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On parameter identification for large space structuresThe design of a controller for large space structures (LSS) based on the LQG theory requires the knowledge of the LSS parameters. Since apriori knowledge of the parameters is usually not reliable, the parameters must be identified prior to the controller synthesis, using methods such as the maximum likelihood technique. An expression is obtained for the Fisher information matrix for LSS, from which Cramer-Rao bounds can be obtained in order to determine the accuracy with which the parameters can be identified.
Document ID
19830016272
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Joshi, S. M.
(Old Dominion Univ. Norfolk, VA, United States)
Goglia, G. L.
(Old Dominion Univ. Norfolk, VA, United States)
Date Acquired
September 4, 2013
Publication Date
May 1, 1983
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
NASA-CR-170306
NAS 1.26:170306
Report Number: NASA-CR-170306
Report Number: NAS 1.26:170306
Accession Number
83N24543
Funding Number(s)
CONTRACT_GRANT: NAG1-102
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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