DocumentCode
835834
Title
Autonomous fault-tolerant attitude reference system using DTGs in symmetrically skewed configuration
Author
Murugesan, Sugumar
Author_Institution
Indian Space Res. Org., Bangalore
Volume
25
Issue
2
fYear
1989
fDate
3/1/1989 12:00:00 AM
Firstpage
302
Lastpage
307
Abstract
A novel symmetrically skewed configuration for an attitude reference system (ARS) using three dynamically tuned gyros (DTGs) is developed. Simple schemes for autonomous detection and identification of a faulty DTG in real time and subsequent reconfiguration of the attitude estimation algorithm are proposed. The performance of the present configuration is shown to be better than that of configurations proposed earlier, and it is shown to have better features. It tolerates all types of failures of DTG failures, requires very simple computations, and gives less error in attitude estimate than the other configurations
Keywords
aerospace instrumentation; attitude control; gyroscopes; parameter estimation; aerospace instrumentation; attitude estimation algorithm; autonomous detection; dynamically tuned gyros; fault-tolerant attitude reference system; identification; real time; reconfiguration; symmetrically skewed configuration; Attitude control; Error correction; Fault detection; Fault diagnosis; Fault tolerance; Fault tolerant systems; Filters; Space vehicles; State estimation; Target tracking; Yield estimation;
fLanguage
English
Journal_Title
Aerospace and Electronic Systems, IEEE Transactions on
Publisher
ieee
ISSN
0018-9251
Type
jour
DOI
10.1109/7.18695
Filename
18695
Link To Document