DocumentCode
1148281
Title
Spectral Analysis of Optimal and Suboptimal Gyro Monitoring Filters
Author
Galdos, Jorge I.
Author_Institution
Lincoln Laboratory
Issue
3
fYear
1985
fDate
5/1/1985 12:00:00 AM
Firstpage
372
Lastpage
378
Abstract
Gyro monitoring filters are used to estimate and correct gyro drift rates of local-level inertial navigation systems. Conventional gyro monitoring filters are usually designed based on a simplified model of gyro drift rate. Furthermore, the effectiveness of these filters-and of many filters of the "Kalman" type-is often measured in terms of the root mean square (rms) criterion in contrast to the spectral content criterion typical of classical Wiener filtering theory. This paper has two objectives: to propose a gyro monitoring filter which is based on a more detailed model of gyro drift rate; and to propose a method of filter performance evaluation which uses as criterion a measure of the spectral content of the error process. The proposed gyro monitoring filter is shown to have improved spectral contents resulting in superior navigation performance for the gyro error models used in the calculations (comparable to commercial-grade aircraft gyros).
Keywords
Aircraft navigation; Filtering theory; Inertial navigation; Kalman filters; Monitoring; Root mean square; Sea measurements; Spectral analysis; Vehicle dynamics; Wiener filter;
fLanguage
English
Journal_Title
Aerospace and Electronic Systems, IEEE Transactions on
Publisher
ieee
ISSN
0018-9251
Type
jour
DOI
10.1109/TAES.1985.310567
Filename
4104066
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