DocumentCode
1022086
Title
Analytical steady-state solution for a three-state Kalman filter
Author
Beuzit, M.
Author_Institution
Direction des Armements Terrestres Service, ASA, Saint-Cloud, France
Volume
25
Issue
6
fYear
1989
fDate
11/1/1989 12:00:00 AM
Firstpage
828
Lastpage
835
Abstract
A closed-form steady-state solution is presented for the discrete Kalman-Buch filter when only position is measured. The procedure is based on a comparison between the Wiener and Kalman approaches. The solution obtained is more straightforward than the one given by S.N. Gupta (see ibid., vol.AES-20, p.839-49, Nov. 1984), which is difficult to handle when the eigenvalues are complex. The results agree perfectly with those obtained by simulation of Kalman´s recursive equations extended until the steady-state is reached. The results supply apriori tracking performances and are therefore useful for preliminary design. This approach is also applied to the Singer and Fitzgerald model, because of the latter´s physical importance
Keywords
Kalman filters; eigenvalues and eigenfunctions; tracking; Fitzgerald model; Singer model; Wiener; discrete Kalman-Buch filter; recursive equations; steady-state solution; three-state Kalman filter; tracking; Acceleration; Accelerometers; Equations; Kalman filters; Position measurement; Recursive estimation; State estimation; Steady-state; White noise; Wiener filter;
fLanguage
English
Journal_Title
Aerospace and Electronic Systems, IEEE Transactions on
Publisher
ieee
ISSN
0018-9251
Type
jour
DOI
10.1109/7.40721
Filename
40721
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