DocumentCode :
2061010
Title :
Efficient Extended Kalman Filtering for attitude estimation based on gyro and vector observations
Author :
Miao, Yuhong ; Zhou, Jianghua
Author_Institution :
Res. Inst. of Hi-Tech, Xi´´an, China
fYear :
2010
fDate :
6-13 March 2010
Firstpage :
1
Lastpage :
7
Abstract :
This paper presents an efficient Extended Kalman Filter (EKF) which can simultaneously process all the observation information. The EKF applies the Rodrigues parameters of attitude and gyro drift-rate bias vector as the state vector. A new third order measurement equation is used which contains all the observation information. By using this measurement equation, the computation of the gain matrix needs to take the inverse of a 3×3 matrix only once. The measurement sensitivity matrix is not singular if the number of observed vector is not 1. Simulation results show that the proposed EKF improved the computational efficiency without accuracy loss.
Keywords :
Kalman filters; attitude measurement; gyroscopes; Rodrigues parameters; attitude drift-rate bias vector; attitude estimation; extended Kalman filtering; gyro drift-rate bias vector; gyro observations; measurement sensitivity matrix; observation information; state vector; third order measurement equation; vector observations; Automation; Biomedical optical imaging; Equations; Filtering; Gain measurement; Kalman filters; Matrix decomposition; Optical filters; Optical sensors; Space vehicles;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Aerospace Conference, 2010 IEEE
Conference_Location :
Big Sky, MT
ISSN :
1095-323X
Print_ISBN :
978-1-4244-3887-7
Electronic_ISBN :
1095-323X
Type :
conf
DOI :
10.1109/AERO.2010.5446734
Filename :
5446734
Link To Document :
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