DocumentCode
2183887
Title
Fuzzy Adaptive Unscented Kalman Filter for Ultra-Tight GPS/INS Integration
Author
Jwo, Dah-Jing ; Chung, Fong-Chi
Author_Institution
Dept. of Commun., Navig. & Control Eng., Nat. Taiwan Ocean Univ., Keelung, Taiwan
Volume
2
fYear
2010
fDate
29-31 Oct. 2010
Firstpage
229
Lastpage
235
Abstract
This paper presents a sensor fusion method based on the combination of adaptive unscented Kalman filter (UKF) and Fuzzy Logic Adaptive System (FLAS) for the ultra-tightly coupled GPS/INS integrated navigation. The UKF employs a set of sigma points by deterministic sampling, such that the linearization process is not necessary, and therefore the error caused by linearization as in the traditional extended Kalman filter (EKF) can be avoided. The adaptive algorithm has been one of the approaches to prevent divergence problem of the filter when precise knowledge on the system models are not available. Through the use of fuzzy logic, the FLAS has been incorporated into the AUKF as a mechanism for timely detecting the dynamical changes and implementing the on-line tuning of the factors in the weighted covariance matrices by monitoring the innovation information so as to maintain good estimation accuracy and tracking capability. The performance assessment for UKF and FUKF are carried out.
Keywords
Global Positioning System; adaptive Kalman filters; covariance matrices; integration; sensor fusion; EKF; FLAS; UKF; covariance matrices; estimation accuracy; extended Kalman filter; fuzzy adaptive unscented Kalman filter; sensor fusion method; tracking capability; ultra-tight GPS-INS integration; Adaptive filter; Fuzzy logic; Ultra-tight integration; Unscented Kalman filter;
fLanguage
English
Publisher
ieee
Conference_Titel
Computational Intelligence and Design (ISCID), 2010 International Symposium on
Conference_Location
Hangzhou
Print_ISBN
978-1-4244-8094-4
Type
conf
DOI
10.1109/ISCID.2010.148
Filename
5692775
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