• Title of article

    Quaternion-Based Kalman Filter for Micro-machined Strapdown Attitude Heading Reference System

  • Author/Authors

    GAO، نويسنده , , Zhongyu and Niu، نويسنده , , Xiao-ji and GUO، نويسنده , , Mei-feng، نويسنده ,

  • Issue Information
    روزنامه با شماره پیاپی سال 2002
  • Pages
    5
  • From page
    171
  • To page
    175
  • Abstract
    A Kalman filter used in strapdown AHRS (Attitude Heading Reference System) based on micro-machined inertial sensors is introduced. The composition and principle of the system are described. The attitude algorithm and error model of the system are derived based on the quaternion formulation. The real-time quaternion-based Kalman filter is designed. Simulation results show that accuracy of the system is better than 0.04 degree without disturbance of lateral acceleration and reduced to 0.44 degree with lateral acceleration of 0.1 g/1Hz. Primary tests show that the static accuracy of the system is + / − 0.2 degree for pitch and roll, and + / − 0.3 degree for azimuth.
  • Keywords
    Kalman filter , Quaternion algebra , micro-machined inertial sensors , strapdown AHRS
  • Journal title
    Chinese Journal of Aeronautics
  • Serial Year
    2002
  • Journal title
    Chinese Journal of Aeronautics
  • Record number

    2264400