留言板

尊敬的读者、作者、审稿人, 关于本刊的投稿、审稿、编辑和出版的任何问题, 您可以本页添加留言。我们将尽快给您答复。谢谢您的支持!

姓名
邮箱
手机号码
标题
留言内容
验证码

基于自适应UKF的敏感器故障诊断算法

胡迪 董云峰

胡迪, 董云峰. 基于自适应UKF的敏感器故障诊断算法[J]. 北京航空航天大学学报, 2011, 37(6): 639-643.
引用本文: 胡迪, 董云峰. 基于自适应UKF的敏感器故障诊断算法[J]. 北京航空航天大学学报, 2011, 37(6): 639-643.
Hu Di, Dong Yunfeng. Sensor fault diagnosis algorithm based on adaptive UKF[J]. Journal of Beijing University of Aeronautics and Astronautics, 2011, 37(6): 639-643. (in Chinese)
Citation: Hu Di, Dong Yunfeng. Sensor fault diagnosis algorithm based on adaptive UKF[J]. Journal of Beijing University of Aeronautics and Astronautics, 2011, 37(6): 639-643. (in Chinese)

基于自适应UKF的敏感器故障诊断算法

详细信息
  • 中图分类号: V 448.21

Sensor fault diagnosis algorithm based on adaptive UKF

  • 摘要: 针对非线性系统中敏感器测量过程存在异常干扰和出现仪器故障问题,提出一种基于自适应UKF(Unscented Kalman Filtering)的鲁棒故障诊断算法.算法通过新息特性分析引入自适应矩阵对异常干扰和仪器故障建立系统级抑制和部件级诊断.系统级检测将UKF的新息特性通过自适应函数引入状态预测,修正异常值对状态预测值的影响,达到对异常干扰的鲁棒性.部件级检测将新息特性分解成各部件参数的新息特性,建立各自敏感器的自适应矩阵,通过对自适应矩阵的迹进行判断,检测是否发生故障并隔离故障.仿真结果表明,算法对异常值具有较强的鲁棒性,对测量仪器失效造成的故障能够准确地检测并给出故障大小.算法结构简单,计算量小,对工程应用具有较好的参考价值.

     

  • [1] 金磊,徐世杰.基于扩张状态观测器的飞轮故障检测与恢复[J].北京航空航天大学学报,2008,34(11):1272-1275 Jin Lei,Xu Shijie.Extended sate observer-based fault detection and recovery for flywheels [J].Journal of Beijing University of Aeronautics and Astronautics,2008,34(11):1272-1275(in Chinese) [2] Mehra R,Seereeram S,Bayard D,et al.Adaptive Kalman filtering failure detection and identification for spacecraft attitude estimation //Proceedings of the 4th IEEE Conference on Control Applications.Albany:IEEE,1995:176-181 [3] Wang Xudong,Syrmos V L,Fault detection,identification and estimation in the electro-hydraulic actuator system using EKF-based multiple-model estimation //16th Mediterranean Conference on Control and Automation.Ajaccio:IEEE,2008:1693-1698 [4] Li Linglai,Zhou Donghua,Wang Youaing, et al.Unknown input extended Kalman filter and applications in nonlinear fault diagnosis [J].Chinese Journal of Chemical Engineering,2005,13(6):783-790 [5] Julier S J,Uhlmann J K,Durrant-Whyten H F.A new approach for filtering nonlinear system //Pro of the American Control Conference.Seattle:IEEE,1995:1628-1632 [6] 张磊,李行善,于劲松,等.一种基于二元估计与粒子滤波的故障预测算法[J].北京航空航天大学学报,2008,34(7):798-802 Zhang Lei,Li Xingshan,Yu Jinsong,et al.Fault prognostic algorithm based on dual estimation and particle filter [J].Journal of Beijing University of Aeronautics and Astronautics,2008,34(7):798-802(in Chinese) [7] Cao Yuping,Tian Xuemin.An adaptive UKF algorithm for process fault prognostics //2009 Second International Conference on Intelligent Computation Technology and Automation.Changsha:IEEE,2009:487-490 [8] Soken H E,Hajiye C.Adaptive unscented kalman filter with multiple fading factors for pico satellite attitude estimation //RAST-09.4th International Conference on Recent Advances In Space Technologies.Istanbul:IEEE,2009:541-546 [9] Crassidis J L,Markley F L.Unscented filtering for spacecraft attitude Estimation //AIAA Guidance,Navigation,and Control Conference and Exhibit.Texas:AIAA,2003:11-14 [10] 章仁为.卫星轨道姿态动力学与控制[M].北京:北京航空航天大学出版社,1998:148,172 Zhang Renwei.Satellite orbit & attitude dynamics and control [M].Beijing:Beihang University Press,1998:148,172 (in Chinese)
  • 加载中
计量
  • 文章访问数:  6368
  • HTML全文浏览量:  69
  • PDF下载量:  1095
  • 被引次数: 0
出版历程
  • 收稿日期:  2010-03-12
  • 网络出版日期:  2011-06-30

目录

    /

    返回文章
    返回
    常见问答