Title :
Adaptive-gain-and-tau tracking filters for correlated target maneuvers
Author_Institution :
Israel Aircraft Ind. & Bioscan Technol. Ltd., Yokneam
fDate :
March 31 2008-April 4 2008
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;
Conference_Titel :
Acoustics, Speech and Signal Processing, 2008. ICASSP 2008. IEEE International Conference on
Conference_Location :
Las Vegas, NV
Print_ISBN :
978-1-4244-1483-3
Electronic_ISBN :
1520-6149
DOI :
10.1109/ICASSP.2008.4518419