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基于自适应粒子滤波的涡扇发动机故障诊断

黄金泉 冯敏 鲁峰

黄金泉, 冯敏, 鲁峰. 基于自适应粒子滤波的涡扇发动机故障诊断[J]. 航空动力学报, 2014, (6): 1498-1504. doi: 10.13224/j.cnki.jasp.2014.06.033
引用本文: 黄金泉, 冯敏, 鲁峰. 基于自适应粒子滤波的涡扇发动机故障诊断[J]. 航空动力学报, 2014, (6): 1498-1504. doi: 10.13224/j.cnki.jasp.2014.06.033
HUANG Jin-quan, FENG Min, LU Feng. Turbo-fan engine fault diagnosis based on adaptive particle filtering[J]. Journal of Aerospace Power, 2014, (6): 1498-1504. doi: 10.13224/j.cnki.jasp.2014.06.033
Citation: HUANG Jin-quan, FENG Min, LU Feng. Turbo-fan engine fault diagnosis based on adaptive particle filtering[J]. Journal of Aerospace Power, 2014, (6): 1498-1504. doi: 10.13224/j.cnki.jasp.2014.06.033

基于自适应粒子滤波的涡扇发动机故障诊断

doi: 10.13224/j.cnki.jasp.2014.06.033
基金项目: 

国家自然科学基金(51276087);江苏省博后科学基金(201202063)

详细信息
    作者简介:

    黄金泉(1963- ),男,江苏泰兴人,教授,博士,主要从事航空发动机建模、控制及故障诊断研究.

  • 中图分类号: V233.7

Turbo-fan engine fault diagnosis based on adaptive particle filtering

  • 摘要: 针对涡扇发动机非线性、非高斯的特点,提出了一种自适应的粒子滤波算法用于涡扇发动机气路部件突变故障的诊断.为了减小算法的计算量并且保证滤波精度,分析了滤波精度和样本数目的关系,提出根据滤波过程中状态的方差自适应地调整粒子数,在保证一定的滤波精度下可以有效地减少滤波过程中使用的粒子数,提高了算法的实时性.同时,引入扩展卡尔曼滤波(EKF)用于更新粒子,产生重要概率密度函数,在一定程度上避免了粒子的退化.通过某型涡扇发动机的仿真分析表明:改进的算法相比标准粒子滤波算法用于涡扇发动机气路部件故障诊断时,参数估计的方均根误差减小了50%左右,且算法的计算量减小了30%.

     

  • [1] Link C.Recent advancements in aircraft engine health management (EHM) technologies and recommendations for the next step.ASME Paper GT2005-68625,2005.
    [2] 姜彩虹,孙志岩,王曦.航空发动机预测健康管理系统设计的关键技术[J].航空动力学报,2009,24(11):2589-2594. JIANG Caihong,SUN Zhiyan,WANG Xi.Critical technologies for aero-engine prognostics and health management systems development[J].Journal of Aerospace Power,2009,24(11):2589-2594.(in Chinese)
    [3] 黄伟斌,黄金泉.航空发动机故障诊断的机载自适应模型[J].航空动力学报,2008,23(3):580-584. HUANG Weibin,HUANG Jinquan.On board self-tuning model for aero-engine fault diagnostics[J].Journal of Aerospace Power,2008,23(3):580-584.(in Chinese)
    [4] Dorel D L.Interpretation of weight-least-squares gas path analysis results[J].Journal of Engineering Gas Turbines Power,2005,125(3):624-633.
    [5] Simon D L,Garg S.Optimal tuner selection for Kalman filter-based aircraft engine performance estimation.NASA/TM-2010-216076,2010.
    [6] 江传尚,樊丁,马冲.小波网络在某型航空发动机故障诊断中的应用[J].航空动力学报,2009,24(4):892-895. JIANG Chuanshang,FAN Ding,MA Chong.Application of the wavelet network in fault diagnosis for some kind of aero-engine[J].Journal of Aerospace Power,2009,24(4):892-895.(in Chinese)
    [7] 尉询楷,陆波,汪诚,等.支持向量机在航空发动机故障诊断中的应用[J].航空动力学报,2004,19(6):844-848. WEI Xunkai,LU Bo,WANG Cheng,et al.Application of support vector machines to aeroengine fault diagnosis[J].Journal of Aerospace Power,2004,19(6):844-848.(in Chinese)
    [8] 徐启华,师军.基于支持向量机的航空发动机故障诊断[J].航空动力学报,2005,20(2):298-302. XU Qihua,SHI Jun.Aero-engine fault diagnosis based on support vector machine[J].Journal of Aerospace Power,2005,20(2):298-302.(in Chinese)
    [9] Christophe B,Laurent T,Jean G.EKF and particle filter track to track fusion:a quantitative comparison from radar/lidar obstacle tracks.Philadelphia,PA:8th International Conference on Information Fusion (FUSION),2005.
    [10] Simon J,Jeffrey K U.Unscented filtering and nonlinear estimation[J].Proceedings of IEEE,2004,92(3):401-422.
    [11] 朱志宇.粒子滤波算法及其应用[M].北京:科学出版社,2010.
    [12] Gordon N J,Salmond D J,Smith A F M.Novel approach to nonlinear/non-Gaussian Bayesian state estimation[J].Proceedings of IEEE,1993,140(2):107-113.
    [13] LU Feng,HUANG Jinquan,LV Yiqiu.Gas path health monitoring for a turbofan engine based on nonlinear filtering approach[J].Energies,2013,6(1):492-513.
    [14] ZHANG Gongyuan,CHENG Yongmei,YANG Feng,et al.Design of an adaptive particle filter based on variance reduction technique[J].Acta Automatica Sinica,2010,36(7):1020-1024.
    [15] Jayesh H K,Petar M D.Gaussian particle filtering[J].IEEE Transactions on Signal Processing,2003,51(10):2592-2601.
    [16] Fox D.Adaptiving the sample size in particle filters through KLD-sample. Washington:University of Washington,2003.
    [17] 李文峰,王永生,杨纪明,等.航空发动机测试信号噪声分析[J].航空动力学报,2005,20(5):900-904. LI Wenfeng,WANG Yongsheng,YANG Jiming,et al.Noise characteristics analysis of aero-engine testing signals[J].Journal of Aerospace Power,2005 20(5):900-904.(in Chinese)
    [18] Borguet S,Leonard O.Comparison of adaptive filters for gas turbine performance monitoring[J]. Journal of Computational and Applied Mathematics,2010,234(7):2202-2212.
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出版历程
  • 收稿日期:  2013-04-11
  • 刊出日期:  2014-06-28

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