A Mixed Integer Efficient Global Optimization Algorithm with Multiple Infill Strategy - Applied to a Wing Topology Optimization ProblemWith the advancement in high performance computing and numerical optimization techniques,engineering design optimization problems are becoming more complex, larger scale,higher fidelity, and computationally more demanding, requiring longer run times than ever before. There exists methodologies and techniques that can address some of these challenges but very few can address all, and most are limited in the extent that these concerns can be addressed. With the goal of addressing such challenging engineering problems, we developed anew optimization framework, named AMIEGO, that combines concepts from surrogate-based optimization approaches, gradient-based numerical methods, Partial Least Squares, evolutionary algorithms, and Branch-and-Bound, providing newer capabilities that were not previouslyperceived. However, the original version of this framework, in the process of adaptive samplingto explore and exploit the design space, finds only a single sample point per iteration. The efforthere builds upon this previously developed optimization framework to include multiple infillsampling capability that combines the concept of generalized expected improvement function,unsupervised learning, and multi-objective evolutionary technique. To demonstrate, AMIEGOwith the multiple infill capability (called AMIEGO-MIMOS) solves a series of increasingly difficultengineering design optimization problems. The results reveal the performance of the newapproach is problem dependent. When applied to a ten-bar truss problem, the newly proposedmultiple infill strategy consistently leads to a better design solutions when compared to theexisting CPTV method (implemented with the context of the AMIEGO framework). On theother hand, when applied to a mixed-integer high fidelity wing topology optimization problem- MIMOS, despite showing a steeper convergence at the start, eventually leads to an inferiorsolution as compared to CPTV approach. These results also reveal that a small number ofstarting points, in general, are sufficient to lead to a good overall solution.
Document ID
20190004989
Acquisition Source
Glenn Research Center
Document Type
Conference Paper
Authors
Roy, Satadru (National Inst. of Aerospace Associates Reston, VA, United States)
Crossley, William A. (Purdue Univ. Westiville, IN, United States)
Stanford, Bret K. (NASA Langley Research Center Hampton, VA, United States)
Moore, Kenneth T. (DB Consulting Group, Inc. Cleveland, OH, United States)
Gray, Justin S. (NASA Glenn Research Center Cleveland, OH, United States)
Date Acquired
May 6, 2019
Publication Date
January 7, 2019
Subject Category
Aeronautics (General)
Report/Patent Number
GRC-E-DAA-TN63373Report Number: GRC-E-DAA-TN63373
Meeting Information
Meeting: AIAA Science and Technology Forum and Exposition (SciTech)
Location: San Diego, CA
Country: United States
Start Date: January 7, 2019
End Date: January 11, 2019
Sponsors: American Institute of Aeronautics and Astronautics (AIAA)