• DocumentCode
    3394759
  • Title

    Study on a method of rapid transfer alignment

  • Author

    Luan Hongzhong ; Mao Yuliang

  • Author_Institution
    Sch. of Autom., Beijing Inst. of Technol., Beijing, China
  • fYear
    2011
  • fDate
    19-22 Aug. 2011
  • Firstpage
    1423
  • Lastpage
    1426
  • Abstract
    For the rapidity and accuracy which airborne INS transfer alignment requires, the paper analyzed different transfer alignment matching method, chose velocity plus attitude matching method, deduced system error model and measurement equation in detail. Finally, the paper designed a new Kalman filter for simulation with a classic trajectory. Simulation shows that, the estimation of the misalignment angles can reach the accuracy requirement in a short time, the design of simulation is accurate, and the velocity plus attitude matching method is efficient.
  • Keywords
    Kalman filters; inertial navigation; measurement theory; Kalman filter; airborne INS transfer alignment; deduced system error model; measurement equation; misalignment angle estimation; rapid transfer alignment; transfer alignment matching method; velocity plus attitude matching method; Accuracy; Equations; Estimation; Kalman filters; Mathematical model; Navigation; Velocity measurement; Kalman filtering; matching method; transfer alignment;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Mechatronic Science, Electric Engineering and Computer (MEC), 2011 International Conference on
  • Conference_Location
    Jilin
  • Print_ISBN
    978-1-61284-719-1
  • Type

    conf

  • DOI
    10.1109/MEC.2011.6025738
  • Filename
    6025738