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Integrated control/structure optimization by multilevel decompositionA method for integrated control/structure optimization by multilevel decomposition is presented. It is shown that several previously reported methods were actually partial decompositions wherein only the control was decomposed into a subsystem design. One of these partially decomposed problems was selected as a benchmark example for comparison. The system is fully decomposed into structural and control subsystem designs and an improved design is produced. Theory, implementation, and results for the method are presented and compared with the benchmark example.
Document ID
19900009965
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Zeiler, Thomas A.
(Lockheed Engineering and Sciences Co. Hampton, VA., United States)
Gilbert, Michael G.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 6, 2013
Publication Date
March 1, 1990
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
NASA-TM-102619
NAS 1.15:102619
Report Number: NASA-TM-102619
Report Number: NAS 1.15:102619
Meeting Information
Meeting: AIAA Structures, Structural Dynamics, and Materials Conference
Location: Long Beach, CA
Country: United States
Start Date: April 2, 1990
End Date: April 4, 1990
Accession Number
90N19281
Funding Number(s)
PROJECT: RTOP 505-63-21-04
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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