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JOURNALS // Avtomatika i Telemekhanika // Archive

Avtomat. i Telemekh., 2011 Issue 5, Pages 175–182 (Mi at1712)

This article is cited in 3 papers

System Analysis and Operations Research

Applications of kernel ridge estimation to the problem of computing the aerodynamical characteristics of a passenger plane (in comparison with results obtained with artificial neural networks)

A. Ya. Chervonenkisa, S. S. Chernovab, T. V. Zykovac

a Trapeznikov Institute of Control Sciences, Russian Academy of Sciences, Moscow, Russia
b Institute for Systems Analysis, Russian Academy of Sciences, Moscow, Russia
c International Research Institute of Control Problems, Moscow, Russia

Abstract: We show the results of applying the kernel ridge regression method to the problem of fast computation of aerodynamical characteristics of an airplane. We compare our results with the results found with surrogate models constructed with artificial neural networks.

Presented by the member of Editorial Board: A. V. Bernshtein

Received: 25.12.2009


 English version:
Automation and Remote Control, 2011, 72:5, 1061–1067

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