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Robust controller synthesis for a large flexible space antennaThe linear-quadratic Gaussian/loop-transfer-recovery method is used to synthesize a fine-pointing control system for a large space antenna. A finite-element model for the 122-m hoop/column antenna is employed, and a compensator, utilizing attitudes sensors and torque actuators, is designed which achieves pointing performance while maintaining stability robustness to unmodeled dynamics. Inclusion of the rigid-body modes plus the first three elastic modes is found to be necessary to achieve a 0.1-rad/s bandwidth. Results are obtained by employing a modification of the standard robustness recovery procedure, which reduces the conservative nature of the design methodology. Performance degradation is encountered due to the presence of unavoidable invariant zeros within the design bandwidth.
Document ID
19870044961
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Sundararajan, N.
(Old Dominion University Research Foundation, Norfolk, VA, United States)
Joshi, S. M.
(Old Dominion Univ. Norfolk, VA, United States)
Armstrong, E. S.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 13, 2013
Publication Date
April 1, 1987
Publication Information
Publication: Journal of Guidance, Control, and Dynamics
Volume: 10
ISSN: 0731-5090
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
ISSN: 0731-5090
Accession Number
87A32235
Distribution Limits
Public
Copyright
Other

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