• DocumentCode
    761121
  • Title

    Direct Kalman filtering approach for GPS/INS integration

  • Author

    Qi, Honghui ; Moore, John B.

  • Volume
    38
  • Issue
    2
  • fYear
    2002
  • fDate
    4/1/2002 12:00:00 AM
  • Firstpage
    687
  • Lastpage
    693
  • Abstract
    We present a novel Kalman filtering approach for GPS/INS integration. In the approach, GPS and INS nonlinearities are preprocessed prior to a Kalman filter. The GPS preprocessed data are taken as measurement input, while the INS preprocessed data are taken as additional information for the state prediction of the Kalman filter. The advantage of this approach, over the well-studied (extended) Kalman filtering approaches is that a simple and linear Kalman filter can be implemented to achieve significant computation saving with very competitive performance figures
  • Keywords
    Global Positioning System; Kalman filters; aircraft navigation; inertial navigation; sensor fusion; GPS/INS integration; computation saving; data fusion; dead reckoning; direct Kalman filtering approach; inertial measurement unit; linear stochastic model; nonlinearities; receiver clock error; state prediction; strapdown navigator; transition matrix; Acceleration; Aircraft navigation; Data preprocessing; Earth; Filtering; Global Positioning System; Kalman filters; Measurement units; Nonlinear equations; Radio navigation;
  • fLanguage
    English
  • Journal_Title
    Aerospace and Electronic Systems, IEEE Transactions on
  • Publisher
    ieee
  • ISSN
    0018-9251
  • Type

    jour

  • DOI
    10.1109/TAES.2002.1008998
  • Filename
    1008998