• DocumentCode
    1123502
  • Title

    Performance Evaluation of Suboptimal Filters

  • Author

    Asher, Robert B. ; Reeves, Richard M.

  • Author_Institution
    Frank J. Seiler Research Laboratory, US Air Force Academy, Colorado
  • Issue
    3
  • fYear
    1975
  • fDate
    5/1/1975 12:00:00 AM
  • Firstpage
    400
  • Lastpage
    405
  • Abstract
    The use of a Kalman filter in an applications problem requires a detailed model of both the system dynamics and the measurement dynamics. The model for many problems may be extremely large in dimensionality. However, in many instances one has a limited computer capability and, thus, must purposely introduce modeling errors into the filter in order to gain a computational advantage. However, as is well known, this may lead to the phenomenon of filter divergence. This paper considers the development of equations which allow one to evaluate a filter of reduced state. The equations are based upon using covariance analysis techniques in order to determine the true root-mean-square estimation error. These equations are computationally more advantageous than others appearing in the literature.
  • Keywords
    Aerodynamics; Aerospace electronics; Computer errors; Covariance matrix; Equations; Estimation error; Filters; Force measurement; Laboratories; State estimation;
  • fLanguage
    English
  • Journal_Title
    Aerospace and Electronic Systems, IEEE Transactions on
  • Publisher
    ieee
  • ISSN
    0018-9251
  • Type

    jour

  • DOI
    10.1109/TAES.1975.308092
  • Filename
    4101422