DocumentCode
2552204
Title
An attitude tracking method considering acceleration compensation and based on UKF
Author
Zou, Wei ; Du, Qingxiu ; Yuan, Kui ; Li, Jianfeng
Author_Institution
Inst. of Autom., Chinese Acad. of Sci., Beijing, China
fYear
2011
fDate
21-25 June 2011
Firstpage
52
Lastpage
57
Abstract
In this paper, an attitude tracking method considering acceleration compensation and based on UKF is proposed for measurement units integrating gyroscopes, accelerometers and magnetic sensors. Main characteristics of this method include: 1) the translational acceleration vector is combined with the quaternion describing attitude and the aggregate error vector of gyroscopes to constitute the system state vector; 2) acceleration vector measured by the accelerometers is regarded as combination of the gravity and the translational acceleration of the unit, then according to its amplitude and its normalized directional vector, the system state model and measurement model are established; 3) UKF is applied to implement filtering and tracking for the sake of nonlinearity of the system model. Comparing to the traditional Kalman filter, our method not only can achieve more accurate tracking results, but has stronger robustness to the unit´s motion mode, which broadens its application field to some extent.
Keywords
Kalman filters; attitude control; compensation; gyroscopes; nonlinear control systems; UKF; acceleration compensation; attitude tracking method; gyroscope aggregate error vector; measurement units; quaternion describing attitude; system model nonlinearity; system state vector; translational acceleration vector; Acceleration; Estimation; Gyroscopes; Kalman filters; Measurement units; Noise; Quaternions; UKF; acceleration compensation; attitude tracking; measurement unit; quaternion;
fLanguage
English
Publisher
ieee
Conference_Titel
Intelligent Control and Automation (WCICA), 2011 9th World Congress on
Conference_Location
Taipei
Print_ISBN
978-1-61284-698-9
Type
conf
DOI
10.1109/WCICA.2011.5970600
Filename
5970600
Link To Document