DocumentCode
810019
Title
Adaptive parameter identification
Author
Kaufman, Howard ; Beaulier, Daniel
Author_Institution
Rensselaer Polytechnic Institute, Troy, NY, USA
Volume
17
Issue
5
fYear
1972
fDate
10/1/1972 12:00:00 AM
Firstpage
729
Lastpage
731
Abstract
An extended Kalman filter with a fictitious noise input is developed for tracking time-varying parameters. An adaptation algorithm is used for adjusting the covariance of the fictitious noise according to the magnitude of the measured residuals and applied to the tracking of time-varying VTOL parameters.
Keywords
Adaptive Kalman filtering; Aircraft control; Kalman filtering; Linear systems, time-varying discrete-time; Parameter identification; VTOL aircraft; Equations; Gaussian noise; Gold; Kalman filters; Noise measurement; Parameter estimation; Q measurement; State estimation; Testing; US Government;
fLanguage
English
Journal_Title
Automatic Control, IEEE Transactions on
Publisher
ieee
ISSN
0018-9286
Type
jour
DOI
10.1109/TAC.1972.1100111
Filename
1100111
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