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Large space structure damping designSeveral FORTRAN subroutines and programs were developed which compute complex eigenvalues of a damped system using different approaches, and which rescale mode shapes to unit generalized mass and make rigid bodies orthogonal to each other. An analytical proof of a Minimum Constrained Frequency Criterion (MCFC) for a single damper is presented. A method to minimize the effect of control spill-over for large space structures is proposed. The characteristic equation of an undamped system with a generalized control law is derived using reanalysis theory. This equation can be implemented in computer programs for efficient eigenvalue analysis or control quasi synthesis. Methods to control vibrations in large space structure are reviewed and analyzed. The resulting prototype, using electromagnetic actuator, is described.
Document ID
19830011534
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Pilkey, W. D.
(Virginia Univ. Charlottesville, VA, United States)
Haviland, J. K.
(Virginia Univ. Charlottesville, VA, United States)
Date Acquired
September 4, 2013
Publication Date
January 1, 1983
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
NAS 1.26:170020
UVA/528201/MAE83/101
NASA-CR-170020
Report Number: NAS 1.26:170020
Report Number: UVA/528201/MAE83/101
Report Number: NASA-CR-170020
Accession Number
83N19805
Funding Number(s)
CONTRACT_GRANT: NAG1-137
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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