• DocumentCode
    2553918
  • Title

    Application of two methods for alignment of FOG INS

  • Author

    Wang, Jinxi ; Lu, Wen ; Li, Lanfei

  • Author_Institution
    Dept. of Radiol., Taishan Med. Coll., Tai´´an, China
  • fYear
    2010
  • fDate
    16-18 April 2010
  • Firstpage
    581
  • Lastpage
    584
  • Abstract
    Initial alignment is of vital importance to inertial navigation systems (INS). There are mailnly two popular methods in self-alignment, which are traditional gyrocompassing alignment algorithm and kalman filter algorithm. After giving the basic principle of the two, we do some simulation and test in use of INS based fiber opitic gyroscope (FOG). The simulation and real experiment show that kalman filter is better than gyrocompassing in level alignment, however, the accuracy of azimuth misalignment angle estimation is lower. The real data test result is as similar as simulation. This provides a useful reference for design alignment algorithm for FOG INS.
  • Keywords
    Kalman filters; fibre optic gyroscopes; inertial navigation; FOG INS; Kalman filter algorithm; fiber optic gyroscope; gyrocompassing alignment algorithm; inertial navigation systems; initial alignment; Accelerometers; Azimuth; Earth; Field programmable gate arrays; Filters; Gyroscopes; Navigation; Silicon compounds; Space technology; Testing; FOG INS; gyrocompassing; initial alignment; kalman filter;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Information Management and Engineering (ICIME), 2010 The 2nd IEEE International Conference on
  • Conference_Location
    Chengdu
  • Print_ISBN
    978-1-4244-5263-7
  • Electronic_ISBN
    978-1-4244-5265-1
  • Type

    conf

  • DOI
    10.1109/ICIME.2010.5478076
  • Filename
    5478076