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 :
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