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Preliminary Structural Design Using Topology Optimization with a Comparison of Results from Gradient and Genetic Algorithm MethodsIn this paper, genetic algorithm based and gradient-based topology optimization is presented in application to a real hardware design problem. Preliminary design of a planetary lander mockup structure is accomplished using these methods that prove to provide major weight savings by addressing the structural efficiency during the design cycle. This paper presents two alternative formulations of the topology optimization problem. The first is the widely-used gradient-based implementation using commercially available algorithms. The second is formulated using genetic algorithms and internally developed capabilities. These two approaches are applied to a practical design problem for hardware that has been built, tested and proven to be functional. Both formulations converged on similar solutions and therefore were proven to be equally valid implementations of the process. This paper discusses both of these formulations at a high level.
Document ID
20140011600
Acquisition Source
Marshall Space Flight Center
Document Type
Conference Paper
Authors
Burt, Adam O.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Tinker, Michael L.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
September 12, 2014
Publication Date
June 16, 2014
Subject Category
Structural Mechanics
Report/Patent Number
M13-3070
Report Number: M13-3070
Meeting Information
Meeting: AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference
Location: Atlanta, GA
Country: United States
Start Date: June 16, 2014
End Date: June 20, 2014
Sponsors: American Inst. of Aeronautics and Astronautics
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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