• DocumentCode
    1149136
  • Title

    An Application of Kalman Filtering and Time Averaging to Inertial Guidance Evaluation

  • Author

    Rosenthal, P.L. ; Brownlow, J.D.

  • Author_Institution
    Lockheed-California Company P.O. Box 551 D/72-51, B/310, P/B-6 Burbank, CA 91520
  • Issue
    6
  • fYear
    1985
  • Firstpage
    821
  • Lastpage
    822
  • Abstract
    A method is developed for estimating circular error probable values and circular error probable rate values of an inertial navigation system using the concepts of Kalman filtering and time averaging.
  • Keywords
    Autocorrelation; Data analysis; Filtering; History; Inertial navigation; Kalman filters; Random variables; System performance; System testing; Target tracking;
  • fLanguage
    English
  • Journal_Title
    Aerospace and Electronic Systems, IEEE Transactions on
  • Publisher
    ieee
  • ISSN
    0018-9251
  • Type

    jour

  • DOI
    10.1109/TAES.1985.310669
  • Filename
    4104153
    • Link To Document
    https://search.isc.ac/dl/search/defaultta.aspx?DTC=49&DC=1149136