• DocumentCode
    596640
  • Title

    Research of Fuzzy Inference based on Simplified UKF for large alignment errors in SINS alignment on a swaying base

  • Author

    Weiwei Yang ; Lingjuan Miao ; Ze Guo

  • Author_Institution
    Sch. of Autom., Beijing Inst. of Technol., Beijing, China
  • fYear
    2012
  • fDate
    18-20 Oct. 2012
  • Firstpage
    539
  • Lastpage
    544
  • Abstract
    In the condition of large alignment angles which brought about nonlinear problem in SINS, a precise SINS error model was established on the concept of Euler platform error angles. To reduce the computation of initial alignment in SINS, a Simplified UKF (SUKF) could be used since its state equation was nonlinear while the measurement equation was linear. A novel method combined Fuzzy Inference System (FIS) and system noise´s online estimation together on the basis of SUKF was proposed to adjust the system noise covariance, and online improve the performance of the SINS initial alignment. In the SINS alignment for large misalignment angles simulation conditions, the SUKF via FIS showed higher accuracy, better stability and also better real-time performance compared with conventional UKF.
  • Keywords
    Kalman filters; aerospace computing; digital simulation; fuzzy reasoning; inertial navigation; FIS; SINS alignment; SUKF; alignment errors; fuzzy inference system; large alignment angles; misalignment angles simulation conditions; nonlinear problem; precise SINS error model; simplified UKF; swaying base; Equations; Estimation; Kalman filters; Mathematical model; Noise; Silicon compounds;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Advanced Computational Intelligence (ICACI), 2012 IEEE Fifth International Conference on
  • Conference_Location
    Nanjing
  • Print_ISBN
    978-1-4673-1743-6
  • Type

    conf

  • DOI
    10.1109/ICACI.2012.6463222
  • Filename
    6463222