• DocumentCode
    1881691
  • Title

    Robust nonlinear filtering applied to integrated navigation system INS/GNSS under non Gaussian measurement noise effect

  • Author

    Benzerrouk, Hamza ; Nebylov, Alexander

  • Author_Institution
    Int. Inst. for Adv. Aerosp. Technol., St.-Petersburg State Univ. of Aerosp. Instrum., St. Petersburg, Russia
  • fYear
    2012
  • fDate
    3-10 March 2012
  • Firstpage
    1
  • Lastpage
    8
  • Abstract
    In this paper, robust design of INS/GNSS navigation system is proposed for solving problem of state space models with non Gaussian measurement noise based on parallel non linear filtering. GNSS in this paper is assumed a combination of GPS and GLONASS signals in order to improve and increase accuracy of satellite positioning. Non linear approximation techniques such as Extended Kalman Filter (EKF), Sigma Point Kalman Filter (SPKF) are adapted. Robust navigation system is designed and efficiently estimates state vector of navigation. Three parallel algorithms are simulated and compared through RMSE criteria under several conditions.
  • Keywords
    Global Positioning System; Kalman filters; nonlinear filters; GLONASS signals; GPS signals; INS/GNSS; extended Kalman filter; integrated navigation system; nonGaussian measurement noise effect; nonlinear approximation techniques; parallel nonlinear filtering; robust nonlinear filtering; satellite positioning; sigma point Kalman filter; state space models; Estimation; Global Navigation Satellite Systems; Kalman filters; Mathematical model; Maximum likelihood detection; Nonlinear filters; Robustness;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Aerospace Conference, 2012 IEEE
  • Conference_Location
    Big Sky, MT
  • ISSN
    1095-323X
  • Print_ISBN
    978-1-4577-0556-4
  • Type

    conf

  • DOI
    10.1109/AERO.2012.6187141
  • Filename
    6187141