• DocumentCode
    1733489
  • Title

    A filtering method of gyroscope random drift for Miniature Unmanned Helicopter

  • Author

    Pan, Vue ; Song, Ping ; Li, KeJie ; Lin, Ran ; Huang, Wei

  • Author_Institution
    Sch. of Mechatronical Eng., Beijing Inst. of Technol., Beijing, China
  • Volume
    2
  • fYear
    2011
  • Firstpage
    730
  • Lastpage
    734
  • Abstract
    Low-cost MEMS gyroscopes used in the Miniature Unmanned Helicopter (MUH) have great random drift. In order to improve the performance of MEMS gyroscopes, a one-order AR model was established for the random drift. Then Sage-Husa adaptive Kalman filter was applied to process the random drift signal. Experiments were carried out to verify the validity of the method. Tests results demonstrate that the method based on AR model and Sage-Husa adaptive Kalman filter is convenient and effective and it significantly reduces random drift. Compared to conventional Kalman filter, Sage-Husa adaptive Kalman filter can estimate statistic characteristics of system noise and measurement noise and modify filter parameters on-time. It improves stability and adaptability and thus can give a more accurate filtering result.
  • Keywords
    Kalman filters; autonomous aerial vehicles; gyroscopes; micromechanical devices; Sage-Husa adaptive Kalman filter; filtering method; gyroscope random drift; low-cost MEMS gyroscopes; measurement noise; miniature unmanned helicopter; one-order AR model; random drift signal; system noise; Adaptation models; Equations; Gyroscopes; Kalman filters; Lead; Mathematical model; Size measurement; AR model; MUH; Sage-Husa adaptive Kalman filter; gyroscope random drift;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Computer Science and Network Technology (ICCSNT), 2011 International Conference on
  • Conference_Location
    Harbin
  • Print_ISBN
    978-1-4577-1586-0
  • Type

    conf

  • DOI
    10.1109/ICCSNT.2011.6182068
  • Filename
    6182068