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
Link To Document