Research on a surrogate model updating-based efficient multi-objective optimization framework for supertall buildings

被引:10
作者
Wang, Zhaoyong [1 ]
Mulyanto, Joshua Adriel [1 ]
Zheng, Chaorong [1 ,2 ]
Wu, Yue [1 ,2 ]
机构
[1] Harbin Inst Technol, Sch Civil Engn, Harbin 150090, Peoples R China
[2] Harbin Inst Technol, Key Lab Struct Dynam Behav & Control, Minist Educ, Harbin 150090, Peoples R China
来源
JOURNAL OF BUILDING ENGINEERING | 2023年 / 72卷
关键词
Multi-objective optimization framework; Efficiency; Surrogate model; Generalized regression neural network; Refinement update; Non-dominated sorting genetic algorithm (NSGA-II); AERODYNAMIC SHAPE OPTIMIZATION; NEURAL-NETWORK; DESIGN; AIRFOIL; PERFORMANCE; ALGORITHM;
D O I
10.1016/j.jobe.2023.106702
中图分类号
TU [建筑科学];
学科分类号
0813 ;
摘要
In order to solve the multi-objective optimization problems of supertall buildings (such as structural design optimization, aerodynamic shape optimization, etc.) with sizable design space more effectively, it is necessary to develop an efficient multi-objective optimization method. Therefore, generalized regression neural network optimized by genetic algorithm (GA-GRNN) based surrogate model was constructed, and a multi-objective optimization framework based on the non-dominated sorting genetic algorithm (NSGA-II) and GA-GRNN surrogate model updating was proposed. The feasibility of multi-objective optimization framework based on surrogate model updating was verified by using the experimental wind pressure data of a supertall building model, and the influencing factors of optimization efficiency were analyzed. The results show that the proposed framework has satisfactory optimization accuracy and efficiency. The optimal sample data set proportional distribution (training set: verification set: test set, i.e., T: V: T) is 7:2:1. With the increase of the total number of sample points in the design space, the optimal proportion of the initial sample points decreases significantly. A thorough consideration of the acquisition time of a single sample value and the optimal proportion of initial sample points is helpful to improve the multi-objective optimization efficiency further. Therefore, for the optimization problems in engineering applications (especially supertall buildings), it is suggested that the reasonable proportion of initial sample points of the surrogate model should be determined according to the acquisition time of a single sample value and the total number of sample points in the design space. The framework is more suitable for complex problems with large total number of sample points in design space and long acquisition time of a single sample value. This study can provide a valuable reference for further research or efficient solution to multi-objective optimization problems in practical engineering applications (such as the optimization problem of supertall buildings).
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页数:20
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共 62 条
  • [1] [Anonymous], 2009, The elements of statistical learning: Data mining, inference, and prediction, DOI [10.1007/978-0-387-84858-714, DOI 10.1007/978-0-387-84858-714]
  • [2] Aerodynamic shape optimization of civil structures: A CFD-enabled Kriging-based approach
    Bernardini, Enrica
    Spence, Seymour M. J.
    Wei, Daniel
    Kareem, Ahsan
    [J]. JOURNAL OF WIND ENGINEERING AND INDUSTRIAL AERODYNAMICS, 2015, 144 : 154 - 164
  • [3] Approach to Aerodynamic Design Through Numerical Optimization
    Buckley, Howard P.
    Zingg, David W.
    [J]. AIAA JOURNAL, 2013, 51 (08) : 1972 - 1981
  • [4] Optimization of expensive black-box problems via Gradient-enhanced Kriging
    Chen, Liming
    Qiu, Haobo
    Gao, Liang
    Jiang, Chen
    Yang, Zan
    [J]. COMPUTER METHODS IN APPLIED MECHANICS AND ENGINEERING, 2020, 362
  • [5] A multi-fidelity surrogate modeling method based on variance-weighted sum for the fusion of multiple non-hierarchical low-fidelity data
    Cheng, Meng
    Jiang, Ping
    Hu, Jiexiang
    Shu, Leshi
    Zhou, Qi
    [J]. STRUCTURAL AND MULTIDISCIPLINARY OPTIMIZATION, 2021, 64 (06) : 3797 - 3818
  • [6] Surrogate model for viscous drag in aircraft empennage conceptual design
    de Lucas, S.
    Vega, J. M.
    Velazquez, A.
    [J]. AEROSPACE SCIENCE AND TECHNOLOGY, 2013, 31 (01) : 99 - 107
  • [7] A multi-fidelity shape optimization via surrogate modeling for civil structures
    Ding, Fei
    Kareem, Ahsan
    [J]. JOURNAL OF WIND ENGINEERING AND INDUSTRIAL AERODYNAMICS, 2018, 178 : 49 - 56
  • [8] RADIAL BASIS FUNCTION NEURAL-NETWORK FOR APPROXIMATION AND ESTIMATION OF NONLINEAR STOCHASTIC DYNAMIC-SYSTEMS
    ELANAYAR, S
    SHIN, YC
    [J]. IEEE TRANSACTIONS ON NEURAL NETWORKS, 1994, 5 (04): : 594 - 603
  • [9] Enhancing wind performance of tall buildings using corner aerodynamic optimization
    Elshaer, Ahmed
    Bitsuamlak, Girma
    El Damatty, Ashraf
    [J]. ENGINEERING STRUCTURES, 2017, 136 : 133 - 148
  • [10] Design of optimal aerodynamic shapes using stochastic optimization methods and computational intelligence
    Giannakoglou, KC
    [J]. PROGRESS IN AEROSPACE SCIENCES, 2002, 38 (01) : 43 - 76