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
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;
Conference_Titel :
Electrical and Control Engineering (ICECE), 2011 International Conference on
Conference_Location :
Yichang
Print_ISBN :
978-1-4244-8162-0
DOI :
10.1109/ICECENG.2011.6057240