NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
A consistent model reduction of measured modal parameters for reduced-order active controlThe problem of synthesizing reduced-order linear models of vibrating structures for the design of fixed-order dynamic feedback control is investigated. The present technique builds on a recently developed procedure for constructing an objective set of mass and stiffness matrices from measured modal parameters that are akin to the Craig-Bampton synthesized ones obtained from finite element models. The constructed mass and stiffness matrices are determined directly from the identification of experimental data, however, rather than through correlation or reconciliation of a finite element model. A model truncation criterion is then applied to the identified minimum-order mass and stiffness model to satisfy certain observability/controllability requirements for the reduced model. Numerical examples illustrate the effectiveness of the proposed technique for synthesizing reduced-order controllers from system realizations of experimental data. The dynamic performance of the resulting closed-loop models is assessed using the known full-order structural dynamics and compared with existing model reduction techniques.
Document ID
19930067367
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Alvin, K. F.
(NASA Langley Research Center Hampton, VA, United States)
Park, K. C.
(NASA Langley Research Center Hampton, VA, United States)
Peterson, L. D.
(Colorado Univ. Boulder, United States)
Date Acquired
August 16, 2013
Publication Date
January 1, 1993
Publication Information
Publication: In: AIAA Guidance, Navigation and Control Conference, Monterey, CA, Aug. 9-11, 1993, Technical Papers. Pt. 2 (A93-51301 22-63)
Publisher: American Institute of Aeronautics and Astronautics
Subject Category
Cybernetics
Report/Patent Number
AIAA PAPER 93-3769
Accession Number
93A51364
Funding Number(s)
CONTRACT_GRANT: JPL-959444
CONTRACT_GRANT: NAG1-1200
Distribution Limits
Public
Copyright
Other

Available Downloads

There are no available downloads for this record.
No Preview Available