DocumentCode
1123502
Title
Performance Evaluation of Suboptimal Filters
Author
Asher, Robert B. ; Reeves, Richard M.
Author_Institution
Frank J. Seiler Research Laboratory, US Air Force Academy, Colorado
Issue
3
fYear
1975
fDate
5/1/1975 12:00:00 AM
Firstpage
400
Lastpage
405
Abstract
The use of a Kalman filter in an applications problem requires a detailed model of both the system dynamics and the measurement dynamics. The model for many problems may be extremely large in dimensionality. However, in many instances one has a limited computer capability and, thus, must purposely introduce modeling errors into the filter in order to gain a computational advantage. However, as is well known, this may lead to the phenomenon of filter divergence. This paper considers the development of equations which allow one to evaluate a filter of reduced state. The equations are based upon using covariance analysis techniques in order to determine the true root-mean-square estimation error. These equations are computationally more advantageous than others appearing in the literature.
Keywords
Aerodynamics; Aerospace electronics; Computer errors; Covariance matrix; Equations; Estimation error; Filters; Force measurement; Laboratories; State estimation;
fLanguage
English
Journal_Title
Aerospace and Electronic Systems, IEEE Transactions on
Publisher
ieee
ISSN
0018-9251
Type
jour
DOI
10.1109/TAES.1975.308092
Filename
4101422
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