DocumentCode
552540
Title
SCKF for MAV attitude estimation
Author
Li, Chao ; Ge, Quan-bo
Author_Institution
Inst. of Inf. & Control, Hangzhou Dianzi Univ., Hangzhou, China
Volume
3
fYear
2011
fDate
10-13 July 2011
Firstpage
1313
Lastpage
1318
Abstract
In this paper, a novel quaternion-based attitude estimation algorithm with the square-root cubature Kalman filter (SCKF) is proposed to improve the attitude estimation performance for micro air vehicle (MAV). The SCKF is a kind of new effective method to solve nonlinear state estimation, it can directly deal with nonlinear systems, and the QR decomposition in SCKF avoids the square-root operation of the covariance matrix, which ensures the continuity of the filtering process. We use quaternion to represent the attitude, treat the strap down attitude as state update, and adopt the bi-vector method to update the measurement vector. Simulation example shows that the proposed algorithm can get better performance on the estimate accuracy and error robustness than that of extended Kalman filter (EKF) and unscented Kalman filter (UKF).
Keywords
Kalman filters; aircraft control; attitude control; covariance matrices; nonlinear systems; stability; state estimation; MAV attitude estimation; QR decomposition; bivector method; covariance matrix; error robustness; filtering process continuity; measurement vector; microair vehicle; nonlinear state estimation; nonlinear system; quaternion-based attitude estimation algorithm; square-root cubature Kalman filter; square-root operation; state update; strap down attitude; Accuracy; Covariance matrix; Equations; Estimation; Kalman filters; Mathematical model; Quaternions; Attitude estimation; MAV; Quaternion; SCKF;
fLanguage
English
Publisher
ieee
Conference_Titel
Machine Learning and Cybernetics (ICMLC), 2011 International Conference on
Conference_Location
Guilin
ISSN
2160-133X
Print_ISBN
978-1-4577-0305-8
Type
conf
DOI
10.1109/ICMLC.2011.6016854
Filename
6016854
Link To Document