LUO Xing-yu, ZHANG Qi, CHANG Qinget al. Control Strategy and Implementation for Acquiring C/A Code of High Dynamic GPS Signals[J]. Journal of Beijing University of Aeronautics and Astronautics, 2002, 28(3): 358-361. (in Chinese)
Citation: FU Jinbin, SUN Jinping, LU Songtao, et al. Maneuvering target tracking with modified unbiased FIR filter[J]. Journal of Beijing University of Aeronautics and Astronautics, 2015, 41(1): 77-82. doi: 10.13700/j.bh.1001-5965.2014.0068(in Chinese)

Maneuvering target tracking with modified unbiased FIR filter

doi: 10.13700/j.bh.1001-5965.2014.0068
  • Received Date: 24 Feb 2014
  • Publish Date: 20 Jan 2015
  • In the field of maneuvering target tracking, the performance of Kalman filter(KF)and its variants is dependeds on the accuracy of the assumed process noise statistics. If the assumed process noise is not accurate, the performance of the KF and its improved algorithms will be degraded significantly. In some cases, the filters might even cannot be converged. Unbiased finite impulse response (UFIR) filter does not need the prior knowledge of the process noise statistics during filtering. Hence, it can be utilized to overcome the problem of the inaccurate assumed process noise statistics to realize the maneuvering target tracking. Since the generalized noise power gain (GNPG) of the existing UFIR filter cannot be adapted to the measurements innovation, an improved UFIR filter was proposed. The proposed UFIR dynamically adjusts GNPG according to the ratio of measurements innovations between the adjacent time such that it can improve the detecting ability of the UFIR filter for target maneuver. The simulation results illustrate that if assumed process noise is accurate, the performance of the existing UFIR filter and the proposed FIR filter is similar to KF; but if assumed process noise is not accurate, the performance of the proposed UFIR shows better than the other ones.

     

  • [1]
    Houles A,Bar-Shalom Y.Multisensor tracking of a maneuvering target in clutter[J].IEEE Transactions on Aerospace and Electronic Systems,1989,25(2):176-188.
    [2]
    Bar-Shalom Y,Birmiwal K.Variable dimension filter for maneuvering target tracking[J].IEEE Transactions on Aerospace and Electronic Systems,1982,18(5):621-629.
    [3]
    Magrill D T.Optimal adaptive estimation of sampled stochastic processes[J].IEEE Transactions on Automatic Control,1965,10(4):434-439.
    [4]
    Nadarajah N,Tharmarasa R,McDonald M,et al.IMM forward filtering and backward smoothing for maneuvering target tracking[J].IEEE Transactions on Aerospace and Electronic Systems,2012,48(3):2673-2678.
    [5]
    Gibbs B.Advanced Kalman filtering,least-squares and modeling[M].New York:Wiley,2011.
    [6]
    Shmaliy Y S.An unbiased FIR filter for TIE model of a local clock in applications to GPS-based timekeeping[J].IEEE Transactions on Ultrasonics,Ferroelectrics,and Frequency Control,2006,53(5):862-869.
    [7]
    Kwon O K,Kwon W H,Lee K S.FIR filters and recursive forms for discrete-time state-space models[J].Automatica,1989,25(5):715-728.
    [8]
    Kwon W H,Kim P S,Han S H.A receding horizon unbiased FIR filter for discrete-time state space models[J].Automatica,2002,38(3):545-551.
    [9]
    Kwon W H,Kim P S,Park P.A receding horizon Kalman FIR filter for discrete time-invariant systems[J].IEEE Transactions on Automatic Control,1999,44(9):1787-1791.
    [10]
    Shmaliy Y S.An iterative Kalman-like algorithm ignoring noise and initial conditions[J].IEEE Transactions on Signal Processing,2011,59(6):2465-2473.
    [11]
    Ramirez-Echeverria F,Sarr A,Shmaliy Y S.Optimal memory for discrete-time FIR filters in state-space[J].IEEE Transactions on Signal Processing,2014,62(3):557-561.
    [12]
    Song T L,Speyer J L.A stochastic analysis of a modified gain extended Kalman filter with application to estimation with bearing only measurements[J].IEEE Transactions on Automatic Control,1985,AC-30(10):940-949.
    [13]
    Shmaliy Y S,Ibarra-Manzano O.Time-variant linear optimal finite impulse response estimator for discrete-time state-space models[J].International Journal of Adaptive Control and Signal Processing,2012,26(2):95-104.
    [14]
    Shmaliy Y S.Linear optimal FIR estimation of discrete time-invariant state-space models[J].IEEE Transactions on Signal Processing,2010,58(6):3086-3096.
    [15]
    Shmaliy Y S,Simon D.Iterative unbiased FIR state estimation: a review of algorithms[J].Eurasip Journal on Advances in Signal Processing,2013(1):1-16.
    [16]
    Simon D,Shmaliy Y S.Unified forms for Kalman and finite impulse response filtering and smoothing[J].Automatica,2013,49(6):1892-1899

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