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基于衰减因子的时变增益KALMAN滤波 被引量:1

Kalman Filter Based Adaptive Fading Memory
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摘要 常用的卡尔曼滤波器(KF,EKF)一般只适用于平稳的状态过程,当目标处于变化不大的过程时,目标状态突然变化时,KF和EKF将产生较大的估计偏差,甚至丢失目标.文中根据正交性原理,采用时变衰减因子,使得残差达到正交或近似正交,从而使滤波器在不确定模型下保持较好的鲁棒性.通过实时调节增益,促使测量残差近似正交,从而提高对机动目标的跟踪性能.仿真实验表明,应用该方法可以快速、稳定地完成目标运动要素的估计. The common Kalman filters generally apply to steady status process,when the target′s status changed suddenly KF and EKF′s filter effect becomes deteriorate.This article introduced adopting attenuation factor,made the measure remnants to hit decussate or close to decussate,make the filter keep better rubust under the uncertainty model though real-time adjusting gain,urged the measure remnants close to decussate,raise the on the trail of performance of mobile target.Simulation shows that the method can estimate the target′s status rapidly and stability.
作者 周浩 胡科强
出处 《武汉理工大学学报(交通科学与工程版)》 2011年第6期1234-1236,共3页 Journal of Wuhan University of Technology(Transportation Science & Engineering)
基金 总装备部预研项目资助(批准号:513040302)
关键词 状态估计 衰减因子 时变增益 status estimate attenuation factor real-time adjust gain
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  • 1YANG Yuanxi,GAO Weiguang.A new learning statistic for adaptive filter based on predicted residuals[J].Progress in Natural Science:Materials International,2006,16(8):833-837. 被引量:71
  • 2周浩,蒋兴舟,顾晓东.多声呐基阵时差定位无解问题研究[J].武汉理工大学学报(交通科学与工程版),2006,30(6):935-938. 被引量:5
  • 3Fawcett J A. Effect of course maneuvers on bearing- only range estimation [J]. IEEE Transactions on Acoustics, Speech and Signal Processing, 1988:36 (8): 1 193-1 199.
  • 4Jauffret C, Pillon D. Observability in passive target motion analysis[J]. IEEE Transactions on Aerospace and Electronic Systems. 1996, 32(4) :1290-1 300.
  • 5石章松,周丰,孙世岩.目标跟踪与数据融合理论及方法[M].北京:国防工业出版社,2007.
  • 6Ljung L. Asymptotic behavior of extended kalman filter as a pa2rameter estimator for linear systems [J]. IEEE Trans on Automat2ic Control, 1979,24 (1) : 36-50.
  • 7Tarn T, Zarbosky J. A practical non-driving filter[J]. AIAA Journal,1970,8(6): 1 127-1 133.
  • 8张金槐.自适应衰减记忆滤波中时变衰减因子的最佳选择[J].飞行器测控技术,1994(1):9-13. 被引量:8

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