Optimization Using Surrogate Objectives on a Helicopter Test Example
Andrew J. Booker, John E. Dennis, Paul D. Frank, David Serafini, Virginia J. Torczon · Birkhäuser Boston eBooks · 1998
This paper presents results for a 31 variable helicopter rotor design example. Results are given for several numerical methods. This is a brief description of a portion of the Boeing/IBM/Rice University collaboration whose purpose is to develop effective numerical methods for managing the use of approximation concepts or response surface methodology in design optimization. These keywords were added by machine and not by the authors. This process is experimental and the keywords may be updated as the learning algorithm improves.