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基于自适应容积卡尔曼滤波方法的涡扇发动机气路部件故障诊断

胡宇 张世英 罗雷 朱杰堂 马鸿飞

胡宇, 张世英, 罗雷, 朱杰堂, 马鸿飞. 基于自适应容积卡尔曼滤波方法的涡扇发动机气路部件故障诊断[J]. 航空动力学报, 2016, 31(5): 1260-1267. doi: 10.13224/j.cnki.jasp.2016.05.030
引用本文: 胡宇, 张世英, 罗雷, 朱杰堂, 马鸿飞. 基于自适应容积卡尔曼滤波方法的涡扇发动机气路部件故障诊断[J]. 航空动力学报, 2016, 31(5): 1260-1267. doi: 10.13224/j.cnki.jasp.2016.05.030
HU Yu, ZHANG Shi-ying, LUO Lei, ZHU Jie-tang, MA Hong-fei. Turbofan engine gas path components fault diagnosis based on adaptive cubature Kalman filter[J]. Journal of Aerospace Power, 2016, 31(5): 1260-1267. doi: 10.13224/j.cnki.jasp.2016.05.030
Citation: HU Yu, ZHANG Shi-ying, LUO Lei, ZHU Jie-tang, MA Hong-fei. Turbofan engine gas path components fault diagnosis based on adaptive cubature Kalman filter[J]. Journal of Aerospace Power, 2016, 31(5): 1260-1267. doi: 10.13224/j.cnki.jasp.2016.05.030

基于自适应容积卡尔曼滤波方法的涡扇发动机气路部件故障诊断

doi: 10.13224/j.cnki.jasp.2016.05.030
详细信息
    作者简介:

    胡宇(1984-),男,湖南湘阴人,讲师,博士,研究领域为涡扇发动机建模与故障诊断.

  • 中图分类号: V233.7

Turbofan engine gas path components fault diagnosis based on adaptive cubature Kalman filter

  • 摘要: 针对涡扇发动机气路部件故障诊断中参数存在不同的噪声统计特性,提出了一种自适应平方根容积卡尔曼滤波(ASRCKF)器的自适应滤波方法.该方法直接利用基于3阶容积积分方法近似发动机的非线性统计特性,用于替代非线性无迹卡尔曼滤波方法的系统模型,避免了滤波过程参数选取的问题;采用移动窗口法对噪声协方差矩阵进行自适应估计,提高了算法对不同统计特性噪声的自适应能力和滤波精度.通过对发动机气路部件健康参数蜕化过程仿真结果表明:ASRCKF方法相比平方根容积卡尔曼滤波(SRCKF)方法,精度提高40%~50%,对不同噪声信号具有更好的适应能力.

     

  • [1] Rajamani R,Wang J,Jeong K Y.Conditioned based maintenance for aircraft engine[J].ASME Paper GT2004-54127,2004.
    [2] Naderi E,Meskin N,Khorasani K.Nonlinear fault diagnosis of jet engines by using a multiple model-based approach[J].Journal of Engineering for Gas Turbines and Power,2012,134(1):011602.1-011602.10.
    [3] Luppold R H,Roman J R,Gallops G W,et al.Estimating in flight engine performance variations using Kalman filter concepts[R].AIAA-89-2584,1989.
    [4] Kobayashi T.Application of a constant gain extended Kalman filter for in-flight estimation of aircraft engine performance parameters[R].NASA/TM 2005-213865,2005.
    [5] Kamboukos Ph,Mathioudakis K.Comparison of linear and nonlinear gas turbine performance diagnostics[J].Journal of Engineering for Gas Turbine and Power,2005,127(1):49-56.
    [6] 张鹏,黄金泉.航空发动机气路故障诊断的平方根UKF方法研究[J].航空动力学报,2008,23(1):169-173. ZHANG Peng,HUANG Jinquan.SRUKF research on aeroengines for gas path component fault diagnostics[J].Journal of Aerospace Power,2008,23(1):169-173.(in Chinese)
    [7] Simon D.A comparison of filtering approaches for aircraft engine health estimation[J].Aerospace Science and Technology,2008,12(4):276-284.
    [8] 何志昆,刘光斌,赵曦晶,等.基于GPR模型的自适应平方根容积卡尔曼滤波算法[J].航空学报,2013,34(9):2202-2211. HE Zhikun,LIU Guangbin,ZHAO Xijing,et al.Adaptive square-root cubature Kalman filer algrorithm based on Gaussian process regression models[J].Acta Aeronautica et Astronautica Sinica,2013,34(9):2202-2211.(in Chinese)
    [9] 赵琳,王小旭,李亮,等.非线性系统滤波理论[M].北京:国防工业出版社,2012.
    [10] Arasaratnam I,Haykin S.Cubature Kalman filters[J]. IEEE Trans.on Automatic Control,2009,54(6):1254-1269.
    [11] Arasaratnam I,Haykin S,Hurd T R.Cubture Kalman filtering for continuous-discrete systems:theory and simulations[J].IEEE Trans.on Signal Processing,2010,58(10):4977-4993.
    [12] 胡宇,张世英,杨月诚,等.基于超球体平方根无迹Kalman滤波算法的涡扇发动机气路部件故障诊断[J].航空动力学报,2014,29(3):689-695. HU Yu,ZHANG Shiying,YANG Yuecheng,et al.Fault diagnosis of gas path components of turbofan engine based on sepherical square root unscented Kalman filter algorithm[J].Journal of Aerospace Power,2014,29(3):689-695.(in Chinese)
    [13] 魏喜庆,宋申民.基于改进容积卡尔曼滤波的奇异避免姿态估计[J].航空学报,2013,34(3):610-619. WEI Xiqing,SONG Shenmin.Improved cubature Kalman filter based attitude estimation avoiding singularity[J].Acta Aeronautica et Astronautica Sinica,2013,34(3):610-619.(in Chinese)
    [14] 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)
    [15] 刘小勇,樊思齐.自适应卡尔曼滤波在航空发动机参数估计中的应用[J].航空动力学报,1995,10(3):304-306. LIU Xiaoyong,FAN Siqi.Application of Kalman filtering for an aeroengine parameter estimation[J].Journal of Aerospace Power,1995,10(3):304-306.(in Chinese)
    [16] 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,2014,29(6):1498-1504. HUANG Jinquan,FENG Min,LU Feng.Turbofan engine fault diagnosis based on adaptive particle filtering[J].Journal of Aerospace Power,2014,29(6):1498-1504.(in Chinese)
    [17] LU Feng,HUANG Jinquan,LÜ Yiqiu.Gas path health monitoring for a turbofan engine based on a nonlinear filtering approach[J].Energies,2013,6(1):492-513.
    [18] Borguet S,Léonard O.A generalized likelihood ratio test for adaptive gas turbine performance monitoring[J].Journal of Engineering for Gas Turbines and Power,2009,131(1):1-8.
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出版历程
  • 收稿日期:  2014-08-21
  • 刊出日期:  2016-05-28

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