Multiobjective Optimization Using Adjoint Gradient Enhanced Approximation Models for Genetic Algorithms

作者: Sangho Kim , Hyoung-Seog Chung

DOI: 10.1007/11751649_54

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摘要: In this work, a multiobjective design optimization framework is developed by combining GAs and an approximation technique called Kriging method which can produce fairly accurate global approximations to the actual space provide function evaluations efficiently. It applied wing planform problem its results demonstrate efficiency applicability of proposed framework. Furthermore, improve propsed using adjoint gradients two different approaches are tested. The show that gradient efficiently replace computationally expensive sample data needed for constructing models, gradient-based techniques be utilized refine candidates obtained through model based genetic algorithms.

参考文章(25)
Sean Rikio Wakayama, Lifting surface design using multidisciplinary optimization Stanford University. ,(1995)
Timothy W. Simpson, Comparison of Response Surface and Kriging Models in the Multidisciplinary Design of an Aerospike Nozzle Institute for Computer Applications in Science and Engineering (ICASE). ,(1998)
Carlos A. Coello Coello Coello, Gregorio Toscano Pulido, A Micro-Genetic Algorithm for Multiobjective Optimization international conference on evolutionary multi criterion optimization. pp. 126- 140 ,(2001) , 10.1007/3-540-44719-9_9
Antony Jameson, Aerodynamic design via control theory Journal of Scientific Computing. ,vol. 3, pp. 233- 260 ,(1988) , 10.1007/BF01061285
Kalyanmoy Deb, An introduction to genetic algorithms Sadhana-academy Proceedings in Engineering Sciences. ,vol. 24, pp. 293- 315 ,(1999) , 10.1007/BF02823145
J. Vassberg, L. Martinelli, J. Reuther, J. Vassberg, J. Alonso, A. Jameson, J. Alonso, A. Jameson, L. Martinelli, J. Reuther, An Efficient Multiblock Method for Aerodynamic Analysis and Design on Distributed Memory Systems 13th Computational Fluid Dynamics Conference, 1997. ,(1997) , 10.2514/6.1997-1893
Michael Stein, Large sample properties of simulations using latin hypercube sampling Technometrics. ,vol. 29, pp. 143- 151 ,(1987) , 10.2307/1269769
Antony Jameson, Optimum aerodynamic design using CFD and control theory 12th Computational Fluid Dynamics Conference. ,(1995) , 10.2514/6.1995-1729
R. J. Beckman, M. D. McKay, W. J. Conover, A comparison of three methods for selecting values of input variables in the analysis of output from a computer code Technometrics. ,vol. 42, pp. 55- 61 ,(2000) , 10.2307/1271432