TY - GEN
T1 - Study of hybrid radial basis function for design optimization problems
AU - Shi, Renhe
AU - Liu, Li
AU - Long, Teng
AU - Liu, Jian
N1 - Publisher Copyright:
© 2015, American Institute of Aeronautics and Astronautics Inc, AIAA. All rigths reserved.
PY - 2015
Y1 - 2015
N2 - Radial basis function (RBF) surrogate model has been widely applied in engineering design optimization problems. Ensemble of RBF (ERBF) combines individual RBF together linearly by using weighted factors to improve approximation behavior of surrogate models. In this paper, a new RBF ensemble method referred as hybrid radial basis function (HRBF) is proposed. Different from the conventional ERBF methods, HRBF determines the weighted factors through solving an optimal quadratic programming problem. Several methods to solve the optimal quadratic programming problem are investigated. Standard numerical test functions are utilized to assess the performances of various ERBFs. The results show that the proposed HRBF can significantly improve the modeling efficiency compared with the conventional ERBF methods. Moreover, the approximation accuracy of HRBF is also slightly improved. Finally, a satellite multidisciplinary design optimization problem is used to illustrate the effectiveness of HRBF in solving real-world engineering design optimization problem.
AB - Radial basis function (RBF) surrogate model has been widely applied in engineering design optimization problems. Ensemble of RBF (ERBF) combines individual RBF together linearly by using weighted factors to improve approximation behavior of surrogate models. In this paper, a new RBF ensemble method referred as hybrid radial basis function (HRBF) is proposed. Different from the conventional ERBF methods, HRBF determines the weighted factors through solving an optimal quadratic programming problem. Several methods to solve the optimal quadratic programming problem are investigated. Standard numerical test functions are utilized to assess the performances of various ERBFs. The results show that the proposed HRBF can significantly improve the modeling efficiency compared with the conventional ERBF methods. Moreover, the approximation accuracy of HRBF is also slightly improved. Finally, a satellite multidisciplinary design optimization problem is used to illustrate the effectiveness of HRBF in solving real-world engineering design optimization problem.
UR - http://www.scopus.com/inward/record.url?scp=85088766526&partnerID=8YFLogxK
U2 - 10.2514/6.2015-3236
DO - 10.2514/6.2015-3236
M3 - Conference contribution
AN - SCOPUS:85088766526
SN - 9781624103681
T3 - 16th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference
BT - 16th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference
PB - American Institute of Aeronautics and Astronautics Inc, AIAA
T2 - 16th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference, 2015
Y2 - 22 June 2015 through 26 June 2015
ER -