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
Link To Document :
بازگشت