首页> 中文期刊> 《中国航空学报(英文版)》 >Inflatable Wing Design Parameter Optimization Using Orthogonal Testing and Support Vector Machines

Inflatable Wing Design Parameter Optimization Using Orthogonal Testing and Support Vector Machines

         

摘要

The robust parameter design method is a traditional approach to robust experimental design that seeks to obtain the optimal combination of factors/levels.To overcome some of the defects of the inflatable wing parameter design method,this paper proposes an optimization design scheme based on orthogonal testing and support vector machines (SVMs).Orthogonal testing design is used to estimate the appropriate initial value and variation domain of each variable to decrease the number of iterations and improve the identification accuracy and efficiency.Orthogonal tests consisting of three factors and three levels are designed to analyze the parameters of pressure,uniform applied load and the number of chambers that affect the bending response of inflatable wings.An SVM intelligent model is established and limited orthogonal test swatches are studied.Thus,the precise relationships between each parameter and product quality features,as well the signal-to-noise ratio (SNR),can be obtained.This can guide general technological design optimization.

著录项

  • 来源
    《中国航空学报(英文版)》 |2012年第6期|887-895|共9页
  • 作者

    WANG Zhifei; WANG Hua;

  • 作者单位

    School of Astronautics,Beihang University,Beijing 100191,China;

    School of Astronautics,Beihang University,Beijing 100191,China;

  • 原文格式 PDF
  • 正文语种 chi
  • 中图分类
  • 关键词

获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号