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A component modes projection and assembly model reduction methodology for articulated, multi-flexible body structuresA two-stage model reduction methodology, combining the classical Component Mode Synthesis (CMS) method and the newly developed Enhanced Projection and Assembly (EP&A) method, is proposed in this research. The first stage of this methodology, called the COmponent Modes Projection and Assembly model REduction (COMPARE) method, involves the generation of CMS mode sets, such as the MacNeal-Rubin mode sets. These mode sets are then used to reduce the order of each component model in the Rayleigh-Ritz sense. The resultant component models are then combined to generate reduced-order system models at various system configurations. A composite mode set which retains important system modes at all system configurations is then selected from these reduced-order system models. In the second stage, the EP&A model reduction method is employed to reduce further the order of the system model generated in the first stage. The effectiveness of the COMPARE methodology has been successfully demonstrated on a high-order, finite-element model of the cruise-configured Galileo spacecraft.
Document ID
19940010149
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Lee, Allan Y.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Tsuha, Walter S.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
September 6, 2013
Publication Date
February 15, 1993
Publication Information
Publication: Proceedings of the Fifth NASA(NSF)DOD Workshop on Aerospace Computational Control
Subject Category
Structural Mechanics
Accession Number
94N14622
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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