Digital platform for aircraft weight design

被引：0

作者：

Skobelev S.I. ^{[1
]}

Strelets D.Y. ^{[1
]}

Kuryanskii M.K. ^{[2
]}

Vyshinskii L.L. ^{[3
]}

Grinev I.L. ^{[4
]}

机构：

[1] Moscow Aviation Institute (National Research University), Volokolamskoe Shosse, 4, Moscow

[2] Joint Stock Company «United Aircraft Corporation», Bolshaya Pionerskaya Str., 1, Moscow

[3] Federal Research Center «Informatics and Management» of the Russian Academy of Sciences, Vavilova, 44, b. 2, Moscow

[4] Joint Stock Company «Universal Systems and Technologies», St. Gilyarovskogo, 57, b. 4, Moscow

来源：

Aerospace Systems | 2022年 / 5卷 / 4期

关键词：

Aircraft; Aircraft weight model; Automated system; Center of gravity; Information technologies; Mass-inertia characteristics; Mathematical models; Weight analysis;

D O I：

10.1007/s42401-022-00154-w

中图分类号：

学科分类号：

摘要：

This paper discusses the concept, general structure and functions of the Digital Platform for Aircraft Weight Design, resulting from joined effort of several organizations with the leading role of the Moscow Aviation Institute. The paper briefly describes the main tasks of weight analysis, methods of their solution, as well as the architecture of the created system. The structure and main components of aircraft weight model are presented. The paper reports the methods for developing a digital platform and its components using a project approach to the creation of information systems. In the Conclusion section, an assessment of the place of the developed digital platform in the training of specialists in the field of weight analysis and the possibility of its application to a real aircraft project is discussed. © 2022, Shanghai Jiao Tong University.

引用

页码：577 / 589

页数：12

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