• DocumentCode
    1976957
  • Title

    Study of experimental design and response surface method for surrogate model of computational simulation

  • Author

    Xi, Rui ; Jia, Hongguang ; Xiao, Qianjin

  • Author_Institution
    Changchun Inst. of Opt., Fine Mech. & Phys., Changchun, China
  • fYear
    2011
  • fDate
    16-18 Sept. 2011
  • Firstpage
    4995
  • Lastpage
    4998
  • Abstract
    While the high-precision simulation is widely used in science and technology, Design of Experiment (DOE) based on Response Surface (RS) method can be employed in surrogate model to reduce the cost and error. In order to illustrate the relationship between parameters and response features , several DOE methods and Response Surface (RS) method are studied. The author used polynomial regression and RBF neural network based on orthogonal array to build a rocket aerodynamic discipline surrogate model respectively which proved their feasibility. From the results of the test case, conclusion is drawn that characteristic as well as acclimatization of DOE methods and different approximation should be considered for different issues, so the factors of cost and accuracy could reach a balance synthetically.
  • Keywords
    aerodynamics; design of experiments; mechanical engineering computing; polynomials; radial basis function networks; regression analysis; response surface methodology; rockets; simulation; DOE; RBF neural network; computational simulation; design of experiment; experimental design; polynomial regression; response surface method; rocket aerodynamic; science and technology; surrogate model; Accuracy; Approximation methods; Arrays; Atmospheric modeling; Computational modeling; Polynomials; Response surface methodology; Experimental Design; RBF neural approximation; RSM approximation; surrogate model;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Electrical and Control Engineering (ICECE), 2011 International Conference on
  • Conference_Location
    Yichang
  • Print_ISBN
    978-1-4244-8162-0
  • Type

    conf

  • DOI
    10.1109/ICECENG.2011.6057240
  • Filename
    6057240