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Bi-Level Integrated System Synthesis (BLISS)BLISS is a method for optimization of engineering systems by decomposition. It separates the system level optimization, having a relatively small number of design variables, from the potentially numerous sub-system optimizations that may each have a large number of local design variables. The subsystem optimizations are autonomous and may be conducted concurrently. Subsystem and system optimizations alternate, linked by sensitivity data, producing a design improvement in each iteration. Starting from a best guess initial design, the method improves that design in iterative cycles, each cycle comprised of two steps. In step one, the system level variables are frozen and the improvement is achieved by separate, concurrent, and autonomous optimizations in the local variable subdomains. In step two, further improvement is sought in the space of the system level variables. Optimum sensitivity data link the second step to the first. The method prototype was implemented using MATLAB and iSIGHT programming software and tested on a simplified, conceptual level supersonic business jet design, and a detailed design of an electronic device.
Document ID
20040090499
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Sobieszczanski-Sobieski, Jaroslaw
(NASA Langley Research Center Hampton, VA, United States)
Agte, Jeremy S.
(Joint Inst. for the Advancement of Flight Sciences Hampton, VA, United States)
Sandusky, Robert R., Jr.
(Joint Inst. for the Advancement of Flight Sciences Hampton, VA, United States)
Date Acquired
August 21, 2013
Publication Date
January 1, 1998
Subject Category
Computer Programming And Software
Report/Patent Number
AIAA Paper 98-4916
Meeting Information
Meeting: 7th AIAA/USAF/NASA/ISSMO Symposium on ultidisciplinary Analysis and Optimization
Location: Saint Louis, MO
Country: United States
Start Date: September 2, 1998
End Date: September 4, 1998
Sponsors: International Society for Structural and Multidisciplinary Optimization, American Inst. of Aeronautics and Astronautics, Department of the Air Force, NASA Headquarters
Distribution Limits
Public
Copyright
Public Use Permitted.
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