Vestnik Yuzhno-Ural'skogo Universiteta. Seriya Matematicheskoe Modelirovanie i Programmirovanie
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Vestnik Yuzhno-Ural'skogo Universiteta. Seriya Matematicheskoe Modelirovanie i Programmirovanie, 2020, Volume 13, Issue 3, Pages 29–42
DOI: https://doi.org/10.14529/mmp200303
(Mi vyuru555)
 

This article is cited in 1 scientific paper (total in 1 paper)

Programming & Computer Software

Statistical analysis module for weight design of aircraft elements

A. I. Kibzun, A. S. Shalaev, V. M. Azanov, A. N. Ignatov

Moscow Aviation Institute, Moscow, Russian Federation
References:
Abstract: The concept of a statistical analysis module for weight design of aircraft elements (for predicting weight characteristics of one or another aircraft elements) is proposed. Models, methods to construct single-point estimates of the predicted characteristic, quality criteria of constructed models are considered. Two approaches to the confidence estimation of the predicted characteristic are proposed. First approach is based on the assumption that errors at predicting are caused by inaccurate identification of the deterministic part of the predicted characteristic behavior. The second one is based on the assumption that the deterministic part of the predicted characteristic behavior is identified correctly and errors at predicting are caused by inaccuracy in the measurements. The structure, goals of each component of the software package that implements the statistical analysis module is considered in details. Based on the real data the problem of predicting the take-off mass of an empty equipped airliner depending on maximum pay load and the maximum flight distance at maximum pay load is given. By this problem applicability of considered models and methods is demonstrated.
Keywords: weight design, aircraft, statistical analysis, software.
Received: 10.04.2020
Document Type: Article
UDC: 519.248
MSC: 62P30, 62-04
Language: English
Citation: A. I. Kibzun, A. S. Shalaev, V. M. Azanov, A. N. Ignatov, “Statistical analysis module for weight design of aircraft elements”, Vestnik YuUrGU. Ser. Mat. Model. Progr., 13:3 (2020), 29–42
Citation in format AMSBIB
\Bibitem{KibShaAza20}
\by A.~I.~Kibzun, A.~S.~Shalaev, V.~M.~Azanov, A.~N.~Ignatov
\paper Statistical analysis module for weight design of aircraft elements
\jour Vestnik YuUrGU. Ser. Mat. Model. Progr.
\yr 2020
\vol 13
\issue 3
\pages 29--42
\mathnet{http://mi.mathnet.ru/vyuru555}
\crossref{https://doi.org/10.14529/mmp200303}
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  • https://www.mathnet.ru/eng/vyuru/v13/i3/p29
  • This publication is cited in the following 1 articles:
    Citing articles in Google Scholar: Russian citations, English citations
    Related articles in Google Scholar: Russian articles, English articles
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    Full-text PDF :53
    References:22