NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Autonomous fault-tolerant attitude reference system using DTGs in symmetrically skewed configurationA 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.
Document ID
19890052254
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
External Source(s)
Authors
Murugesan, S.
(NASA Ames Research Center Moffett Field, CA; ISRO, Satellite Centre, Bangalore, India)
Goel, P. S.
(ISRO, Satellite Centre Bangalore, India)
Date Acquired
August 14, 2013
Publication Date
March 1, 1989
Publication Information
Publication: IEEE Transactions on Aerospace and Electronic Systems
Volume: 25
ISSN: 0018-9251
Subject Category
Spacecraft Design, Testing And Performance
Accession Number
89A39625
Distribution Limits
Public
Copyright
Other

Available Downloads

There are no available downloads for this record.
No Preview Available