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Substructure-based control of flexible structuresA decentralized procedure is presented for the design of controllers for flexible structures. Spatially significant components are created which approximate the response of a specific part of the complete structure. For each component, the controller and observer gain matrices which are used in a controller for the complete structure. The proposed method is illustrated on a model of NASA Langley's CSI testbed structure.
Document ID
19930050218
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Babuska, Vit (NASA Lyndon B. Johnson Space Center Houston, TX, United States)
Craig, Roy R., Jr. (Texas Univ. Austin, United States)
Date Acquired
August 16, 2013
Publication Date
January 1, 1993
Publication Information
Publication: In: AIAA(ASME)ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, 34th and AIAA/ASME Adaptive Structures Forum, La Jolla, CA, Apr. 19-22, 1993, Technical Papers. Pt. 6 (A93-33876 1
Publisher: American Institute of Aeronautics and Astronautics
Subject Category
Cybernetics
Report/Patent Number
AIAA PAPER 93-1671
Report Number: AIAA PAPER 93-1671
Accession Number
93A34215
Funding Number(s)
CONTRACT_GRANT: NAG9-357
Distribution Limits
Public
Copyright
Other

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IDRelationTitle19930049879Collected Works34th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, and AIAA/ASME Adaptive Structures Forum, La Jolla, CA, Apr. 19-22, 1993, Technical Papers. Pts. 1-619930049879Collected Works34th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, and AIAA/ASME Adaptive Structures Forum, La Jolla, CA, Apr. 19-22, 1993, Technical Papers. Pts. 1-6
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