The construction of surrogate models, such as radial basis function (RBF) and Kriging-based surrogates, requires an invertible (square and full rank matrix) or pseudoinvertible (overdetermined) linear system to be solved. This study demonstrates that the method used to solve this linear system may result in up to five orders of magnitude difference in the accuracy of the constructed surrogate model using exactly the same information. Hence, this paper makes the canonic and important point toward reproducible science: the details of solving the linear system when constructing a surrogate model must be communicated. This point is clearly illustrated on a single function, namely the Styblinski–Tang test function by constructing over 200 RBF surrogate models from 128 Latin Hypercubed sampled points. The linear system in the construction of each surrogate model was solved using LU, QR, Cholesky, Singular-Value Decomposition, and the Moore–Penrose pseudoinverse. As we show, the decomposition method influences the utility of the surrogate model, which depends on the application, i.e., whether an accurate approximation of a surrogate is required or whether the ability to optimize the surrogate and capture the optimal design is pertinent. Evidently the selection of the optimal hyperparameters based on the cross validation error also significantly impacts the utility of the constructed surrogate. For our problem, it turns out that selecting the hyperparameters at the lowest cross validation error favors function approximation but adversely affects the ability to optimize the surrogate model. This is demonstrated by optimizing each constructed surrogate model from 16 fixed initial starting points and recording the optimal designs. For our problem, selecting the optimal hyperparameter that coincides with the lowest monotonically decreasing function value significantly improves the ability to optimize the surrogate for most solution strategies.
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July 2019
Research-Article
How We Solve the Weights in Our Surrogate Models Matters
Daniel Correia,
Daniel Correia
1
Center for Asset and Integrity Management,
Department of Mechanical and Aeronautical Engineering,
Pretoria,
e-mail: dan.reia@gmail.com
Department of Mechanical and Aeronautical Engineering,
University of Pretoria
,Pretoria,
South Africa
e-mail: dan.reia@gmail.com
1Corresponding author.
Search for other works by this author on:
Daniel N. Wilke
Daniel N. Wilke
Center for Asset and Integrity Management,
Department of Mechanical and Aeronautical Engineering,
Pretoria,
e-mail: nico.wilke@up.ac.za
Department of Mechanical and Aeronautical Engineering,
University of Pretoria
,Pretoria,
South Africa
e-mail: nico.wilke@up.ac.za
Search for other works by this author on:
Daniel Correia
Center for Asset and Integrity Management,
Department of Mechanical and Aeronautical Engineering,
Pretoria,
e-mail: dan.reia@gmail.com
Department of Mechanical and Aeronautical Engineering,
University of Pretoria
,Pretoria,
South Africa
e-mail: dan.reia@gmail.com
Daniel N. Wilke
Center for Asset and Integrity Management,
Department of Mechanical and Aeronautical Engineering,
Pretoria,
e-mail: nico.wilke@up.ac.za
Department of Mechanical and Aeronautical Engineering,
University of Pretoria
,Pretoria,
South Africa
e-mail: nico.wilke@up.ac.za
1Corresponding author.
Contributed by the Design Automation Committee of ASME for publication in the Journal of Mechanical Design. Manuscript received August 12, 2018; final manuscript received December 29, 2018; published online March 13, 2019. Assoc. Editor: Gary Wang.
J. Mech. Des. Jul 2019, 141(7): 074501 (5 pages)
Published Online: March 13, 2019
Article history
Received:
August 12, 2018
Revision Received:
December 29, 2018
Accepted:
January 1, 2019
Citation
Correia, D., and Wilke, D. N. (March 13, 2019). "How We Solve the Weights in Our Surrogate Models Matters." ASME. J. Mech. Des. July 2019; 141(7): 074501. https://doi.org/10.1115/1.4042622
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