DocumentCode
3419928
Title
Adaptive-gain-and-tau tracking filters for correlated target maneuvers
Author
Chernoguz, Naum
Author_Institution
Israel Aircraft Ind. & Bioscan Technol. Ltd., Yokneam
fYear
2008
fDate
March 31 2008-April 4 2008
Firstpage
3553
Lastpage
3556
Abstract
The so-called adaptive-gain-and-tau filter extends a recently suggested adaptive-gain tracking filter to a case with correlated target maneuver. The transition matrix of an appropriate Kalman filter (KF) depends on the maneuver correlation time, and the associated with this KF transfer function specifies the ARMA coefficients coupling the correlation time and the KF gain. Due to this link, one adaptation scheme is based on the ARMA identification. Another form of the adaptive filter represents a joint parameter/state estimator. Simulations undertaken for tracking filters of orders 2-4 illustrate their behavior and compare adaptively found parameters to optimal.
Keywords
Kalman filters; adaptive filters; autoregressive moving average processes; matrix algebra; tracking filters; transfer functions; ARMA coefficients; Kalman filter; adaptation scheme; adaptive-gain-and-tau tracking filters; correlated target maneuvers; joint parameter-state estimator; maneuver correlation time; transfer function; transition matrix; Adaptive filters; Aerospace industry; Aircraft; Kalman filters; Kinematics; Motion measurement; Noise measurement; Parameter estimation; State estimation; Target tracking; ARMA; Target tracking; adaptive filter;
fLanguage
English
Publisher
ieee
Conference_Titel
Acoustics, Speech and Signal Processing, 2008. ICASSP 2008. IEEE International Conference on
Conference_Location
Las Vegas, NV
ISSN
1520-6149
Print_ISBN
978-1-4244-1483-3
Electronic_ISBN
1520-6149
Type
conf
DOI
10.1109/ICASSP.2008.4518419
Filename
4518419
Link To Document