期刊文献+

临近空间高超声速目标MCT跟踪模型 被引量:11

Near Space Hypersonic Target MCT Tracking Model
下载PDF
导出
摘要 针对传统单模型不能有效跟踪临近空间高超声速目标的问题,提出了一种Modified Coordinate Turn(MCT)跟踪模型。根据临近空间高超声速目标在巡航段跳跃飞行的特点,假设目标角速度为一阶时间相关过程,借助"当前"统计模型的思想,对目标角速度进行实时修正,结合扩展卡尔曼滤波算法,实现对目标的稳定跟踪。Monte Carlo仿真结果表明,新模型能够实现对临近空间高超声速目标在巡航段跳跃飞行的准确跟踪,并且跟踪性能稳定,具有较强的实用性。 In view of the problem that the traditional single model can not track the near space hypersonic targets effectively, a modified coordinate turn (MCT) model was proposed. According to the characteristics of near space hypersonic targets while skip flying in cruise segment, assuming that the target angular velocity for singer process, with the help of the thought of "current" statistical model, revise the target angular velocity for real-time, combine with the extended Caiman filtering algorithm to achieve stable tracking. The Monte Carlo simula- tion results show that the new model can achieve tracking skip flying near space hypersonic target accurately in the cruise segment,and with more stability of the tracking performance and stronger practicality.
机构地区 空军预警学院
出处 《弹箭与制导学报》 CSCD 北大核心 2013年第1期185-188,194,共5页 Journal of Projectiles,Rockets,Missiles and Guidance
关键词 临近空间 高超声速 跳跃飞行 目标跟踪 near space hypersonic skip flying target tracking
  • 相关文献

参考文献8

  • 1关欣,赵静,何友.临近空间高超声速飞行器跟踪技术[J].四川兵工学报,2011,32(8):4-6. 被引量:32
  • 2关欣,赵静,张政超,何友.一种可行的高超声速飞行器跟踪算法[J].电讯技术,2011,51(8):80-84. 被引量:30
  • 3王华楠,刘高峰,顾雪峰.自适应转弯模型的交互多模型算法研究[J].弹箭与制导学报,2008,28(5):241-244. 被引量:4
  • 4Singer R A. Estimating optimal tracking filter performance for manned maneuvering targets [ J ]. IEEE Transactions on Aerospace and Electronic Systems, 1970,6(4) :473 -483.
  • 5Randall T Voland, Lawrence D Huebner, Charles R Mc- Clinton. X-43A Hypersonic vehicle technology development [ C ]//Acta Astronautica59,2006 : 181 - 191.
  • 6Zhang Min, Chen Wei-dong. Variable structure multiple model particle filter for maneuvering radar target tracking [ C ]//Proc. of Int. Microwave and Millimeter Wave Tech- nology, IEEE Press, 2010 : 1754 - 1757.
  • 7Graham Candler, Heath Johnson, Christopher Alba,et al. Analysis of modal growth on the leeward centerplane of the X-51 vehicle[ R]. USA: University of Minnesota,2009.
  • 8Robinson, Jeffrey S. An overview of NASA' s integrated design and engineering analysis (IDEA) environment[ R ]. American Institute of Aeronautics and Astronautics, 2011.

二级参考文献16

  • 1李涛,王宝树,乔向东.曲线模型的半自适应交互多模型跟踪方法[J].电子学报,2005,33(2):332-335. 被引量:13
  • 2李辉,沈莹,张安,程琤.交互式多模型目标跟踪的研究现状及发展趋势[J].火力与指挥控制,2006,31(11):1-4. 被引量:26
  • 3Li X R, Vesselinp Jilkov. Survey of maneuvering target tracking, Part Ⅰ: Dynamic models [J]. IEEE Transactions on Aerospace and Electronic Systems 2003,39(4) : 1346- 1348.
  • 4Li X R. Engineer's guide to variable-structure multiple-model estimation for tracking[M]. New York: Academic Press, 2001.
  • 5Singer R A. Estimation optimal tracking filter performance for manned maneuvering target [J]. IEEE Trans. Aero. Electron System, 1970 (6) : 472-483.
  • 6Anthony Colozza Initial feasibility Assessment of a High Altitude Long Endurance Airship [ R ], NASA CR-2003- 212724. 2003,12.
  • 7Johnston L A, Krishnamurthy V. An improvement to the interacting multiple model (IMM) algorithm [ J ]. IEEE Transactions on Signal Processing, 2001, 49 ( 12 ) : 2909 - 2923.
  • 8Mazor E, Aveebuch A, Bar-Shalom Y, et al. Interacting multiple model methods in target tracking: a survey [ J ]. IEEE Transactions on Aerospace and Electronic Systems, 1998,34(1) : 103 - 122.
  • 9Munir A, Atherton D P. Adaptive interacting multiple model algorithm for tracking a maneuvering target[J]. IEEE Proceedings Radar, Sonar and Navigation,1995,124(1):11 - 17.
  • 10Anthony Colozza, James Dolce. Initial feasibility Assessment of a High Altitude Long Endurance Airship[R]//NASA CR- 2003 - 212724. Columbia, USA: NASA, 2003.

共引文献52

同被引文献222

引证文献11

二级引证文献76

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