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Integrated Structure/Control Design - Present Methodology and Future OpportunitiesAttention is given to current methodology applied to the integration of the optimal design process for structures and controls. Multilevel linear decomposition techniques proved to be most effective in organizing the computational efforts necessary for ISCD (integrated structures and control design) tasks. With the development of large orbiting space structures and actively controlled, high performance aircraft, there will be more situations in which this concept can be applied.
Document ID
19860064356
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
T A Weisshaar
(Purdue University West Lafayette, IN, United States)
J R Newsom
(NASA Langley Research Center Hampton, VA, United States)
T A Zeiler
(Purdue Univ. West Lafayette, IN, United States)
M G Gilbert
(PRC Kentron, Inc. Hampton, VA, United States)
Date Acquired
August 12, 2013
Publication Date
January 1, 1986
Publication Information
Publication: Proceedings of the 15th Congress of the International Council of the Aeronautical Sciences
Publisher: American Institute of Aeronautics and Astronautics
Volume: 1
ISBN: 0930403169
Subject Category
Cybernetics
Report/Patent Number
ICAS-86-4.8.1
Meeting Information
Meeting: 15th Congress of the International Council of the Aeronautical Sciences (ICAS)
Location: London
Country: GB
Start Date: September 7, 1986
End Date: September 14, 1986
Sponsors: International Council of the Aeronautical Sciences, American Institute of Aeronautics and Astronautics
Accession Number
86A49094
Distribution Limits
Public
Copyright
Other

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