相关技术

临近空间高超声速目标MCT跟踪模型

  • 肖松 ,
  • 谭贤四 ,
  • 李志淮 ,
  • 王红
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  • 空军预警学院,武汉 430019

肖松(1985-),男,湖北武汉人,博士,研究方向:临近空间高超声速目标相关问题研究。

收稿日期: 2012-04-02

  网络出版日期: 2025-05-24

Near Space Hypersonic Target MCT Tracking Model

  • XIAO Song ,
  • TAN Xiansi ,
  • LI Zhihuai ,
  • WANG Hong
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  • Air Force Early Warning Academy, Wuhan 430019, China

Received date: 2012-04-02

  Online published: 2025-05-24

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ModifiedCoordinateTurn(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。MonteCarlo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。

本文引用格式

肖松 , 谭贤四 , 李志淮 , 王红 . 临近空间高超声速目标MCT跟踪模型[J]. 弹箭与制导学报, 2013 , 33(1) : 185 -188,194 . DOI: 10.15892/j.cnki.djzdxb.2013.01.022

Abstract

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 Calman filtering algorithm to achieve stable tracking. The Monte Carlo simulation 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.

参考文献

[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.
[2]
关欣, 赵静, 张政超,等. 一种可行的高超声速飞行器跟踪算法. 电讯技术, 2011,51(8): 80- 84.
[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.
[4]
Singer RA. Estimating optimal tracking filter performancefor manned maneuvering targets [J]. IEEE Transactions onAerospace and Electronic Systems, 1970, 6(4): 473- 483.
[5]
周宏仁, 敬忠良, 王培德. 机动目标跟踪[M]. 北京: 国防工业出版社, 1991.
[6]
Randall T Voland, Lawrence D Huebner, Charles R Mc-Clinton. X-43A Hypersonic vehicle technology development[C]//Acta Astronautica59,2006: 181 – 191.
[7]
Zhang Min, Chen Wei-dong. Variable structure multiplemodel particle filter for maneuvering radar target tracking[C]//Proc. of Int. Microwave and Millimeter Wave Tech-nology, IEEE Press, 2010: 1754 – 1757.
[8]
Graham Candler, Heath Johnson, Christopher Alba, et al. Analysis of modal growth on the leeward centerplane of theX-51 vehicle [R]. USA: University of Minnesota, 2009.
[9]
Robinson, Jeffrey S. An overview of NASA's integrateddesign and engineering analysis (IDEA) environment [R]. American Institute of Aeronautics and Astronautics, 2011.
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