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基于动力学演化样本的代理模型优化方法

Surrogate model optimization method based on dynamic evolution sample
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摘要 为提高代理模型的精度,将动力学演化样本生成方法引入代理模型优化设计。采用拉丁超立方抽样得到初始样本点集,基于动力学演化计算生成均匀性更佳的样本点集,并用于Kriging代理模型构造,结合遗传算法给出一套基于动力学演化的代理模型优化方法。通过经典测试函数和某实际机床横梁的优化分析,证明演化后点集在代理模型构建和模型全局寻优上的优越性。 To improve the accuracy of the surrogate model, the dynamic evolution sample generation method is introduced into surrogate model optimization design. The initial sample point set is obtained by Latin hypercube sampling, and the sample point set with better uniformity is generated based on the dynamic evolution calculation, which is used to construct Kriging surrogate model. Combined with genetic algorithm, an optimization method of surrogate model based on the dynamic evolution is proposed. The superiority of the evolved point set in the surrogate model construction and the model global optimization is proved by the classical test functions and the optimization analysis of an actual machine tool beam.
作者 胡钊晖 邓琎 李再参 吴锋 钟万勰 HU Zhaohui;DENG Jin;LI Zaican;WU Feng;ZHONG Wanxie(Department of Engineering Mechanics,Dalian University of Technology,Dalian 116024,Liaoning,China;Yunnan Provincial Key Laboratory of Mechatronics Application Technology,Yunnan Machinery Research and Design Institute Co.,Ltd.,Kunming 650031,China;ZHONG Wanxie Academician Workstation,Yunnan Machinery Research and Design Institute Co.,Ltd.,Kunming 650031,China)
出处 《计算机辅助工程》 2022年第3期1-4,共4页 Computer Aided Engineering
基金 国家自然科学基金(51609034) 辽宁省科学基金(2021-MS-119) 中央高校基本科研业务费(DUT20GJ216) 云南省科技人才与平台计划钟万勰院士云南工作站(202005AF150002) 大连市青年科技之星项目(2018RQ06) 先进装备制造专项(202102AC080002)。
关键词 动力学演化 KRIGING模型 遗传算法 机床横梁 优化 样本集 dynamic evolution Kriging model genetic algorithm machine tool beam optimization sample set
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  • 1穆雪峰,姚卫星,余雄庆,刘克龙,薛飞.多学科设计优化中常用代理模型的研究[J].计算力学学报,2005,22(5):608-612. 被引量:152
  • 2韩永志,高行山,李立州,岳珠峰.基于Kriging模型的涡轮叶片多学科设计优化[J].航空动力学报,2007,22(7):1055-1059. 被引量:38
  • 3GOLOVIDOV, OLEG B, MASON, et al. Response Surface Approximations for Aerodynamic Parameters in High Speed Civil Transport Optimization[A]. Technical Report,Computer Science[DB/OL], Virginia Polytechnic Institute and State University. http://historical.ncstrl.org/tr/ps/vatechcs/TR-97-15.ps.
  • 4KNILL D L, GIUNTA A A, BAKER C A, et al. Response surface models combining linear and euler aerodynamics for supersonic transport design[J]. J Aircraft, 1999,36(1):75-86.
  • 5UNAL R, LEPSCH R A, MCMILLIN M. Response Surface Model Building and Multidisciplinary Optimization Using D-Optimal Designs[A]. Colle-ction of Technical Papers for 7th Annual AIAA/NASA/ISSMO Symposium on Multidisciplinary Analysis and Optimization[C].1998,405-411.
  • 6JIN R, CHEN W, SIMPSON T W. Comparative studies of metamodeling techniques under multiple modeling criteria[J]. Journal of Structural and Multidisciplinary Optimization, 2001,23(1):1-13.
  • 7GIUNTA A A, DUDLEY J M, NARDUCCI R, et al. Noisy Aerodynamic Response and Smooth Approximations in HSCT Design[A]. Proceedings of the 5th AIAA/USAF/NASA/ISSMO Symposium on Multidisciplinary Analysis and Optimization[C]. Panama City Beach, FL, AIAA Paper94-4376, 1994,1117-1128.
  • 8GIUNTA A A, WATSON L T. A Comparison of Approximation Modeling Techniques: Polynomial Versus Interpolating Models[A]. 7th AIAA/USAF/NASA/ISSMO Symposium on Multidiscipli-nary Analysis & Optimization[C]. St. Louis, MO, AIAA, September 2-4, 1998, 1:392-404.
  • 9SOREN N. Lophaven, Hans Bruun Nielsen, Jacob Sondergaard. Aspects of the Matlab Toolbox DACE[A]. Report IMM-REP-2002-12, Informatics and Mathematical Modeling[DB/OL],Technical Univer-sity of Denmark,2002. http://www.imm.dtu.dk/-hbn/dace/.
  • 10SOREN N. Lophaven, Hans Bruun Nielsen, Jacob Sondergaard. DACE A Matlab Kriging Toolbox[A].Report IMM -REP-2002-13,Informatics and Mathematical Modeling[DB/OL].Technical Univer-sity of Denmark, 2002. http://www.imm.dtu.dk/-hbn/dace/.

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