• DocumentCode
    2583648
  • Title

    A sliding window filter for real-time attitude independent TAM calibration

  • Author

    Grandvallet, B. ; Zemouche, A. ; Boutayeb, M. ; Changey, S.

  • Author_Institution
    Centre de Rech. en Autom. de Nancy, Univ. of Henri Poincare, Cosnes et Romain, France
  • fYear
    2010
  • fDate
    15-17 Dec. 2010
  • Firstpage
    467
  • Lastpage
    472
  • Abstract
    This paper deals with real time Three-Axis Magnetometers (TAM) calibration, applied to gun-launched spinning projectiles. The first part of this note present a new model used for real time estimation without any knowledge of the attitude of the projectile. Then the main contribution is a new simple and useful filter used for parameters estimation. The latter is formulated in the framework of a traditional Extended Kalman Filter (EKF), which include previous measurements in order to increase the performances and stability of the estimator. Finally numerical simulations support the contribution of the presented algorithm, and good performances are shown in a noisy context without requiring many more computation time than for the classical EKF.
  • Keywords
    Kalman filters; calibration; magnetometers; military equipment; nonlinear filters; numerical analysis; parameter estimation; projectiles; weapons; extended Kalman filter; gun-launched spinning projectiles; numerical simulation; parameters estimation; real time estimation; sliding window filter; three-axis magnetometer calibration; Calibration; Estimation; Noise; Noise measurement; Projectiles; Real time systems; Sensors;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Decision and Control (CDC), 2010 49th IEEE Conference on
  • Conference_Location
    Atlanta, GA
  • ISSN
    0743-1546
  • Print_ISBN
    978-1-4244-7745-6
  • Type

    conf

  • DOI
    10.1109/CDC.2010.5718124
  • Filename
    5718124