Surrogate Modeling
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Recent papers in Surrogate Modeling
В настоящее время одним из основных средств уменьшения сроков проектирова- ния и снижения затрат на разработку различных образцов как гражданской, так и военной техни- ки является использование систем автоматизиро- ванного... more
Предоставлены широкие возможности программного комплекса PSE/MACROS автоматиза- ции инженерных расчетов, содержащего современные высокоэффективные алгоритмы опти- мизации, средства интеграции с различными CAD/CAE системами, разнообразные... more
Surrogate models have been widely used in engineering design because of their capability to approximate computationally complex engineering systems. In practice, the choice of surrogate models is extremely important since there are many... more
Metamodel-Assisted Evolution Strategies (MAES) are proposed as a new approach for simulator-based optimization in the domain of Electromagnetic Compatibility (EMC) design. In the given application domain function evaluations tend to be... more
Problem of aircraft structural components (wing, fuselage, tail) optimization is considered. Solution of this problem is very computationally intensive, since it requires at each iteration a twolevel process: first from previous... more
In Japanese. About Construction of Low Dimensional Structures from Object Surface Description using Feature Extraction Techniques, i.e. so-called Effective Dimension Reduction technique to parameterise geometry of an airfoil in order to... more
This work concerns a construction of surrogate models for a specific aerodynamic data base. This data base is generally available from wind tunnel testing or from CFD aerodynamic simulations and contains aerodynamic coefficients for... more
Most control engineering problems are characterized by several objectives, which have to be satisfied simultaneously. Two widely used methods for finding the optimal solution to such problems are aggregating to a single criterion, and... more
The problem of construction of a surrogate model based on available low and highfidelity data is considered. The lowfidelity data can be obtained, e.g., by performing the computer simulation and the highfidelity data can be obtained... more
Problem of aircraft structural components (wing, fuselage, tail) optimization is considered. Solution of this problem is very computationally intensive, since it requires at each iteration a two-level process: first from previous... more