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机动目标状态估计的最小均方误差界 被引量:2

Minimum mean square error bound for state estimation of maneuvering targets
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摘要 基于多项式模型的各种自适应滤波算法被广泛应用于机动目标跟踪领域,但尚没有统一的评估标准来衡量这些跟踪算法的优劣。由于存在确定的时变未知输入,机动目标的状态估计实际为有偏估计。基于状态估计均方误差最小的准则,推导了多项式模型滤波的最小均方误差界计算方法,获得了使状态估计均方误差最小的过程噪声方差变化规律。该方法给出了各种基于多项式模型的机动目标跟踪算法的估计均方误差下限,也为机动目标跟踪中最优过程噪声方差的设定提供了依据。仿真结果验证了算法的有效性。 The adaptive filtering algorithms based on the polynomial model are widely used in the field of maneuvering target tracking, but there is no uniform evaluation criterion to measure the quality of these tracking algorithms. Due to the existence of time-varying unknown inputs, the maneuvering target state estimation is actually biased. To solve this problem, the minimum mean square error bound calculation method for polynomial model Kalman filters was derived based on the minimum mean square error criterion, and the process noise variance law minimizing the state estimation mean square error was obtained. The proposed algorithm provides a unified evaluation standard for maneuvering target tracking algorithms based on the polynomial model, and also provides the basis for the setting of the actual process noise variance in maneuvering target tracking. The effectiveness of the proposed algorithm is demonstrated by the simulation results.
出处 《国防科技大学学报》 EI CAS CSCD 北大核心 2013年第6期1-8,共8页 Journal of National University of Defense Technology
基金 国家自然科学基金资助项目(41240031)
关键词 机动目标跟踪 最小均方误差界 自适应卡尔曼滤波 有偏估计 多项式模型 maneuvering target tracking minimum mean square error bound adaptive kalman filtering biased estimation polynomial model
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参考文献17

  • 1Singer R A. Estimating optimal tracking filter performance for manned maneuvering targets[J].{H}IEEE Transactions on Aerospace and Electronic Systems,1970,(4):473-483.
  • 2Li X R,Jilkov V P. A survey of maneuvering target tracking:dynamic models[A].Orlando,Florida,USA,2000.212-235.
  • 3Mehrotra K,Mahapatra P R. A jerk model to tracking highly maneuvering targets[J].{H}IEEE Transactions on Aerospace and Electronic Systems,1997,(4):1094-1105.
  • 4Zhou H R,Kumar K S P. A current statistical model and adaptive algorithm for estimating maneuvering targets[J].AIAA Journal Guidance Control and Dynamics,1984,(5):596-602.
  • 5钱华明,陈亮,杨峻巍.基于AR模型的非线性目标跟踪自适应算法[J].华中科技大学学报(自然科学版),2012,40(9):52-56. 被引量:2
  • 6Sage A P,Husa G W. Adaptive filtering with unknown prior statistics[A].Boulder Colorado,USA,1969.760-769.
  • 7Kirlin R L,Moghaddamjoo A. Arobust running window detector and estimator for step signals in contaminated Gaussian noise[J].{H}IEEE Transactions on Acoustics Speech and Signal Processing,.
  • 8Sinha A,Kirubarajan T,Bar-Shalom Y. Application of the kalman-levy filter for tracking maneuvering targets[J].{H}IEEE Transactions on Aerospace and Electronic Systems,2007,(3):1099-1107.
  • 9Chan Y T,Hu A G,Plant J B. A kalman filter based tracking scheme with input estimation[J].{H}IEEE Transactions on Aerospace and Electronic Systems,1989,(2):237-244.
  • 10Li X R,Jilkov V P,Ru J F. Multiple-model estimation with variable structure-part VI:expected-mode augmentation[J].{H}IEEE Transactions on Aerospace and Electronic Systems,2005,(3):853-867.

二级参考文献34

  • 1宋强,何友,杨俭.基于强跟踪滤波器的Jerk模型目标跟踪算法[J].海军航空工程学院学报,2007,22(3):329-332. 被引量:5
  • 2雷明,韩崇昭.多级修正的高机动Jerk模型研究[J].西安交通大学学报,2006,40(2):138-141. 被引量:11
  • 3[1]Chen Y T,Hu A G C,Plant J B.A Kalman Filter Based Tracking Scheme with Input Estimation[J].IEEE Trans.Aerosp.Electron.Syst.,1979,15 (3):237-244.
  • 4[2]Bar-Shalom Y,Birmiwal K.Variable Dimension Filter for Maneuvering Target Tracking[J].IEEE Trans.Aerosp.Electron.Syst.,1982,18(5):621-629.
  • 5[4]Mazor E,Averbuch A Y,Bar-Shalom Y,et al.Interacting Multiple Model Methods in Target Tracking:A Survey[J].IEEE Trans.Aerosp.Electron.Syst.,1998,34 (1):103-123.
  • 6[5]Ristic B,Arulampalam S.Tracking a Manoeuvring Target Using Angle-only Measurements:Algorithms and Performance[J].Signal Processing,2003,83(6):1223-1238.
  • 7[6]Duh F B,Lin C T.Tracking a Maneuvering Target Using Neural Fuzzy Network[J].IEEE Trans.Syst.,Man,Cybem.B,2004,34 (1):16 -33.
  • 8[7]Li X R,Jilkon V P.Survey of Maneuvering Target Tracking-Part Ⅰ:Dynamic Models[J].IEEE Trans.Aerosp.Electron.Syst.,2003,39(4):1333-1364.
  • 9[8]Bkcker.A General Approach to TMA Observability from Angle and Frequency Measurements[J].IEEE Trans.Aerosp.Electron.Syst.,1996,32(1):487-494.
  • 10[9]Key S M.统计信号处理基础[M].罗鹏飞,译.北京:电子工业出版社,2003.

共引文献11

同被引文献13

  • 1袁俊.导弹防御系统的弹道导弹突防[J].上海航天,2005,22(1):48-51. 被引量:9
  • 2Legowik, Diana M. Case study on a systems: The ballistic missile defence system (BMDS) [C]//29th Annual National Conference of the American Society for Engineering Manage- ment. West Point, NY, 2008: 727-728.
  • 3USA Department of Defence. Ballistic missile defense review report, ADA514210[R]. USA Department of Defense, 2010.
  • 4Walker S H, Rodgers F. Falcon hypersonic technology over- view [C]//13th AIAA International Space Planes and Hyper- sonic Systems and Technologies Conference. Capua, Italy, 2005 : AIAA-2005-3253.
  • 5Walker S H, Jeffrey L, Shell D. The DARPA/AF falcon program= The hypersonic technology vehicle-2 (HTV-2) flight demonstration phase [C]~//15th AIAA International Space Planes and Hypersonic Systems and Technologies Con- ference. Dayton, Ohio, 2008: AIAA 2008-2539.
  • 6Farina A, Ristic B, Benvenuti D. Tracking a ballistic target comparison of several nonlinear filters [J]. IEEE Transac tions on Aerospace and Electronic Systems, 2002, 38 (3) 855-867.
  • 7Li Pengcheng, Yang Suochang, Feng Delong. Research on the improved proportional navigation guidance law using CA- DET [J]. Applied Mechanics and Materials, 2014, 488: 1061-1063.
  • 8汤文辉,程周.弹道导弹的突防手段与突防策略研究[J].导弹与航天运载技术,2009(2):17-19. 被引量:11
  • 9陈小庆,侯中喜,刘建霞.高超声速滑翔飞行器弹道特性分析[J].导弹与航天运载技术,2011(2):5-9. 被引量:27
  • 10张昌芳,朱启超,匡兴华.美国弹道导弹防御C2BMC系统发展综述[J].装备学院学报,2012,23(3):60-63. 被引量:16

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