A conservative multi-fidelity surrogate model-based robust optimization method for simulation-based optimization

被引:9
|
作者
Hu, Jiexiang [1 ]
Zhang, Lili [2 ]
Lin, Quan [1 ]
Cheng, Meng [2 ]
Zhou, Qi [1 ]
Liu, Huaping [1 ]
机构
[1] Huazhong Univ Sci Technol, Sch Aerosp Engn, Wuhan 430074, Peoples R China
[2] Huazhong Univ Sci Technol, Sch Mech Sci & Engn, Wuhan 430074, Peoples R China
基金
中国博士后科学基金; 中国国家自然科学基金;
关键词
Multi-fidelity surrogate model; Robust optimization; Conservative surrogate model; Simulation-based optimization; Interval uncertainty; DESIGN; UNCERTAINTY; BOOTSTRAP;
D O I
10.1007/s00158-021-03007-w
中图分类号
TP39 [计算机的应用];
学科分类号
081203 ; 0835 ;
摘要
Multi-fidelity (MF) surrogate model-based robust optimization has been used to deal with engineering design and optimization problems that have uncertainty in their inputs. However, the MF surrogate model constructed by a limited number of samples ineluctable has prediction uncertainty, which often leads to the optimal solutions becoming infeasible. In this paper, a MF surrogate model-assisted semi-nested variable adjustment robust optimization (CMF-SN-VARO) method is proposed to address the impact of prediction uncertainty of the MF surrogate model during the optimization process. A piecewise conservative MF surrogate modeling method is proposed to replace the objective functions and constraints, in which the safety margin is calculated by different error metrics according to their performance in problems with different dimensions. The variable adjustment robust optimization (VARO) framework is adopted to solve the robust optimization problem by adjusting the preexisting design. A switch criterion is utilized to adaptively determine when to use surrogate models or inner optimization problems to evaluate the robustness index of design alternatives. The performance of the proposed method is illustrated with an analytical example, a torque arm design problem, and a micro aerial vehicle fuselage design problem. Results show that the proposed method achieves better optimal design solutions that are both objective robust and feasibility robust.
引用
收藏
页码:2525 / 2551
页数:27
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