• Title of article

    Inner Attitude Integration Algorithm Based on Fault Detection for Strapdown Inertial Attitude and Heading Reference System

  • Author/Authors

    Jianye، نويسنده , , Liu and Yanhua، نويسنده , , Zhu and Jizhou، نويسنده , , Lai and Yongjun، نويسنده , , Yu، نويسنده ,

  • Issue Information
    روزنامه با شماره پیاپی سال 2010
  • Pages
    7
  • From page
    68
  • To page
    74
  • Abstract
    This article proposes a new inner attitude integration algorithm to improve attitude accuracy of the strapdown inertial attitude and heading reference system(SIAHRS), which, by means of a Kalman filter, integrates the calculated attitude from the accelerometers in inertial measuring unit(IMU), called damping attitudes, with those from the conventional IMU. As vehicleʹs acceleration could produce damping attitude errors, the horizontal outputs from accelerometers are firstly used to judge the vehicleʹs motion so as to determine whether the damping attitudes could be reasonably applied. This article also analyzes the limitation of this approach. Furthermore, it suggests a residual chi-square test to judge the validity of damping attitude measurement in real time, and accordingly puts forward proper information fusion strategy. Finally, the effectiveness of the proposed algorithm is proved through the experiments on a real system in dynamic and static states.
  • Keywords
    Kalman filter , residual chi-square test , Navigation , strapdown inertial attitude and heading reference system , inner attitude integration algorithm , Internal damping
  • Journal title
    Chinese Journal of Aeronautics
  • Serial Year
    2010
  • Journal title
    Chinese Journal of Aeronautics
  • Record number

    2264877