• DocumentCode
    174783
  • Title

    A least squares approach to size effect in inertial navigation

  • Author

    Eilon, S.

  • Author_Institution
    TAMAM Div., Israel Aerosp. Ind. Ltd., Yehud, Israel
  • fYear
    2014
  • fDate
    5-8 May 2014
  • Firstpage
    721
  • Lastpage
    732
  • Abstract
    This paper deals with the size effect problem in high-end Inertial Navigation Systems (INS). A focus is given to velocity errors in the geographical frame, which endure even after dynamic angular conditions are terminated. A least squares (LS) approach is taken to derive an algorithm for size effect compensation. The suggested algorithm implementation is based on low computation rate and does not involve highsampled increments. A performance analysis of the algorithm is presented, both in simulation and in real-life systems´ tests.
  • Keywords
    inertial navigation; least squares approximations; INS; LS approach; dynamic angular conditions; geographical frame; high-end inertial navigation systems; least squares approach; low computation rate; performance analysis; real-life system tests; size effect compensation; velocity errors; Acceleration; Accelerometers; Algorithm design and analysis; Navigation; Rotation measurement; Sensitivity; Vectors; High-end Inertial Naviagation Systems; Least Squares; Size Effect;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Position, Location and Navigation Symposium - PLANS 2014, 2014 IEEE/ION
  • Conference_Location
    Monterey, CA
  • Print_ISBN
    978-1-4799-3319-8
  • Type

    conf

  • DOI
    10.1109/PLANS.2014.6851438
  • Filename
    6851438