TY - GEN
T1 - A study of low-cost attitude and heading reference system under high magnetic interference
AU - Wu, Falin
AU - Fu, Yong
AU - Liang, Yuan
AU - Ji, Xinchun
N1 - Publisher Copyright:
© 2016 IEEE.
PY - 2016/5/26
Y1 - 2016/5/26
N2 - In an Attitude and Heading Reference System (AHRS), the heading estimation is generally achieved by measuring the Earth's magnetic field. However the Earth's magnetic field is easily distorted by magnetic interference from ferrous or magnetic objects. The traditional AHRS algorithm fuses the magnetic measurement into the estimation process of three attitude angles, acceleration and angular velocity with a Kalman filter. It may cause simultaneous misalignment of pitch, roll and yaw if the magnetic field is under high interference. In order to reduce the effect of the magnetic interference on orientation estimation, this paper proposed an adaptive Kalman filter algorithm, which alternates measurement equations in different magnetic conditions to achieve accurate and stable attitude and heading estimation. Quaternion is used to present the relation between body coordinate frame and navigation coordinate frame. To validate the algorithm, a prototype AHRS is designed. The experiments' results show that the prototype AHRS with the proposed algorithm could achieve both high accuracy and stability even under high magnetic interference.
AB - In an Attitude and Heading Reference System (AHRS), the heading estimation is generally achieved by measuring the Earth's magnetic field. However the Earth's magnetic field is easily distorted by magnetic interference from ferrous or magnetic objects. The traditional AHRS algorithm fuses the magnetic measurement into the estimation process of three attitude angles, acceleration and angular velocity with a Kalman filter. It may cause simultaneous misalignment of pitch, roll and yaw if the magnetic field is under high interference. In order to reduce the effect of the magnetic interference on orientation estimation, this paper proposed an adaptive Kalman filter algorithm, which alternates measurement equations in different magnetic conditions to achieve accurate and stable attitude and heading estimation. Quaternion is used to present the relation between body coordinate frame and navigation coordinate frame. To validate the algorithm, a prototype AHRS is designed. The experiments' results show that the prototype AHRS with the proposed algorithm could achieve both high accuracy and stability even under high magnetic interference.
KW - AHRS
KW - Kalman Filter
KW - Magnetic Interference
KW - Quaternion
UR - https://www.scopus.com/pages/publications/84978531220
U2 - 10.1109/PLANS.2016.7479788
DO - 10.1109/PLANS.2016.7479788
M3 - 会议稿件
AN - SCOPUS:84978531220
T3 - Proceedings of the IEEE/ION Position, Location and Navigation Symposium, PLANS 2016
SP - 916
EP - 923
BT - Proceedings of the IEEE/ION Position, Location and Navigation Symposium, PLANS 2016
PB - Institute of Electrical and Electronics Engineers Inc.
T2 - IEEE/ION Position, Location and Navigation Symposium, PLANS 2016
Y2 - 11 April 2016 through 14 April 2016
ER -