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Passive stabilization for large space systemsThe optimal tuning of multiple tuned-mass dampers for the transient vibration damping of large space structures is investigated. A multidisciplinary approach is used. Structural dynamic techniques are applied to gain physical insight into absorber/structure interaction and to optimize specific cases. Modern control theory and parameter optimization techniques are applied to the general optimization problem. A design procedure for multi-absorber multi-DOF vibration damping problems is presented. Classical dynamic models are extended to investigate the effects of absorber placement, existing structural damping, and absorber cross-coupling on the optimal design synthesis. The control design process for the general optimization problem is formulated as a linear output feedback control problem via the development of a feedback control canonical form. The techniques are applied to sample micro-g and pointing problems on the NASA dual keel space station.
Document ID
19870010322
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Sesak, J. R.
(Lockheed Missiles and Space Co. Sunnyvale, CA, United States)
Gronet, M. J.
(Lockheed Missiles and Space Co. Sunnyvale, CA, United States)
Marinos, G. M.
(Lockheed Missiles and Space Co. Sunnyvale, CA, United States)
Date Acquired
September 5, 2013
Publication Date
April 1, 1987
Publication Information
Publisher: NASA
Subject Category
Structural Mechanics
Report/Patent Number
NAS 1.26:4067
NASA-CR-4067
Report Number: NAS 1.26:4067
Report Number: NASA-CR-4067
Accession Number
87N19755
Funding Number(s)
CONTRACT_GRANT: NAS1-17660
PROJECT: RTOP 506-43-41-02
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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