• CN:11-2187/TH
  • ISSN:0577-6686

›› 2009, Vol. 45 ›› Issue (12): 7-14.

• 论文 • 上一篇    下一篇

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基于代理模型的水下滑翔机机翼设计优化方法

谷海涛;林扬;胡志强;俞建成   

  1. 中国科学院沈阳自动化研究所机器人学国家重点实验室;中国科学院研究生院
  • 发布日期:2009-12-15

Surrogate Models Based Optimization Methods for the Design of Underwater Glider Wing

GU Haitao;LIN Yang;HU Zhiqiang;YU Jiancheng   

  1. State Key Laboratory of Robotics, Shenyang Institute of Automation, Chinese Academy of Sciences Graduate School, Chinese Academy of Sciences
  • Published:2009-12-15

摘要: 在复杂工程系统的概念设计优化中,高精度数值分析方法得到广泛应用,将高精度数值分析与优化方法有机结合,对设计空间展开全面搜索与寻优,已经成为现代设计优化方法的重要发展方向。以水下滑翔机的概念设计为研究对象,引入代理模型,控制高精度分析试验的数量,有效地化解精度与效率之间的矛盾。将参数化几何建模、网格划分以及流体数值模拟分析集成为自动分析流程,并以此为基础采用试验设计理论,构建代理模型,解决水下滑翔机机翼的多目标设计优化问题。给出基于代理模型的设计优化过程,并系统地比较几种试验设计方法的适应性,重点讨论多项式响应面和径向基函数代理模型,所得代理模型相对误差小于2%。采用梯度寻优方法与遗传算法在给定设计空间内进行全面搜索,获得机翼的最佳平 面构形,水下滑翔机的升阻比提高6.76%,俯仰力矩的绝对值由0.276 0 N•m降低为0.001 5 N•m,提高水下滑翔机的运动性能。

关键词: 代理模型, 设计优化, 试验设计, 水下滑翔机

Abstract: High precision numerical analysis methods have been extensively used in the conceptual design of complex engineering systems. Combining high precision numerical analysis methods with optimization algorithms to make a systematic exploration of the design space has become an important topic in the modern design method. During the design process of an underwater glider’s wing, a surrogate model is introduced to decrease the computation times of high precision analysis. By this means, the contradiction between precision and efficiency is solved effectively. Through integrating the parametric geometry modeling, mesh generation and computational fluid dynamics analysis as an automatic workflow, and adopting the design of experiment (DOE) theory, a surrogate model is constructed to solve the multi-objects design optimization problem of the underwater glider. The procedure of surrogate model construction is presented and several DOE methods are compared systematically, especially the characteristics and applicability of the response surface model and the radial basis functions model. A fast design exploration and optimization is implemented and the optimal plane of the underwater glider is found out based on the surrogate model. Optimization results show that the lift drag ratio improves about 6.76%, and the pitch moment is reduced from 0.276 0 N•m to 0.001 5 N•m.

Key words: Design of experiment, Design optimization, Surrogate models, Underwater glider

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