DocumentCode
1124897
Title
A Fault-Tolerant Estimator for Redundant Systems
Author
Broen, Robert B.
Author_Institution
Control Dynamics McDonnell Aircraft Company, St. Louis, Missouri 63166
Issue
6
fYear
1975
Firstpage
1281
Lastpage
1285
Abstract
This paper proposes a digital estimator for redundant systems which is superior to Kalman Filtering if a failure is present and reduces to Kalman Filtering if no failure is present. Fault tolerant estimation is achieved by defining the non-stationary weighting matrix associated with the nominal least squares estimator (Kalman filter) as a continuous ous nonlinear function of the measurements. Despite the nonlinear character of the failure detection and isolation feature, the estimator equations have closed form and hence require no iterative computations ions or approximations for implementation.
Keywords
Aerodynamics; Aircraft navigation; Digital filters; Equations; Fault tolerant systems; Filtering; Kalman filters; Least squares approximation; Satellite navigation systems; Voting;
fLanguage
English
Journal_Title
Aerospace and Electronic Systems, IEEE Transactions on
Publisher
ieee
ISSN
0018-9251
Type
jour
DOI
10.1109/TAES.1975.308185
Filename
4101560
Link To Document