An enhanced variable-fidelity optimization approach for constrained optimization problems and its parallelization

被引:10
作者
Cheng, Ji [1 ,2 ]
Lin, Qiao [3 ]
Yi, Jiaxiang [4 ]
机构
[1] Delft Univ Technol, Fac Aerosp Engn, Delft, Netherlands
[2] Huazhong Univ Sci & Technol, Sch Mech Sci & Engn, Wuhan, Peoples R China
[3] Wuhan Univ Technol, Sch Energy & Power Engn, Wuhan, Peoples R China
[4] Delft Univ Technol, Mat Sci & Engn, Delft, Netherlands
关键词
Variable-fidelity surrogate model; Computationally expensive constrained optimization; Lower confidence bound; Parallel computing; EFFICIENT GLOBAL OPTIMIZATION; SURROGATE-BASED OPTIMIZATION; ENGINEERING OPTIMIZATION; COMPLEX; MODELS; UNCERTAINTY;
D O I
10.1007/s00158-022-03283-0
中图分类号
TP39 [计算机的应用];
学科分类号
081203 ; 0835 ;
摘要
In this paper, a variable-fidelity constrained lower confidence bound (VF-CLCB) criterion is presented for computationally expensive constrained optimization problems (COPs) with two levels of fidelity. In VF-CLCB, the hierarchical Kriging model is adopted to model the objective and inequality constraints. Two infill sampling functions are developed based on the objective and the constraints, respectively, and an adaptive selection strategy is set to select the elite sample points. Moreover, based on the VF-CLCB criterion, a parallel optimization method noted as PVF-CLCB is subsequently developed to accelerate the optimization process. In PVF-CLCB, a VF influence function is defined to approximately evaluate the estimation error of the hierarchical Kriging models, based on which multiple promising points can be determined at each iteration. In addition, an allocation strategy is proposed to distribute the computation resources between the objective- and constraint-oriented functions properly. Lastly, the proposed VF-CLCB and PVF-CLCB approaches are compared with the alternative methods on 12 benchmark numerical cases, and their significant superiority in solving computationally expensive COPs is verified. Furthermore, the proposed methods are employed to optimize the global stability of the stiffened cylindrical shell, and the optimum structure is yielded.
引用
收藏
页数:21
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