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自适应无迹增量滤波方法

傅惠民 吴云章 娄泰山

傅惠民, 吴云章, 娄泰山. 自适应无迹增量滤波方法[J]. 航空动力学报, 2013, 28(2): 259-263.
引用本文: 傅惠民, 吴云章, 娄泰山. 自适应无迹增量滤波方法[J]. 航空动力学报, 2013, 28(2): 259-263.
FU Hui-min, WU Yun-zhang, LOU Tai-shan. Adaptive unscented incremental filter method[J]. Journal of Aerospace Power, 2013, 28(2): 259-263.
Citation: FU Hui-min, WU Yun-zhang, LOU Tai-shan. Adaptive unscented incremental filter method[J]. Journal of Aerospace Power, 2013, 28(2): 259-263.

自适应无迹增量滤波方法

基金项目: 国家重点基础研究发展计划(2012CB720000)

Adaptive unscented incremental filter method

  • 摘要: 提出自适应无迹增量滤波(AUIF)的概念和定义,建立自适应无迹增量滤波模型及其分析方法,给出递推算法.传统的滤波方法极少关注量测方程的系统误差.在许多实际情况(如深空探测),量测方程由于受环境因素及测量设备不稳定等影响往往无法进行验证或校准而存在未知的系统误差,并且模型参数和噪声统计量也具有不确定性.这种不确定性会使递推过程产生较大误差,甚至导致发散,从而降低滤波精度.提出的AUIF能够成功消除这种未知的系统误差,也能够实时估计变化的噪声统计量,提高滤波精度.该方法计算简单,便于工程应用.

     

  • [1] Sunahara Y.An approximate method of state estimation for nonlinear dynamical systems[J].Journal Basic Engineering,1970,9(2):385-393.
    [2] Fujimoto O,Okita Y,Ozaki S.Nonlinearity compensation extended Kalman filter and its application to target motion[J].Oki Technical Review,1997,63(159):1-12.
    [3] Arulampalam M S,Maskell S,Cordon N,et al.A tutorial on particle filters for online nonlinear/non-Gaussian Bayesian tracking[J].IEEE Trans on Signal Processing,2002,50(2):174-188.
    [4] 赵琳,王小旭,薛红香,等.带噪声统计估计器的Unscented卡尔曼滤波器设计[J].控制与决策,2009, 24(10):1483-1488. ZHAO Lin,WANG Xiaoxu,XUE Hongxiang,et al.Design of unscented Kalman filter with noise statistic estimator[J].Control and Decision,2009,24(10):1483-1488.(in Chinese)
    [5] 郝钢,叶秀芬.多传感器加权观测融合自适应UKF滤波器[J].宇航学报,2011,32(6):1400-1408. HAO Gang,YE Xiufen.Adaptive weighted measurement fusion unscented Kalman filter for multisensor system[J].Journal of Astronautics,2011,32(6):1400-1408.(in Chinese)
    [6] Julier S,Uhlmann J K.A new extension of Kalman filter to nonlinear systems[C]//Proceedings of AeroSense:the 11th International Symposium Aerospace/Defense Sensing,Simulation and Controls.Orlando:SPIE,1997:182-193.
    [7] Julier S J,Uhlmauu J K.Unscented filter and nonlinear estimation[J].Proceedings of the IEEE,2004,92(3):401-402.
    [8] Tamer A,Miibeccel D.An adaptive unscented Kalman filter for tightly coupled INS/GPS integration[C]//Proceedings of Position Location and Navigation Symposium(PLANs).Mytle Beach,SC:IEEE,2012:389-395.
    [9] JIANG Zhe,SONG Qi,HE Yuqing,et al.A novel adaptive unscented Kalman filter for nonlinear estimation[C]//Proceedings of the 46th IEEE Conference on Decision and Control.New Orleans:IEEE,2007:4293-4298.
    [10] 傅惠民,吴云章,娄泰山.欠观测条件下的增量Kalman滤波方法[J].机械强度,2012,34(1):43-47. FU Huimin,WU Yunzhang,LOU Taishan.Incremental Kalman filter method under poor observation condition[J]. Journal of Mechanical Strength,2012,34(1):43-47.(in Chinese)
    [11] 傅惠民,娄泰山,吴云章.欠观测条件下的扩展增量Kalman滤波方法[J].航空动力学报,2012,27(4):777-781. FU Huimin,LOU Taishan,WU Yunzhang.Extended incremental Kalman filter method under poor observation condition[J].Journal of Aerospace Power,2012,27(4):777-781.(in Chinese)
    [12] 傅惠民,娄泰山,吴云章.无迹增量滤波方法[J].航空动力学报,2012,27(7):1625-1629. FU Huimin,LOU Taishan,WU Yunzhang.Unscented incremental filter method[J].Journal of Aerospace Power,2012,27(7):1625-1629.(in Chinese)
    [13] 傅惠民,吴云章,娄泰山.自适应增量Kalman滤波方法[J].航空动力学报, 2012,27(6):1225-1229. FU Huimin,WU Yunzhang,LOU Taishan.Adaptive incremental Kalman filter method[J].Journal of Aerospace Power,2012,27(6):1225-1229.(in Chinese)
    [14] Julier S J. The scaled unscented transformation[C]//Proceedings of American Control Confernce.Jefferson City:IEEE,2002:4555-4559.
    [15] Julier S J,Uhlmann J K.Reduced sigma point filters for the propagation of means and covariances through nonlinear transformations[C]//Proceedings of the American Control Conference.Anchorage:IEEE,2002:887-892.
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出版历程
  • 收稿日期:  2012-02-29
  • 刊出日期:  2013-02-28

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