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
Link To Document :
بازگشت