DocumentCode :
866379
Title :
Constrained filtering method for attitude determination using GPS and gyro
Author :
Chiang, Y.-T. ; Wang, L.S. ; Chang, F.R. ; Peng, H.M.
Author_Institution :
Dept. of Electr. Eng., Nat. Taiwan Univ., Taipei, Taiwan
Volume :
149
Issue :
5
fYear :
2002
fDate :
10/1/2002 12:00:00 AM
Firstpage :
258
Lastpage :
264
Abstract :
In attitude determination using the unit quaternion representation, the unit norm constraint results in singularity of the covariance matrix using classical filtering methods. To cope with this problem, a constrained filtering method is developed. In this method, the constraint equations and the state equations are treated as pseudo-measurement equations, so that they can be processed simultaneously with the real measurement equations. To illustrate the application of the proposed scheme, a scenario using GPS and gyro to perform attitude determination is considered. Software simulations show that the proposed scheme is sound, effective, and superior to existing methods.
Keywords :
Global Positioning System; attitude measurement; covariance matrices; digital simulation; filtering theory; gyroscopes; GPS; attitude determination; constrained filtering method; constraint equations; gyro; measurement equations; pseudo-measurement equations; singular covariance matrix; software simulations; state equations; unit norm constraint; unit quaternion representation;
fLanguage :
English
Journal_Title :
Radar, Sonar and Navigation, IEE Proceedings -
Publisher :
iet
ISSN :
1350-2395
Type :
jour
DOI :
10.1049/ip-rsn:20020531
Filename :
1047703
Link To Document :
بازگشت