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Informatika i Ee Primeneniya [Informatics and its Applications], 2021, Volume 15, Issue 1, Pages 50–56
DOI: https://doi.org/10.14357/19922264210107
(Mi ia711)
 

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

Information model of aircraft weight profile

L. L. Vyshinsky, Yu. A. Flerov

A. A. Dorodnicyn Computing Center, Federal Research Center “Computer Science and Control” of the Russian Academy of Sciences, 40 Vavilov Str., Moscow 119333, Russian Federation
Full-text PDF (256 kB) Citations (1)
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Abstract: The article is devoted to the description of the information model of the weight profile of an aircraft. The weight profile of an aircraft is understood as a set of interconnected information objects containing a description of the structure, parameters, and characteristics of the aircraft sufficient for weight calculations, weight analysis, and weight control at all stages of the product life cycle. The described information model can serve as the basis for a scheme of a database in the development of automated weight design systems. In the article, the weight model of an aircraft is described in terms of network data structures.
Keywords: design automation, aircraft, weight design, weighting model, design tree, project generator.
Received: 20.01.2020
Document Type: Article
Language: Russian
Citation: L. L. Vyshinsky, Yu. A. Flerov, “Information model of aircraft weight profile”, Inform. Primen., 15:1 (2021), 50–56
Citation in format AMSBIB
\Bibitem{VysFle21}
\by L.~L.~Vyshinsky, Yu.~A.~Flerov
\paper Information model of~aircraft weight profile
\jour Inform. Primen.
\yr 2021
\vol 15
\issue 1
\pages 50--56
\mathnet{http://mi.mathnet.ru/ia711}
\crossref{https://doi.org/10.14357/19922264210107}
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  • https://www.mathnet.ru/eng/ia/v15/i1/p50
  • 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
    Информатика и её применения
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    Full-text PDF :48
    References:25
     
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