• DocumentCode
    3428037
  • Title

    Health diagnosis for aircraft based on the ARMA model

  • Author

    Jianguo, Cui ; Zhang Jie ; Liqiu, Liu ; Yun, Zhao ; Keli, Zhang ; Zhou Guoqiang

  • Author_Institution
    Sch. of Autom., Shenyang Aerosp. Univ., Shenyang, China
  • fYear
    2010
  • fDate
    22-24 Oct. 2010
  • Firstpage
    277
  • Lastpage
    280
  • Abstract
    According to the AE (Acoustic Emission, AE) signal that caused by the aircraft structural crack, this paper proposed a health diagnosis approach based on ARMA model and SVM (Support Vector Machine, SVM). Firstly, this method apperceives the healthy information of a real aircraft stabilizer with real time by using AE detecting system. And then, deal with the information collected. Secondly, built an ARMA model and extracting parameter of ARMA model to set up characteristic vector. Finally, design and apply SVM monitor to diagnose the aircraft structure healthy state. Experiments show that the monitor has good performance to recognize and diagnose the fatigue crack of aircraft stabilizer, this approach is proposed to be effective. And it presents a new kind of approach to monitor the health state of aircraft structure and can also be used in other complex system structure health monitoring.
  • Keywords
    aircraft maintenance; autoregressive moving average processes; condition monitoring; fatigue cracks; mechanical engineering computing; structural acoustics; structural engineering; support vector machines; AE detecting system; ARMA model; SVM; acoustic emission signal; aircraft structural crack; fatigue crack; health diagnosis; structural health monitoring; support vector machine; Acoustic emission; Aerospace electronics; Aircraft; Atmospheric modeling; Biological system modeling; NASA; ARMA model; Aircraft; SVM; health diagnosis;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Intelligent Computing and Integrated Systems (ICISS), 2010 International Conference on
  • Conference_Location
    Guilin
  • Print_ISBN
    978-1-4244-6834-8
  • Type

    conf

  • DOI
    10.1109/ICISS.2010.5657166
  • Filename
    5657166