• DocumentCode
    3532716
  • Title

    Fault Prognosis Modeling of Aviation Electronic System Based on Kalman Filtering

  • Author

    Kong Qing-chun ; Xiao Ming-qing ; Zhao Xin

  • Author_Institution
    Eng. Sch., Air Force Eng. Univ., Xi´an
  • fYear
    2009
  • fDate
    28-29 April 2009
  • Firstpage
    1
  • Lastpage
    4
  • Abstract
    According to characteristics of fault in aviation electronic system, first of all, fault prognosis model based on Kalman filtering is established and analyzed in this paper, a certain method of to determine fault point critical status value is given, and then a project for fault prognosis is decided and fault prognosis algorithm is designed. And at last, historical data in system operation and test is fully utilized by fault prognosis model, and by so doing a theoretical foundation is provided for predicting fault and performance.
  • Keywords
    Kalman filters; avionics; built-in self test; Kalman filtering; aviation electronic system; condition-based maintenance; fault prognosis modeling; Aerospace electronics; Algorithm design and analysis; Control system synthesis; Design engineering; Fault detection; Filtering; Kalman filters; Maintenance; Modeling; System testing;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Testing and Diagnosis, 2009. ICTD 2009. IEEE Circuits and Systems International Conference on
  • Conference_Location
    Chengdu
  • Print_ISBN
    978-1-4244-2587-7
  • Type

    conf

  • DOI
    10.1109/CAS-ICTD.2009.4960822
  • Filename
    4960822