期刊文献+

弹道导弹打击航空母舰末制导有效区的确定与评估 被引量:2

Determination and Evaluation of Effective Range for Terminal Guidance Ballistic Missile Attacking Aircraft Carrier
下载PDF
导出
摘要 在地地弹道式导弹与航空母舰攻防对抗中,需要研究航母是否在导弹进攻的有效区内。针对具有末制导的弹道式导弹具有再入机动变轨特性,建立了导弹再入机动飞行模型,提出了导弹在不同的再入条件下,对其飞行弹道及机动能力进行仿真计算的方法,通过仿真确定出了导弹打击航空母舰的有效区域。在此基础上,探讨了导弹在以不同的再入姿态、不同的再入飞行高度实施末制导时,导弹落点的有效区域、边界外形及有效区的变化范围。从所得结果来看,所建模型及仿真方法正确可行,在一定程度上解决了弹道导弹打击航空母舰战斗群作战保障急需解决的一些问题。 In the counter of ground-to-ground ballistic missile against aircraft carrier, it is necessary to know whether the carrier is in the effective fire range. Aiming at the characteristic of the mobile trajectory while terminal guidance missile enters atmosphere again, this paper establishes its re-entry mobile trajectory model, presents the simulative and calculative 'method in different reentry conditions. By simulation, the effective range for ballistic missile attacking carrier is determined. Based on this, the paper researches the change of effective range of terminal guidance when the missile is taken under different reentry attitude and height. This model and its simulation are provided with correct and feasible. It is useful to solve some urgent problems of ballistic missile countermining aircraft carrier group.
出处 《指挥控制与仿真》 2006年第4期6-9,共4页 Command Control & Simulation
基金 第二炮兵武器装备发展资助项目(EPF03016)
关键词 弹道导弹 航空母舰 末制导 有效区 评估 ballistic missiles aircraft carrier terminal guidance effective range evaluation
  • 相关文献

参考文献2

  • 1张毅 杨辉耀 等.弹道导弹弹道学[M].长沙:国防科技大学出版社,1999.8-20.
  • 2[3]王永刚,刘新学.地地导弹制导原理与方法[M].西安:第二炮兵工程学院,2002.

共引文献23

同被引文献13

  • 1许黎明,李讯.“标准”-3导弹独臂支撑海军战区弹道导弹防御[J].现代舰船,2005,0(07A):32-37. 被引量:2
  • 2李文皓,张珩.无人机编队飞行技术的研究现状与展望[J].飞行力学,2007,25(1):9-11. 被引量:38
  • 3Zarchan P. Complete Statistical analysis of nonlinear missile guidance systems- SLAM [J]. Journal of Guidance and Control, 1979, 2(1):71-78.
  • 4Zarchan P. Representation of realistic evasive maneuvers by the use of shaping filters[J]. Journal of Guidance and Control,1979 ,2 (4) : 71 - 78.
  • 5Fitzgerald R J. Shaping filters for disturbances with random starting times[J]. Journal of Guidance and Control, 1979,2(2) :152-154.
  • 6Nesline F W and Zarchan P. Miss distance dynamics in homing missiles[C]// Proceedings of AIAA Guidance and Control Conference. AIAA. New York, 1984, Aug. 84-98.
  • 7Mark Stokes. China' s evolving conventional strategic strike ca- pability. Project 2049 Institute, 2009(9).
  • 8Eric Hagt, Matthew D. China' s anti-ship ballistic missile-developments and missing links. Naval War College Review, 2009 (4).
  • 9Office of the Secretary of Defense, Washington, DC. Unmanned systems roadmap 2007-2032, 2007.
  • 10Thomas P E, Robert O W. The unmanned combat air system carrier demonstration program : A New Dawn For Naval Aviation. Center for Strategic and Budgetary Assessments, 2007 (5).

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