DocumentCode
183658
Title
SO(3)-constrained Kalman filtering with application to attitude estimation
Author
de Ruiter, Anton H. J.
Author_Institution
Dept. of Aerosp. Eng., Ryerson Univ., Toronto, ON, Canada
fYear
2014
fDate
4-6 June 2014
Firstpage
4937
Lastpage
4942
Abstract
This paper presents a new continuous-time Kalman-like filter directly on SO(3) for attitude estimation of a vehicle with vector and gyro measurements. The presented filter is inspired by a recently developed norm-constrained Kalman-like filter, which has successfully been applied to the attitude estimation problem when a quaternion parameterization is used. The filter is compared with a continuous-time multiplicative extended Kalman filter, which is also formulated directly on SO(3).
Keywords
Kalman filters; attitude measurement; nonlinear filters; SO(3)-constrained Kalman filtering; attitude estimation problem; continuous-time Kalman-like filter; gyro measurements; multiplicative extended Kalman filter; norm-constrained Kalman-like filter; quaternion parameterization; vector measurements; Covariance matrices; Equations; Estimation; Kalman filters; Kinematics; Vectors; Vehicles; Aerospace; Estimation; Kalman filtering;
fLanguage
English
Publisher
ieee
Conference_Titel
American Control Conference (ACC), 2014
Conference_Location
Portland, OR
ISSN
0743-1619
Print_ISBN
978-1-4799-3272-6
Type
conf
DOI
10.1109/ACC.2014.6858692
Filename
6858692
Link To Document