Optimizations Under Uncertainty Using Gradients, Hessians, and Surrogate Models
Author:
Affiliation:
1. Department of Mechanical and Aerospace Engineering, University of Dayton, Ohio 45469-0238
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.J051847
Reference54 articles.
1. Uncertainty in Computational Aerodynamics
2. GumbertC. R.NewmanP. A.HouG. J. “Effect of Random Geometric Uncertainty on the Computational Design of 3-D Wing,” AIAA Paper 2002-2806, June 2002.
3. Foreword: special issue on robust optimization
4. PilchM.TrucanoT. G.HeltonJ. C. “Ideas Underlying Quantification of Margins and Uncertainties (QMU): A White Paper,” Sandia National Lab. TR SAND2006-5001, 2006.
5. Measures of agreement between computation and experiment: Validation metrics
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