A Mixed Integer Efficient Global Optimization Algorithm with Multiple Infill Strategy - Applied to a Wing Topology Optimization Problem

Roy, Satadru ; Crossley, William A ; Stanford, Bret K ; Moore, Kenneth T ; Gray, Justin S

关键词: ALGORITHMS;    COMPUTERIZED SIMULATION;    DESIGN ANALYSIS;    DESIGN OPTIMIZATION;    DISCRETE FUNCTIONS;    GRADIENTS;    INTEGERS;    MACHINE LEARNING;    MULTIDISCIPLINARY DESIGN OPTIMIZATION;    NONLINEAR PROGRAMMING;    NONLINEARITY;    NUMERICAL ANALYSIS;    PROBABILITY DISTRIBUTION FUNCTIONS;    WINGS;   

RP-ID  :  GRC-E-DAA-TN63373

学科分类：航空航天科学

美国|英语

来源: NASA Technical Reports Server

【 摘 要 】

With 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.