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
收藏
页码：577 / 589
页数：12
相关论文
共 50 条
  • [21] Correction of Aircraft Empty Weight CG due to LRU Modification
    Lee, Jin Won
    Kwon, Na-Eun
    Kim, Ji-Hong
    Park, Jae Hyun
    JOURNAL OF THE KOREAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, 2022, 50 (08) : 551 - 557
  • [22] Advanced flow simulation methods in aircraft design
    Sillén, M
    AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY, 2002, 74 (02) : 138 - 146
  • [23] Silent aircraft pushes traditional design boundaries
    Assembly, 2007, 50 (05): : 8 - 15
  • [24] On a cellular division method for aircraft structural design
    Kobayashi, M. H.
    Pedro, H-T. C.
    Kolonay, R. M.
    Reich, G. W.
    AERONAUTICAL JOURNAL, 2009, 113 (1150) : 821 - 831
  • [25] DESIGN AND ANALYSIS OF WINGLETS FOR A SMALL COMMUTER AIRCRAFT
    Kant, Thusshaal
    Teja, S. V. S. Sai
    Nikhil, Y.
    D'Souza, Carine Viola
    Krishna, V.
    PROCEEDINGS OF THE 25TH NATIONAL AND 3RD INTERNATIONAL ISHMT-ASTFE HEAT AND MASS TRANSFER CONFERENCE, IHMTC 2019, 2019,
  • [26] Design of durable, repairable and maintainable aircraft composites
    Cole, W
    43RD INTERNATIONAL SAMPE SYMPOSIUM AND EXHIBITION ON MATERIALS AND PROCESS AFFORDABILITY - KEYS TO THE FUTURE, VOL 43, 1998, : 406 - 412
  • [27] Design Algorithm of an Aircraft Power Generation System
    Ismagilov, Flur Rashitovich
    Kiselev, Mikhail Anatolyevich
    Vavilov, Viacheslav Evgenievich
    Gusakov, Denis Valerievich
    IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS, 2019, 55 (06) : 2899 - 2910
  • [28] Application of System Engineering in Aircraft System Design
    Wang, Hao
    Tang, Yu
    Lv, Guangliang
    Yu, Yonggang
    Lan, Qingsheng
    Zhou, Zhu
    PROCEEDINGS OF THE 2024 3RD INTERNATIONAL SYMPOSIUM ON INTELLIGENT UNMANNED SYSTEMS AND ARTIFICIAL INTELLIGENCE, SIUSAI 2024, 2024, : 187 - 192
  • [29] Aircraft design using a variable density model
    Komarov, Valeriy A.
    Boldyrev, Andrey V.
    Kuznetsov, Anton S.
    Lapteva, Marina Yu.
    AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY, 2012, 84 (03) : 162 - 171
  • [30] A model for solar powered aircraft preliminary design
    Rizzo, E.
    Frediani, A.
    AERONAUTICAL JOURNAL, 2008, 112 (1128) : 57 - 78
12345