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Control methodologies for large space structuresThe objectives of this research were to develop techniques of controlling a dc-motor driven flywheel which would apply torque to the structure to which it was mounted. The motor control system was to be implemented using a microprocessor based controller. The purpose of the torque applied by this system was to dampen oscillations of the structure to which it was mounted. Before the work was terminated due to the unavailability of equipment, a system was developed and partially tested which would provide tight control of the flywheel velocity when it received a velocity command in the form of a voltage. The procedure followed in this development was to first model the motor and flywheel system on an analog computer. Prior to the time the microprocessor development system was available, an analog control loop was replaced by the microprocessor and the system was partially tested.
Document ID
19840026396
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Mcree, G. J.
(Old Dominion Univ. Norfolk, VA, United States)
Altonji, E.
(Old Dominion Univ. Norfolk, VA, United States)
Date Acquired
September 4, 2013
Publication Date
August 1, 1984
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
NASA-CR-173987
NAS 1.26:173987
Report Number: NASA-CR-173987
Report Number: NAS 1.26:173987
Accession Number
84N34467
Funding Number(s)
CONTRACT_GRANT: NAG1-318
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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