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Bi-Level Integrated System Synthesis (BLISS) for Concurrent and Distributed ProcessingThe paper introduces a new version of the Bi-Level Integrated System Synthesis (BLISS) methods intended for optimization of engineering systems conducted by distributed specialty groups working concurrently and using a multiprocessor computing environment. The method decomposes the overall optimization task into subtasks associated with disciplines or subsystems where the local design variables are numerous and a single, system-level optimization whose design variables are relatively few. The subtasks are fully autonomous as to their inner operations and decision making. Their purpose is to eliminate the local design variables and generate a wide spectrum of feasible designs whose behavior is represented by Response Surfaces to be accessed by a system-level optimization. It is shown that, if the problem is convex, the solution of the decomposed problem is the same as that obtained without decomposition. A simplified example of an aircraft design shows the method working as intended. The paper includes a discussion of the method merits and demerits and recommendations for further research.
Document ID
20030015489
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Sobieszczanski-Sobieski, Jaroslaw
(NASA Langley Research Center Hampton, VA United States)
Altus, Troy D.
(George Washington Univ. Hampton, VA United States)
Phillips, Matthew
(George Washington Univ. Hampton, VA United States)
Sandusky, Robert
(George Washington Univ. Hampton, VA United States)
Date Acquired
September 7, 2013
Publication Date
January 1, 2002
Subject Category
Computer Programming And Software
Report/Patent Number
AIAA Paper 2002-5409
Report Number: AIAA Paper 2002-5409
Meeting Information
Meeting: 9th AIAA/NASA/USAF/ISSMO Symposium on Multidisciplinary Analysis and Optimization
Location: Atlanta, GA
Country: United States
Start Date: September 4, 2002
End Date: September 6, 2002
Sponsors: Department of the Air Force, International Society for Structural and Multidisciplinary Optimization, American Inst. of Aeronautics and Astronautics, NASA Headquarters
Distribution Limits
Public
Copyright
Public Use Permitted.
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