TY - GEN
T1 - Dual-sampling based co-kriging method for design optimization problems with multi-fidelity models
AU - Shi, Renhe
AU - Liu, Li
AU - Long, Teng
AU - Wu, Yufei
AU - Tang, Yifan
N1 - Publisher Copyright:
© 2018, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.
PY - 2018
Y1 - 2018
N2 - To improve the efficiency and quality of simulation-driven design optimization, metamodel-based design and optimization (MBDO) technologies have been widely employed. In this paper, a novel dual-sampling based Co-Kriging method, notated as DS-CoKriging, is proposed to effectively solve the expensive design optimization problems with multi-fidelity simulation models. In DS-CoKriging, expensive data from high-fidelity simulation models are integrated with the cheap ones from low-fidelity simulation models to create an accurate Co-Kriging metamodel with moderate cost, and the Co-Kriging metamodel is gradually updated by sequentially sampling based on a dual-sampling approach during the optimization. Different from expected improvement (EI) criterion oriented sampling approach, the proposed dual-sampling approach consists of two sub-sampling processes, i.e., trust region based sampling and mean square error (MSE) prediction based sampling, to balance the global exploration and local exploitation effectively. The procedure of DS-CoKriging and the algorithm of dual-sampling approach are first presented. Then a numerical benchmark problem is used to demonstrate the merits of the proposed method compared with EI criterion based Co-Kriging method. Finally, DS-CoKriging is applied in an all-electric propulsion geostationary Earth orbit (GEO) transfer design optimization problem. The results show that the total transfer time is successfully reduced by 12 days after optimization. Moreover, DS-CoKriging method significantly reduces the computational cost by 43.6% compared with that of simply optimizing the expensive high-fidelity simulation model, which illustrates the effectiveness and practicality of the proposed DS-CoKriging in solving real-world engineering design optimization problems.
AB - To improve the efficiency and quality of simulation-driven design optimization, metamodel-based design and optimization (MBDO) technologies have been widely employed. In this paper, a novel dual-sampling based Co-Kriging method, notated as DS-CoKriging, is proposed to effectively solve the expensive design optimization problems with multi-fidelity simulation models. In DS-CoKriging, expensive data from high-fidelity simulation models are integrated with the cheap ones from low-fidelity simulation models to create an accurate Co-Kriging metamodel with moderate cost, and the Co-Kriging metamodel is gradually updated by sequentially sampling based on a dual-sampling approach during the optimization. Different from expected improvement (EI) criterion oriented sampling approach, the proposed dual-sampling approach consists of two sub-sampling processes, i.e., trust region based sampling and mean square error (MSE) prediction based sampling, to balance the global exploration and local exploitation effectively. The procedure of DS-CoKriging and the algorithm of dual-sampling approach are first presented. Then a numerical benchmark problem is used to demonstrate the merits of the proposed method compared with EI criterion based Co-Kriging method. Finally, DS-CoKriging is applied in an all-electric propulsion geostationary Earth orbit (GEO) transfer design optimization problem. The results show that the total transfer time is successfully reduced by 12 days after optimization. Moreover, DS-CoKriging method significantly reduces the computational cost by 43.6% compared with that of simply optimizing the expensive high-fidelity simulation model, which illustrates the effectiveness and practicality of the proposed DS-CoKriging in solving real-world engineering design optimization problems.
UR - http://www.scopus.com/inward/record.url?scp=85051622205&partnerID=8YFLogxK
U2 - 10.2514/6.2018-3747
DO - 10.2514/6.2018-3747
M3 - Conference contribution
AN - SCOPUS:85051622205
SN - 9781624105500
T3 - 2018 Multidisciplinary Analysis and Optimization Conference
BT - 2018 Multidisciplinary Analysis and Optimization Conference
PB - American Institute of Aeronautics and Astronautics Inc, AIAA
T2 - 19th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference, 2018
Y2 - 25 June 2018 through 29 June 2018
ER -