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Published in: Structural and Multidisciplinary Optimization 4/2020

05-12-2019 | Research Paper

Toward the robust establishment of variable-fidelity surrogate models for hierarchical stiffened shells by two-step adaptive updating approach

Authors: Kuo Tian, Zengcong Li, Xiangtao Ma, Haixin Zhao, Jiaxin Zhang, Bo Wang

Published in: Structural and Multidisciplinary Optimization | Issue 4/2020

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Abstract

Since the high-fidelity model (HFM) of hierarchical stiffened shells is time-consuming, the sampling points based on HFM are generally few, which would result in a certain randomness of the sampling process. In some cases, the prediction accuracy of the variable-fidelity surrogate model (VFSM) is prone to be not robust and reliable. In order to improve the robustness of the prediction accuracy of VFSM, a two-step adaptive updating approach is proposed for the robust establishment of VFSM. In the first step, the leave-one-out (LOO) cross validation is carried out for sampling points of the low-fidelity model (LFM), aiming at finding out those with large prediction error. Then, these points are evaluated by HFM and then added into the original HFM set. In the second step, another LOO cross validation is performed on sampling points of the hybrid bridge function linking HFM and LFM. Based on the Voronoi diagram method, new updating points are chosen from where the largest prediction error of the bridge function lies, and then the VFSM is updated. After above two-step updating process, the VFSM is established. Three simple examples of test functions are firstly presented to verify the effectiveness and efficiency of the proposed method. Further, the proposed method is applied to an engineering example of hierarchical stiffened shells. In order to provide evaluation indexes for prediction accuracy and robustness of VFSM, the VFSM is established by multiple times, and the mean value and the standard deviation of the relative root mean square error (RRMSE) values of the multiple sets of VFSM are calculated. Results indicate that, under the similar computational cost, the mean value and the standard deviation of the RRMSE values of the proposed method decrease by 24.1% and 82.0% than those of the traditional VFSM based on the direct sampling method, respectively. Therefore, the high prediction accuracy and robustness of the proposed method is verified. Additionally, the total computational time of the proposed VFSM decreases by 70% than that of the surrogate model based on HFM when achieving the similar prediction accuracy, indicating the high prediction efficiency of the proposed VFSM.

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Appendix
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Literature
go back to reference Ariyarit A, Sugiura M, Tanabe Y et al (2018) Hybrid surrogate-model-based multi-fidelity efficient global optimization applied to helicopter blade design. Eng Optim 50(6):1016–1040MathSciNetCrossRef Ariyarit A, Sugiura M, Tanabe Y et al (2018) Hybrid surrogate-model-based multi-fidelity efficient global optimization applied to helicopter blade design. Eng Optim 50(6):1016–1040MathSciNetCrossRef
go back to reference Aurenhammer F (1991) Voronoi diagrams-a survey of a fundamental geometric data structure. ACM Comput Surv (CSUR) 23(3):345–405CrossRef Aurenhammer F (1991) Voronoi diagrams-a survey of a fundamental geometric data structure. ACM Comput Surv (CSUR) 23(3):345–405CrossRef
go back to reference Chagraoui H, Soula M (2018) Multidisciplinary design optimization of stiffened panels using collaborative optimization and artificial neural network. Proc Inst Mech Eng Part C J Mech Eng Sci 232(20):3595–3611CrossRef Chagraoui H, Soula M (2018) Multidisciplinary design optimization of stiffened panels using collaborative optimization and artificial neural network. Proc Inst Mech Eng Part C J Mech Eng Sci 232(20):3595–3611CrossRef
go back to reference Chen HS, Meng Z, Zhou HL (2018) A hybrid framework of efficient multi-objective optimization of stiffened shells with imperfection. Int J Comput Methods 15(8):1850145MathSciNetCrossRef Chen HS, Meng Z, Zhou HL (2018) A hybrid framework of efficient multi-objective optimization of stiffened shells with imperfection. Int J Comput Methods 15(8):1850145MathSciNetCrossRef
go back to reference Choi DH (2002) Cooperative mutation based evolutionary programming for continuous function optimization. Oper Res Lett 30(3):195–201MathSciNetCrossRef Choi DH (2002) Cooperative mutation based evolutionary programming for continuous function optimization. Oper Res Lett 30(3):195–201MathSciNetCrossRef
go back to reference Forrester AIJ, Sóbester A, Keane AJ (2007) Multi-fidelity optimization via surrogate modelling. Proc Royal Soc A Math Phys Eng Sci 463(2088):3251–3269MathSciNetMATH Forrester AIJ, Sóbester A, Keane AJ (2007) Multi-fidelity optimization via surrogate modelling. Proc Royal Soc A Math Phys Eng Sci 463(2088):3251–3269MathSciNetMATH
go back to reference Gano S, Sanders B, Renaud J 2004. Variable fidelity optimization using a kriging based scaling function. 10th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference: 4460. Gano S, Sanders B, Renaud J 2004. Variable fidelity optimization using a kriging based scaling function. 10th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference: 4460.
go back to reference Ghayoor H, Rouhi M, Hoa SV et al (2017) Use of curvilinear fibers for improved bending-induced buckling capacity of elliptical composite cylinders. Int J Solids Struct 109:112–122CrossRef Ghayoor H, Rouhi M, Hoa SV et al (2017) Use of curvilinear fibers for improved bending-induced buckling capacity of elliptical composite cylinders. Int J Solids Struct 109:112–122CrossRef
go back to reference Giselle Fernández-Godino M, Park C, Kim N H, et al. 2019 Issues in deciding whether to use multifidelity surrogates. AIAA J: 1-16. Giselle Fernández-Godino M, Park C, Kim N H, et al. 2019 Issues in deciding whether to use multifidelity surrogates. AIAA J: 1-16.
go back to reference Han ZH, Görtz S (2012) Hierarchical kriging model for variable-fidelity surrogate modeling. AIAA J 50(9):1885–1896CrossRef Han ZH, Görtz S (2012) Hierarchical kriging model for variable-fidelity surrogate modeling. AIAA J 50(9):1885–1896CrossRef
go back to reference Han Z, Zimmerman R, Görtz S (2012) Alternative cokriging method for variable-fidelity surrogate modeling. AIAA J 50(5):1205–1210CrossRef Han Z, Zimmerman R, Görtz S (2012) Alternative cokriging method for variable-fidelity surrogate modeling. AIAA J 50(5):1205–1210CrossRef
go back to reference Han ZH, Görtz S, Zimmermann R (2013) Improving variable-fidelity surrogate modeling via gradient-enhanced kriging and a generalized hybrid bridge function. Aerosp Sci Technol 25(1):177–189CrossRef Han ZH, Görtz S, Zimmermann R (2013) Improving variable-fidelity surrogate modeling via gradient-enhanced kriging and a generalized hybrid bridge function. Aerosp Sci Technol 25(1):177–189CrossRef
go back to reference Hao P, Wang B, Li G et al (2014) Hybrid optimization of hierarchical stiffened shells based on smeared stiffener method and finite element method. Thin-Walled Struct 82:46–54CrossRef Hao P, Wang B, Li G et al (2014) Hybrid optimization of hierarchical stiffened shells based on smeared stiffener method and finite element method. Thin-Walled Struct 82:46–54CrossRef
go back to reference Jiang S, Sun FF, Fan HL et al (2017) Fabrication and testing of composite orthogrid sandwich cylinder. Compos Sci Technol 142:171–179CrossRef Jiang S, Sun FF, Fan HL et al (2017) Fabrication and testing of composite orthogrid sandwich cylinder. Compos Sci Technol 142:171–179CrossRef
go back to reference Jones DR, Schonlau M, Welch WJ (1998) Efficient global optimization of expensive black-box functions. J Global Optim 13(4):455–492MathSciNetCrossRef Jones DR, Schonlau M, Welch WJ (1998) Efficient global optimization of expensive black-box functions. J Global Optim 13(4):455–492MathSciNetCrossRef
go back to reference Keshtegar B, Hao P (2018) A hybrid descent mean value for accurate and efficient performance measure approach of reliability-based design optimization. Comput Methods Appl Mech Eng 336:237–259MathSciNetCrossRef Keshtegar B, Hao P (2018) A hybrid descent mean value for accurate and efficient performance measure approach of reliability-based design optimization. Comput Methods Appl Mech Eng 336:237–259MathSciNetCrossRef
go back to reference Keshtegar B, Hao P, Wang YT et al (2018) An adaptive response surface method and Gaussian global-best harmony search algorithm for optimization of aircraft stiffened panels. Appl Soft Comput 66:196–207CrossRef Keshtegar B, Hao P, Wang YT et al (2018) An adaptive response surface method and Gaussian global-best harmony search algorithm for optimization of aircraft stiffened panels. Appl Soft Comput 66:196–207CrossRef
go back to reference Li G, Meng Z, Hao P et al (2016) A hybrid reliability-based design optimization approach with adaptive chaos control using kriging model. Int J Comput Methods 13(1):1650006MathSciNetCrossRef Li G, Meng Z, Hao P et al (2016) A hybrid reliability-based design optimization approach with adaptive chaos control using kriging model. Int J Comput Methods 13(1):1650006MathSciNetCrossRef
go back to reference Li M, Sun FF, Lai CL et al (2018) Fabrication and testing of composite hierarchical isogrid stiffened cylinder. Compos Sci Technol 157:152–159CrossRef Li M, Sun FF, Lai CL et al (2018) Fabrication and testing of composite hierarchical isogrid stiffened cylinder. Compos Sci Technol 157:152–159CrossRef
go back to reference Liu N, Yu W, Hodges D H 2018. Mechanics of structure genome-based global buckling analysis of stiffened composite panels. Acta Mech: 1-16. Liu N, Yu W, Hodges D H 2018. Mechanics of structure genome-based global buckling analysis of stiffened composite panels. Acta Mech: 1-16.
go back to reference Molga M, Smutnicki C 2005. Test functions for optimization needs Test functions for optimization needs, 101. Molga M, Smutnicki C 2005. Test functions for optimization needs Test functions for optimization needs, 101.
go back to reference Molina-Cristóbal A, Palmer P R, Skinner B A, et al. 2010 Multi-fidelity simulation modelling in optimization of a submarine propulsion system. 2010 IEEE Vehicle Power and Propulsion Conference. IEEE: 1-6. Molina-Cristóbal A, Palmer P R, Skinner B A, et al. 2010 Multi-fidelity simulation modelling in optimization of a submarine propulsion system. 2010 IEEE Vehicle Power and Propulsion Conference. IEEE: 1-6.
go back to reference Pires EJS, Machado JAT, de Moura OPB et al (2010) Particle swarm optimization with fractional-order velocity. Nonlinear Dyn 61(1-2):295–301CrossRef Pires EJS, Machado JAT, de Moura OPB et al (2010) Particle swarm optimization with fractional-order velocity. Nonlinear Dyn 61(1-2):295–301CrossRef
go back to reference Quinn D, Murphy A, Glazebrook C (2012) Aerospace stiffened panel initial sizing with novel skin sub-stiffening features. Int J Struct Stab Dyn 12(05):1250060CrossRef Quinn D, Murphy A, Glazebrook C (2012) Aerospace stiffened panel initial sizing with novel skin sub-stiffening features. Int J Struct Stab Dyn 12(05):1250060CrossRef
go back to reference Rouhi M, Ghayoor H, Hoa SV et al (2016) Stiffness tailoring of elliptical composite cylinders for axial buckling performance. Compos Struct 150:115–123CrossRef Rouhi M, Ghayoor H, Hoa SV et al (2016) Stiffness tailoring of elliptical composite cylinders for axial buckling performance. Compos Struct 150:115–123CrossRef
go back to reference Shields MD, Zhang JX (2016) The generalization of Latin hypercube sampling. Reliab Eng Syst Saf 148:96–108CrossRef Shields MD, Zhang JX (2016) The generalization of Latin hypercube sampling. Reliab Eng Syst Saf 148:96–108CrossRef
go back to reference Sim CH, Park JS, Kim HI et al (2018a) Postbuckling analyses and derivations of knockdown factors for hybrid-grid stiffened cylinders. Aerosp Sci Technol 82:20–31CrossRef Sim CH, Park JS, Kim HI et al (2018a) Postbuckling analyses and derivations of knockdown factors for hybrid-grid stiffened cylinders. Aerosp Sci Technol 82:20–31CrossRef
go back to reference Sim CH, Kim HI, Lee YL et al (2018b) Derivations of knockdown factors for cylindrical structures considering different initial imperfection models and thickness ratios. Int J Aeronaut Space Sci 19(3):626–635CrossRef Sim CH, Kim HI, Lee YL et al (2018b) Derivations of knockdown factors for cylindrical structures considering different initial imperfection models and thickness ratios. Int J Aeronaut Space Sci 19(3):626–635CrossRef
go back to reference Song X G, Lv L Y, Sun W, et al. 2019 A radial basis function-based multi-fidelity surrogate model: exploring correlation between high-fidelity and low-fidelity models. Struct Multidiscip Optim: 1-17. Song X G, Lv L Y, Sun W, et al. 2019 A radial basis function-based multi-fidelity surrogate model: exploring correlation between high-fidelity and low-fidelity models. Struct Multidiscip Optim: 1-17.
go back to reference Sun FF, Fan HL, Zhou CW et al (2013) Equivalent analysis and failure prediction of quasi-isotropic composite sandwich cylinder with lattice core under uniaxial compression. Compos Struct 101:180–190CrossRef Sun FF, Fan HL, Zhou CW et al (2013) Equivalent analysis and failure prediction of quasi-isotropic composite sandwich cylinder with lattice core under uniaxial compression. Compos Struct 101:180–190CrossRef
go back to reference Tian K, Wang B, Zhang K et al (2018a) Tailoring the optimal load-carrying efficiency of hierarchical stiffened shells by competitive sampling. Thin-Walled Struct 133:216–225CrossRef Tian K, Wang B, Zhang K et al (2018a) Tailoring the optimal load-carrying efficiency of hierarchical stiffened shells by competitive sampling. Thin-Walled Struct 133:216–225CrossRef
go back to reference Tian K, Wang B, Zhou Y, Waas AM (2018b) Proper-orthogonal-decomposition-based buckling analysis and optimization of hybrid fiber composite shells. AIAA J 56(5):1723–1730CrossRef Tian K, Wang B, Zhou Y, Waas AM (2018b) Proper-orthogonal-decomposition-based buckling analysis and optimization of hybrid fiber composite shells. AIAA J 56(5):1723–1730CrossRef
go back to reference Tian K, Wang B, Hao P, Waas AM (2018c) A high-fidelity approximate model for determining lower-bound buckling loads for stiffened shells. Int J Solids Struct 148:14–23CrossRef Tian K, Wang B, Hao P, Waas AM (2018c) A high-fidelity approximate model for determining lower-bound buckling loads for stiffened shells. Int J Solids Struct 148:14–23CrossRef
go back to reference Tyan M, Nguyen NV, Lee JW (2015) Improving variable-fidelity modelling by exploring global design space and radial basis function networks for aerofoil design. Eng Optim 47(7):885–908CrossRef Tyan M, Nguyen NV, Lee JW (2015) Improving variable-fidelity modelling by exploring global design space and radial basis function networks for aerofoil design. Eng Optim 47(7):885–908CrossRef
go back to reference Viana F, Haftka R 2010. Surrogate-based optimization with parallel simulations using the probability of improvement. 13th AIAA/ISSMO Multidisciplinary Analysis Optimization Conference: 9392. Viana F, Haftka R 2010. Surrogate-based optimization with parallel simulations using the probability of improvement. 13th AIAA/ISSMO Multidisciplinary Analysis Optimization Conference: 9392.
go back to reference Vitali R, Haftka RT, Sankar BV (2002) Multi-fidelity design of stiffened composite panel with a crack. Struct Multidiscip Optim 23(5):347–356CrossRef Vitali R, Haftka RT, Sankar BV (2002) Multi-fidelity design of stiffened composite panel with a crack. Struct Multidiscip Optim 23(5):347–356CrossRef
go back to reference Wang B, Hao P, Li G et al (2014) Optimum design of hierarchical stiffened shells for low imperfection sensitivity. Acta Mech Sin 30(3):391–402CrossRef Wang B, Hao P, Li G et al (2014) Optimum design of hierarchical stiffened shells for low imperfection sensitivity. Acta Mech Sin 30(3):391–402CrossRef
go back to reference Wang B, Tian K, Hao P et al (2015) Hybrid analysis and optimization of hierarchical stiffened plates based on asymptotic homogenization method. Compos Struct 132:136–147CrossRef Wang B, Tian K, Hao P et al (2015) Hybrid analysis and optimization of hierarchical stiffened plates based on asymptotic homogenization method. Compos Struct 132:136–147CrossRef
go back to reference Wang B, Tian K, Zhou CH et al (2017a) Grid-pattern optimization framework of novel hierarchical stiffened shells allowing for imperfection sensitivity. Aerosp Sci Technol 62:114–121CrossRef Wang B, Tian K, Zhou CH et al (2017a) Grid-pattern optimization framework of novel hierarchical stiffened shells allowing for imperfection sensitivity. Aerosp Sci Technol 62:114–121CrossRef
go back to reference Wang B, Tian K, Zhao HX et al (2017b) Multilevel optimization framework for hierarchical stiffened shells accelerated by adaptive equivalent strategy. Appl Compos Mater 24(3):575–592CrossRef Wang B, Tian K, Zhao HX et al (2017b) Multilevel optimization framework for hierarchical stiffened shells accelerated by adaptive equivalent strategy. Appl Compos Mater 24(3):575–592CrossRef
go back to reference Wang B, Du KF, Hao P et al (2019) Experimental validation of cylindrical shells under axial compression for improved knockdown factors. Int J Solids Struct 164:37–51CrossRef Wang B, Du KF, Hao P et al (2019) Experimental validation of cylindrical shells under axial compression for improved knockdown factors. Int J Solids Struct 164:37–51CrossRef
go back to reference Wu H, Lai C, Sun F et al (2018) Carbon fiber reinforced hierarchical orthogrid stiffened cylinder: fabrication and testing. Acta Astronaut 145:268–274CrossRef Wu H, Lai C, Sun F et al (2018) Carbon fiber reinforced hierarchical orthogrid stiffened cylinder: fabrication and testing. Acta Astronaut 145:268–274CrossRef
go back to reference Xu G (2013) An adaptive parameter tuning of particle swarm optimization algorithm. Appl Math Comput 219(9):4560–4569MathSciNetMATH Xu G (2013) An adaptive parameter tuning of particle swarm optimization algorithm. Appl Math Comput 219(9):4560–4569MathSciNetMATH
go back to reference Xu YM, Tong Y, Liu M et al (2016) A new effective smeared stiffener method for global buckling analysis of grid stiffened composite panels. Compos Struct 158:83–91CrossRef Xu YM, Tong Y, Liu M et al (2016) A new effective smeared stiffener method for global buckling analysis of grid stiffened composite panels. Compos Struct 158:83–91CrossRef
go back to reference Zhao YN, Chen M, Yang F et al (2017) Optimal design of hierarchical grid-stiffened shells based on linear buckling and nonlinear collapse analyses. Thin-Walled Struct 119:315–323CrossRef Zhao YN, Chen M, Yang F et al (2017) Optimal design of hierarchical grid-stiffened shells based on linear buckling and nonlinear collapse analyses. Thin-Walled Struct 119:315–323CrossRef
go back to reference Zhou Q, Shao X, Jiang P et al (2016a) An active learning metamodeling approach by sequentially exploiting difference information from variable-fidelity models. Adv Eng Inform 30(3):283–297CrossRef Zhou Q, Shao X, Jiang P et al (2016a) An active learning metamodeling approach by sequentially exploiting difference information from variable-fidelity models. Adv Eng Inform 30(3):283–297CrossRef
go back to reference Zhou Q, Shao X, Jiang P et al (2016b) An active learning variable-fidelity metamodelling approach based on ensemble of metamodels and objective-oriented sequential sampling. J Eng Des 27(4-6):205–231CrossRef Zhou Q, Shao X, Jiang P et al (2016b) An active learning variable-fidelity metamodelling approach based on ensemble of metamodels and objective-oriented sequential sampling. J Eng Des 27(4-6):205–231CrossRef
Metadata
Title
Toward the robust establishment of variable-fidelity surrogate models for hierarchical stiffened shells by two-step adaptive updating approach
Authors
Kuo Tian
Zengcong Li
Xiangtao Ma
Haixin Zhao
Jiaxin Zhang
Bo Wang
Publication date
05-12-2019
Publisher
Springer Berlin Heidelberg
Published in
Structural and Multidisciplinary Optimization / Issue 4/2020
Print ISSN: 1615-147X
Electronic ISSN: 1615-1488
DOI
https://doi.org/10.1007/s00158-019-02432-2

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