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Uncertainty Quantification in Surrogate Models Based 
on Pattern Classification of Cross-validation Errors 
Jie Zhang*, Souma Chowdhury*, Ali Mehmani# and Achille Messac# 
* Rensselaer Polytechnic Institute, Department of Mechanical, Aerospace, and Nuclear Engineering 
# Syracuse University, Department of Mechanical and Aerospace Engineering 
14th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference 
September 17 – 19, 2012 
Indianapolis, Indiana
Uncertainty in Surrogate Modeling 
• Since a surrogate model is an approximation to an unknown 
function, prediction errors are generally present in the 
estimated function values. 
• The two major sources of uncertainty in surrogate modeling 
are: 
• Uncertainty in the observations (when they are noisy), and 
• Uncertainty due to finite sample. 
• One of the major challenges in surrogate modeling is to 
accurately quantify these uncertainties. 
2
Research Question 
3 
Domain 
Segmentation 
based on 
Uncertainty in 
the Surrogate 
Can we segregate the input space of a 
surrogate, based on the accuracy of the 
surrogate in different regions, and 
characterize the uncertainty in each 
region? 
• By addressing this question, we can: 
Quantify the uncertainty in the surrogate, which is 
applicable to a majority of surrogate models.
Research Motivation 
 Surrogate model can be used with more confidence if 
we can do two things: 
 Quantify the uncertainty in the surrogate model; and 
 Characterize how the levels of errors vary in the variable 
space. 
 Most existing methods to model the uncertainty in 
surrogate are model-dependent. 
4
Research Questions: Corollary Objectives 
5 
 The research question calls for a methodology to enhance 
user confidence in surrogate applications. 
• Develop a methodology to characterize the uncertainty 
attributable to surrogate models, which is applicable to 
both regression and interpolative surrogate models. 
• Evaluate the performance of leave-one-out cross-validation 
errors as local error measures.
Why Domain Segmentation? 
 In surrogate-based optimization: optimal solutions in regions with smaller 
errors are more reliable than solutions in regions with larger errors. The 
domain segmentation technique can quantify the uncertainty in the optimal 
solutions based on their locations in the design space. 
Wind Farm Layout Optimization 
 In surrogate-based system analysis: the knowledge of the errors and 
uncertainties in the surrogate is helpful for decision making by the 
user/engineer. 
Wind Farm Cost Model 
 In surrogate accuracy improvement: the design-domain-based uncertainty 
6 
information can be used to implement adaptive sampling strategies.
Presentation Outline 
 Uncertainty in surrogate overview 
 Domain Segmentation based on Uncertainty in the Surrogate 
(DSUS) 
 Illustrating cross-validation errors as local error measures 
 Applications to wind resource assessment and wind farm 
cost modeling 
 Concluding remarks 
7
Uncertainty in Surrogate Review 
8 
 Uncertainty in Surrogates 
 Bayesian approach (Kennedy and O’Hagan, Apley et al., Xiong et al.) 
 Adding bias using constant or pointwise margins (Picheny) 
 Reliability Based Design Optimization (RBDO) (Neufeld et al.) 
 Efficient Global Optimization (EGO) (Jones et al.) 
 Sequential Kriging Optimization (SKO) (Huang et al.) 
 Importation of uncertainty estimates from one surrogate to another 
(Viana and Haftka)
Domain Segmentation based on Uncertainty in the Surrogate (DSUS) 
9 
• Based on the current level of 
knowledge regarding the problem, 
the engineer may know what 
levels of errors are acceptable for 
particular design purposes. 
Wind Farm Power Generation Model 
Error Decision 
< 5% error Desirable 
5-10% error Acceptable 
> 10% error Unacceptable 
• The engineer can estimate the 
confidence of a new design, based on 
the region into which the design 
point is classified. 
• These regions can correspond to 
“good”, “acceptable”, and 
“unacceptable” levels of accuracy.
Development of the DSUS 
10 
DSUS Key features: 
 Segregates the design domain into 
regions based on the level of errors 
(or level of fidelity). 
 Classifies any new point/design, 
for which the actual functional 
response is not known, into an 
error class, and quantify the 
uncertainty in its predicted 
function response. 
 Is readily applicable to a majority 
of interpolative surrogate models. 
The term "prediction uncertainty" denotes the 
distribution of errors of the surrogate.
Cross-Validation 
 Two popular strategies: (i) leave-one-out; and (ii) q-fold. 
 In order to obtain the error at each training point, the leave-one- 
out strategy is adopted in the DSUS framework. 
 The Relative Accuracy Error (RAE) is used to classify the 
training points into classes. 
11 
Actual 
function value 
Estimated value 
by surrogate
Classifying the Training Points into Error Classes 
• According to the RAE values, we classify the training points into error 
classes, and define the lower and upper bounds of each class. 
12 
Class Design variable RAE 
1 0.573 0.018 
2 0.277 0.691 
1 0.044 0.045 
1 0.371 0.018 
2 0.910 0.345 
2 0.767 0.116 
1 0.720 0.043 
1 0.865 0.060 
1 0.508 0.073 
2 0.637 0.316 
2 0.977 1.078 
1 0.240 0.013 
1 0.184 0.019 
1 0.107 0.004 
1 0.453 0.049 
Class 1 
RAE < 10% 
Class 2 
RAE > 10%
Pattern Classification 
 A wide variety of pattern classification methods are available: 
 Linear discriminant analysis (LDA); 
 Principal components analysis (PCA); 
 Kernel estimation and K-nearest-neighbor algorithms; 
 Perceptrons; 
 Neural Network; and 
 Support Vector Machine (SVM) 1,2. 
a competitive approach for multiclass 
13 
classification problem 
1. Basudhar and Missoum; 2. Sakalkar and Hajela
Support Vector Machine (SVM) 
 Four kernels are popularly used: 
 Linear: 
 Polynomial: 
 Radial basis function: 
 Sigmoid: 
14 
We have used an efficient SVM package, LIBSVM (A 
Library for Support Vector Machines), developed by Chang 
and Lin. 
One-against-one 
classification
Classifying New Designs 
15
Adaptive Hybrid Functions (AHF) 
 Determination of a trust region: 
numerical bounds of the estimated 
parameter (output) as functions of 
the independent parameters (input). 
 Definition of a local measure of 
accuracy (using kernel functions) of 
the estimated function value, and 
representation of the corresponding 
distribution parameters as functions 
of the input vector. 
 Weighted summation of different 
surrogate models based on the local 
measure of accuracy. 
16
Illustrating Cross-validation Errors as Local Error Measures 
17 
 The local errors of the surrogate are evaluated in the neighborhood of each 
training point. 
 A local hypercube is constructed to include one training point. 
 The length of the hypercube along each dimension is determined by 
 The jth hypercube can be expressed by
Illustrating Cross-validation Errors as Local Error Measures 
18 
 The RAE at each test point within the jth local hypercube is given by 
 For the jth local hypercube, the average of the RAE values for points is given by 
The local errors estimated by the leave-one-out surrogate at each 
training point are compared with the RAEte 
value estimated within the 
local hypercube.
Analytical Examples 
19 
 Three analytical examples are tested. 
 The 1-variable function; 
 The 2-variable Dixon & Price function; and 
 The 2-variable Booth function. 
 The leave-one-out cross-validation errors and the actual local errors 
in the local hypercube are specified as 
Percentage Error w.r.t the mean error in the entire 
domain 
Class 1 <50% 
Class 2 50-100 % 
Class 3 100-150% 
Class 4 >150%
Analytical Examples 
20 
 Three analytical examples are tested. 
 The 1-variable function; 
 The 2-variable Dixon & Price function; and 
 The 2-variable Booth function. 
Leave-one-out 
Cross-validation 
Local hypercube
Results of Local Error Measures 
21 
1-variable function 
 The cross-validation errors and the actual local errors belong to the 
same class for 99.33% of the 15 training points.
Results of Local Error Measures 
22 
Dixon & Price function 
Actual local errors (local hypercube) Cross-validation errors 
 The cross-validation errors and the actual local errors belong to the 
same class for 83.33% of the 30 training points.
Results of Local Error Measures 
23 
Booth function 
Actual local errors (local hypercube) Cross-validation errors 
 The cross-validation errors and the actual local errors belong to the 
same class for 86.67% of the 30 training points.
Wind Energy Case Studies 
 We apply the DSUS framework to key aspects of wind resource assessment 
and wind farm cost modeling. 
 Onshore wind farm cost model; and 
 Wind Power Potential (WPP) model. 
24 
 Response Surface-Based Wind Farm Cost (RS-WFC) model 
 The inputs for the surrogate model are 
 The number, and 
 The rated power of wind turbines. 
 The output of the surrogate model is 
 Total annual cost of a wind farm 
Surrogate:
Wind Power Potential (WPP) 
 The WPP method predicts the quality of wind resources by considering 
the joint distribution of wind speed and wind direction, which can help 
decision makers in wind farm siting. The key steps include: 
1. Determining distribution type and parameters; and The 5-parameter 
bivariate normal distribution is adopted. 
2. Sampling the five distribution parameters; 
3. Maximizing the net power generation through farm layout optimization 
for each sample distribution; and 
4. A surrogate model is constructed to represent the computed maximum 
capacity factor as a function of the parameters of the bivariate normal 
distribution. 
 The uncertainty in the WPP is characterized for two cases: 
 Evaluating the WPP for a four-turbine farm; and 
 Evaluating the WPP for a nine-turbine farm 
25
SVM Kernels and Predefined Classes Bounds 
26 
Numerical setup for test problems 
The uncertainty scale in each class
Representation of Prediction Uncertainty 
• Gaussian distribution is adopted to represent the uncertainty in the 
prediction accuracy of the surrogate. 
• For any new point (design) candidate, the DSUS framework can classify 
that point into one of these error classes. 
27 
Wind farm cost model
Uncertainty Prediction Results 
28 
Classification accuracy of each problem 
Problem Parameters Accuracy 
Wind farm cost C=1, γ=0.8 100% (20/20) 
WPP (4 turbines) C=1, γ=1 90% (18/20) 
WPP (9 turbines) C=1, γ=0.2 95% (19/20) 
• The classification accuracy of the DSUS prediction is more than 90% for 
all problems.
Uncertainty Prediction Results 
29 
Uncertainty characterization for new designs (wind farm cost) 
New design No. of turbines Rated 
Power 
Class Uncertainty (μ, σ) 
1 40 1.25 MW 1 0.0018, 0.0011 
2 7 1 MW 2 0.0066, 0.0013 
3 44 1.5 MW 3 0.0216, 0.0102 
 The total annual cost per kilowatt installed (for the thisd wind farm) is 
estimated as 122.28 $/kW. 
 Assuming a lifetime of 20 years, the 2.16% (mean value) error in the cost 
estimation is approximately 3.5 million dollars, which is an appreciable 
value for such a medium scale wind farm.
Uncertainty in The Wind Power Potential 
30 
Uncertainty in the estimated capacity factors 
 For the Ada station, the capacity factor is estimated as 48.52% for the 9- 
turbine farm. 
 The 53.74% (mean value) error in the capacity factor estimation results in 
approximately 3×107 kWh annual energy production, which is significant 
for such a small scale wind farm.
Uncertainty in The Wind Power Potential 
31 
WPP with 4 turbines WPP with 9 turbines
Concluding Remarks 
• The Domain Segmentation based on Uncertainty in the Surrogate 
(DSUS) framework could successfully characterize the uncertainty 
attributable to surrogate models. 
• The mean errors in the wind farm cost and wind power potential 
(in the case studies) are significant for small/medium scale wind 
farms, which should be carefully considered during the decision 
making process. 
• The results show that the leave-one-out cross-validation error can 
capture the local errors of a surrogate with a reasonable accuracy. 
• Future research should investigate other error metrics that better 
represent the performance over the entire design domain 
32
Acknowledgement 
• I would like to acknowledge my research adviser 
Prof. Achille Messac, for his immense help and 
support in this research. 
• I would also like to thank my colleagues Souma 
Chowdhury and Ali Mehmani for their valuable 
contributions to this paper. 
• Support from the NSF Awards is also 
acknowledged. 
33
Selected References 
1. Keane, A. J. and Nair, P. B., Computational Approaches for Aerospace Design: The Pursuit of Excellence, John Wiley and Sons, 
2005. 
2. Basudhar, A. and Missoum, S., “Adaptive Explicit Decision Functions for Probabilistic Design and Optimization Using Support 
Vector Machines,” Computers and Structures, Vol. 86, No. 19-20, 2008, pp. 1904–1917. 
3. Forrester, A. and Keane, A., “Recent Advances in Surrogate-based Optimization,” Progress in Aerospace Sciences, Vol. 45, No. 
1-3, 2009, pp. 50–79. 
4. Wang, G. and Shan, S., “Review of Metamodeling Techniques in Support of Engineering Design Optimization,” Journal of 
Mechanical Design, Vol. 129, No. 4, 2007, pp. 370–380. 
5. Simpson, T., Toropov, V., Balabanov, V., , and Viana, F., “Design and Analysis of Computer Experiments in Multidisciplinary 
Design Optimization: A Review of How Far We Have Come or Not,” 12th AIAA/ISSMO Multidisciplinary Analysis and 
Optimization Conference, Victoria, Canada, September 10-12 2008. 
6. Zhang, J., Chowdhury, S., and Messac, A., “An Adaptive Hybrid Surrogate Model,” Structural and Multidisciplinary 
Optimization, 2012, doi: 10.1007/s00158-012-0764-x. 
7. Forrester, A., Sobester, A., and Keane, A., Engineering Design via Surrogate Modelling: A Practical Guide, Wiley, 2008. 
8. Apley, D. W., Liu, J., and Chen, W., “Understanding the Effects of Model Uncertainty in Robust Design With Computer 
Experiments,” ASME Journal of Mechanical Design, Vol. 128, No. 4, 2006, pp. 945(14 pages). 
9. Neufeld, D. and an J. Chung, K. B., “Aircraft Wing Box Optimization Considering Uncertainty in Surrogate Models,” Structural 
and Multidisciplinary Optimization, Vol. 42, No. 5, 2010, pp. 745–753. 
10. Viana, F. A. C. and Haftka, R. T., “Importing Uncertainty Estimates from One Surrogate to Another,” 50th 
AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, Palm Springs, California, May 4-6 
2009. 
34

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DSUS_MAO_2012_Jie

  • 1. Uncertainty Quantification in Surrogate Models Based on Pattern Classification of Cross-validation Errors Jie Zhang*, Souma Chowdhury*, Ali Mehmani# and Achille Messac# * Rensselaer Polytechnic Institute, Department of Mechanical, Aerospace, and Nuclear Engineering # Syracuse University, Department of Mechanical and Aerospace Engineering 14th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference September 17 – 19, 2012 Indianapolis, Indiana
  • 2. Uncertainty in Surrogate Modeling • Since a surrogate model is an approximation to an unknown function, prediction errors are generally present in the estimated function values. • The two major sources of uncertainty in surrogate modeling are: • Uncertainty in the observations (when they are noisy), and • Uncertainty due to finite sample. • One of the major challenges in surrogate modeling is to accurately quantify these uncertainties. 2
  • 3. Research Question 3 Domain Segmentation based on Uncertainty in the Surrogate Can we segregate the input space of a surrogate, based on the accuracy of the surrogate in different regions, and characterize the uncertainty in each region? • By addressing this question, we can: Quantify the uncertainty in the surrogate, which is applicable to a majority of surrogate models.
  • 4. Research Motivation  Surrogate model can be used with more confidence if we can do two things:  Quantify the uncertainty in the surrogate model; and  Characterize how the levels of errors vary in the variable space.  Most existing methods to model the uncertainty in surrogate are model-dependent. 4
  • 5. Research Questions: Corollary Objectives 5  The research question calls for a methodology to enhance user confidence in surrogate applications. • Develop a methodology to characterize the uncertainty attributable to surrogate models, which is applicable to both regression and interpolative surrogate models. • Evaluate the performance of leave-one-out cross-validation errors as local error measures.
  • 6. Why Domain Segmentation?  In surrogate-based optimization: optimal solutions in regions with smaller errors are more reliable than solutions in regions with larger errors. The domain segmentation technique can quantify the uncertainty in the optimal solutions based on their locations in the design space. Wind Farm Layout Optimization  In surrogate-based system analysis: the knowledge of the errors and uncertainties in the surrogate is helpful for decision making by the user/engineer. Wind Farm Cost Model  In surrogate accuracy improvement: the design-domain-based uncertainty 6 information can be used to implement adaptive sampling strategies.
  • 7. Presentation Outline  Uncertainty in surrogate overview  Domain Segmentation based on Uncertainty in the Surrogate (DSUS)  Illustrating cross-validation errors as local error measures  Applications to wind resource assessment and wind farm cost modeling  Concluding remarks 7
  • 8. Uncertainty in Surrogate Review 8  Uncertainty in Surrogates  Bayesian approach (Kennedy and O’Hagan, Apley et al., Xiong et al.)  Adding bias using constant or pointwise margins (Picheny)  Reliability Based Design Optimization (RBDO) (Neufeld et al.)  Efficient Global Optimization (EGO) (Jones et al.)  Sequential Kriging Optimization (SKO) (Huang et al.)  Importation of uncertainty estimates from one surrogate to another (Viana and Haftka)
  • 9. Domain Segmentation based on Uncertainty in the Surrogate (DSUS) 9 • Based on the current level of knowledge regarding the problem, the engineer may know what levels of errors are acceptable for particular design purposes. Wind Farm Power Generation Model Error Decision < 5% error Desirable 5-10% error Acceptable > 10% error Unacceptable • The engineer can estimate the confidence of a new design, based on the region into which the design point is classified. • These regions can correspond to “good”, “acceptable”, and “unacceptable” levels of accuracy.
  • 10. Development of the DSUS 10 DSUS Key features:  Segregates the design domain into regions based on the level of errors (or level of fidelity).  Classifies any new point/design, for which the actual functional response is not known, into an error class, and quantify the uncertainty in its predicted function response.  Is readily applicable to a majority of interpolative surrogate models. The term "prediction uncertainty" denotes the distribution of errors of the surrogate.
  • 11. Cross-Validation  Two popular strategies: (i) leave-one-out; and (ii) q-fold.  In order to obtain the error at each training point, the leave-one- out strategy is adopted in the DSUS framework.  The Relative Accuracy Error (RAE) is used to classify the training points into classes. 11 Actual function value Estimated value by surrogate
  • 12. Classifying the Training Points into Error Classes • According to the RAE values, we classify the training points into error classes, and define the lower and upper bounds of each class. 12 Class Design variable RAE 1 0.573 0.018 2 0.277 0.691 1 0.044 0.045 1 0.371 0.018 2 0.910 0.345 2 0.767 0.116 1 0.720 0.043 1 0.865 0.060 1 0.508 0.073 2 0.637 0.316 2 0.977 1.078 1 0.240 0.013 1 0.184 0.019 1 0.107 0.004 1 0.453 0.049 Class 1 RAE < 10% Class 2 RAE > 10%
  • 13. Pattern Classification  A wide variety of pattern classification methods are available:  Linear discriminant analysis (LDA);  Principal components analysis (PCA);  Kernel estimation and K-nearest-neighbor algorithms;  Perceptrons;  Neural Network; and  Support Vector Machine (SVM) 1,2. a competitive approach for multiclass 13 classification problem 1. Basudhar and Missoum; 2. Sakalkar and Hajela
  • 14. Support Vector Machine (SVM)  Four kernels are popularly used:  Linear:  Polynomial:  Radial basis function:  Sigmoid: 14 We have used an efficient SVM package, LIBSVM (A Library for Support Vector Machines), developed by Chang and Lin. One-against-one classification
  • 16. Adaptive Hybrid Functions (AHF)  Determination of a trust region: numerical bounds of the estimated parameter (output) as functions of the independent parameters (input).  Definition of a local measure of accuracy (using kernel functions) of the estimated function value, and representation of the corresponding distribution parameters as functions of the input vector.  Weighted summation of different surrogate models based on the local measure of accuracy. 16
  • 17. Illustrating Cross-validation Errors as Local Error Measures 17  The local errors of the surrogate are evaluated in the neighborhood of each training point.  A local hypercube is constructed to include one training point.  The length of the hypercube along each dimension is determined by  The jth hypercube can be expressed by
  • 18. Illustrating Cross-validation Errors as Local Error Measures 18  The RAE at each test point within the jth local hypercube is given by  For the jth local hypercube, the average of the RAE values for points is given by The local errors estimated by the leave-one-out surrogate at each training point are compared with the RAEte value estimated within the local hypercube.
  • 19. Analytical Examples 19  Three analytical examples are tested.  The 1-variable function;  The 2-variable Dixon & Price function; and  The 2-variable Booth function.  The leave-one-out cross-validation errors and the actual local errors in the local hypercube are specified as Percentage Error w.r.t the mean error in the entire domain Class 1 <50% Class 2 50-100 % Class 3 100-150% Class 4 >150%
  • 20. Analytical Examples 20  Three analytical examples are tested.  The 1-variable function;  The 2-variable Dixon & Price function; and  The 2-variable Booth function. Leave-one-out Cross-validation Local hypercube
  • 21. Results of Local Error Measures 21 1-variable function  The cross-validation errors and the actual local errors belong to the same class for 99.33% of the 15 training points.
  • 22. Results of Local Error Measures 22 Dixon & Price function Actual local errors (local hypercube) Cross-validation errors  The cross-validation errors and the actual local errors belong to the same class for 83.33% of the 30 training points.
  • 23. Results of Local Error Measures 23 Booth function Actual local errors (local hypercube) Cross-validation errors  The cross-validation errors and the actual local errors belong to the same class for 86.67% of the 30 training points.
  • 24. Wind Energy Case Studies  We apply the DSUS framework to key aspects of wind resource assessment and wind farm cost modeling.  Onshore wind farm cost model; and  Wind Power Potential (WPP) model. 24  Response Surface-Based Wind Farm Cost (RS-WFC) model  The inputs for the surrogate model are  The number, and  The rated power of wind turbines.  The output of the surrogate model is  Total annual cost of a wind farm Surrogate:
  • 25. Wind Power Potential (WPP)  The WPP method predicts the quality of wind resources by considering the joint distribution of wind speed and wind direction, which can help decision makers in wind farm siting. The key steps include: 1. Determining distribution type and parameters; and The 5-parameter bivariate normal distribution is adopted. 2. Sampling the five distribution parameters; 3. Maximizing the net power generation through farm layout optimization for each sample distribution; and 4. A surrogate model is constructed to represent the computed maximum capacity factor as a function of the parameters of the bivariate normal distribution.  The uncertainty in the WPP is characterized for two cases:  Evaluating the WPP for a four-turbine farm; and  Evaluating the WPP for a nine-turbine farm 25
  • 26. SVM Kernels and Predefined Classes Bounds 26 Numerical setup for test problems The uncertainty scale in each class
  • 27. Representation of Prediction Uncertainty • Gaussian distribution is adopted to represent the uncertainty in the prediction accuracy of the surrogate. • For any new point (design) candidate, the DSUS framework can classify that point into one of these error classes. 27 Wind farm cost model
  • 28. Uncertainty Prediction Results 28 Classification accuracy of each problem Problem Parameters Accuracy Wind farm cost C=1, γ=0.8 100% (20/20) WPP (4 turbines) C=1, γ=1 90% (18/20) WPP (9 turbines) C=1, γ=0.2 95% (19/20) • The classification accuracy of the DSUS prediction is more than 90% for all problems.
  • 29. Uncertainty Prediction Results 29 Uncertainty characterization for new designs (wind farm cost) New design No. of turbines Rated Power Class Uncertainty (μ, σ) 1 40 1.25 MW 1 0.0018, 0.0011 2 7 1 MW 2 0.0066, 0.0013 3 44 1.5 MW 3 0.0216, 0.0102  The total annual cost per kilowatt installed (for the thisd wind farm) is estimated as 122.28 $/kW.  Assuming a lifetime of 20 years, the 2.16% (mean value) error in the cost estimation is approximately 3.5 million dollars, which is an appreciable value for such a medium scale wind farm.
  • 30. Uncertainty in The Wind Power Potential 30 Uncertainty in the estimated capacity factors  For the Ada station, the capacity factor is estimated as 48.52% for the 9- turbine farm.  The 53.74% (mean value) error in the capacity factor estimation results in approximately 3×107 kWh annual energy production, which is significant for such a small scale wind farm.
  • 31. Uncertainty in The Wind Power Potential 31 WPP with 4 turbines WPP with 9 turbines
  • 32. Concluding Remarks • The Domain Segmentation based on Uncertainty in the Surrogate (DSUS) framework could successfully characterize the uncertainty attributable to surrogate models. • The mean errors in the wind farm cost and wind power potential (in the case studies) are significant for small/medium scale wind farms, which should be carefully considered during the decision making process. • The results show that the leave-one-out cross-validation error can capture the local errors of a surrogate with a reasonable accuracy. • Future research should investigate other error metrics that better represent the performance over the entire design domain 32
  • 33. Acknowledgement • I would like to acknowledge my research adviser Prof. Achille Messac, for his immense help and support in this research. • I would also like to thank my colleagues Souma Chowdhury and Ali Mehmani for their valuable contributions to this paper. • Support from the NSF Awards is also acknowledged. 33
  • 34. Selected References 1. Keane, A. J. and Nair, P. B., Computational Approaches for Aerospace Design: The Pursuit of Excellence, John Wiley and Sons, 2005. 2. Basudhar, A. and Missoum, S., “Adaptive Explicit Decision Functions for Probabilistic Design and Optimization Using Support Vector Machines,” Computers and Structures, Vol. 86, No. 19-20, 2008, pp. 1904–1917. 3. Forrester, A. and Keane, A., “Recent Advances in Surrogate-based Optimization,” Progress in Aerospace Sciences, Vol. 45, No. 1-3, 2009, pp. 50–79. 4. Wang, G. and Shan, S., “Review of Metamodeling Techniques in Support of Engineering Design Optimization,” Journal of Mechanical Design, Vol. 129, No. 4, 2007, pp. 370–380. 5. Simpson, T., Toropov, V., Balabanov, V., , and Viana, F., “Design and Analysis of Computer Experiments in Multidisciplinary Design Optimization: A Review of How Far We Have Come or Not,” 12th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference, Victoria, Canada, September 10-12 2008. 6. Zhang, J., Chowdhury, S., and Messac, A., “An Adaptive Hybrid Surrogate Model,” Structural and Multidisciplinary Optimization, 2012, doi: 10.1007/s00158-012-0764-x. 7. Forrester, A., Sobester, A., and Keane, A., Engineering Design via Surrogate Modelling: A Practical Guide, Wiley, 2008. 8. Apley, D. W., Liu, J., and Chen, W., “Understanding the Effects of Model Uncertainty in Robust Design With Computer Experiments,” ASME Journal of Mechanical Design, Vol. 128, No. 4, 2006, pp. 945(14 pages). 9. Neufeld, D. and an J. Chung, K. B., “Aircraft Wing Box Optimization Considering Uncertainty in Surrogate Models,” Structural and Multidisciplinary Optimization, Vol. 42, No. 5, 2010, pp. 745–753. 10. Viana, F. A. C. and Haftka, R. T., “Importing Uncertainty Estimates from One Surrogate to Another,” 50th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, Palm Springs, California, May 4-6 2009. 34

Notes de l'éditeur

  1. In the literature, there are different surrogate models, such as Kriging, RBF and E-RBF. Can we adaptively combine the advantages of different surrogate models into one single hybrid surrogate, which provides more accurate estimation? Can we segregate the input space of a surrogate based on the accuracy of the surrogate in different regions? The power that can be generated by a wind farm is much less than the available wind resource at the farm site. How to assess the maximum wind power generation of a wind farm at a farm site, based on the recorded wind data, and planned wind farm capacity?