等.战术导弹弹道与姿态动力学[M]. 西安:西北工业大学出版社,1991. 被引量:1

共引文献77

同被引文献13

引证文献2

二级引证文献2

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