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NASA Workshop on Distributed Parameter Modeling and Control of Flexible Aerospace SystemsAlthough significant advances have been made in modeling and controlling flexible systems, there remains a need for improvements in model accuracy and in control performance. The finite element models of flexible systems are unduly complex and are almost intractable to optimum parameter estimation for refinement using experimental data. Distributed parameter or continuum modeling offers some advantages and some challenges in both modeling and control. Continuum models often result in a significantly reduced number of model parameters, thereby enabling optimum parameter estimation. The dynamic equations of motion of continuum models provide the advantage of allowing the embedding of the control system dynamics, thus forming a complete set of system dynamics. There is also increased insight provided by the continuum model approach.
Document ID
19940031358
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
Marks, Virginia B.
(NASA Langley Research Center Hampton, VA, United States)
Keckler, Claude R.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 6, 2013
Publication Date
June 1, 1994
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
NASA-CP-3242
NAS 1.55:3242
L-17362
Report Number: NASA-CP-3242
Report Number: NAS 1.55:3242
Report Number: L-17362
Accession Number
94N35865
Funding Number(s)
PROJECT: RTOP 233-01-01-05
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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