Skip to main content
SpringerLink
Log in

Digital platform for aircraft weight design

  • Original Paper
  • Published:
Aerospace Systems Aims and scope Submit manuscript

Abstract

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.

This is a preview of subscription content, log in via an institution to check access.

Access this article

Log in via an institution

Price excludes VAT (USA)
Tax calculation will be finalised during checkout.

Instant access to the full article PDF.

Institutional subscriptions

Fig. 1
Fig. 2
Fig. 3
Fig. 4
Fig. 5
Fig. 6
Fig. 7
Fig. 8
Fig. 9
Fig. 10

Similar content being viewed by others

Availability of data and materials

Not applicable.

Code availability

Not applicable.

References

  1. Aircraft designing (2018) Under the editorship of M.A. Pogosyan, 5-th edn. Innovative Engineering Manufacture, Moscow, pp 864

  2. Sheinin VM, Kozlovskii VI (1977) Weight designing and effectiveness of passenger aircraft, vol 1. Engineering Manufacture, Moscow, p 343

    Google Scholar 

  3. Eger SM, Liseitsev IK, Samoilovich OS (1986) Fundamentals of automated aircraft designing. Engineering Manufacture, Moscow

    Google Scholar 

  4. Approach to definition of digital platforms. Project URL: http://files.data-economy.ru/digital_platforms_project.pdf. Accessed 17.02.2021

  5. Vyshinskii LL, Flerov YA, Shirokov NI (2021) Automated system of aircraft weight designing. In: Informatics and its appliance. ch.12, Release 1, pp 18–30.https://doi.org/10.14357/19922264180103

  6. Vyshinskii LL, Flerov YA (2021) Informational model of weight configuration of airborne vehicles. In: Informatics and its appliance. ch.15, release 1

  7. Shirokov NI (2010) Automated system of weight calculations in the system of automated designing of AV. In: Collection of articles “Automated designing of engineer and financial information systems by means of Project Generator” ed. Flerov YA, Moscow: CC RAS, pp 55–66

  8. Skobelev SI, Shirokov NI (1991) Weight analysis and heck in the system of automated designing of AV. Tasks and methods of automated designing. CC RAN, Moscow

  9. Vyshinskii LL, Shirokov NI (2014) System of calculation automation of mass-inertia characteristics of AV with variable mass. Collection of articles “Development and appliance of tools package of Project Generator”, ed. Flerov YA, Moscow, CC RAS, pp 20–31

  10. Vyshinskii LL, Kuryanskii MK, Flerov YA (2019) Digital model of weight logbook of airborne vehicle. Informatics and its appliance, vol 13, release 4, pp 3–10. https://doi.org/10.14357/19922264190401

  11. Flerov YA, Vyshinskii LL (2018) Automation of designing of application information systems Information technologies and computing systems, vol 3, pp 29–42.https://doi.org/10.14357/20718632180303

  12. Vyshinskii LL, Grinev IL, Flerov YA, Shirokov AN, Shirokov NI (2003) Project generator—integrated tool set for development “client–server” systems. Inform Technol Comput Syst 1–2:6–25

    Google Scholar 

  13. Loginov AA, Shirokov NI (2014) New capabilities of project generator. In: Collection of articles “Development and appliance of integrated tool set Project Generator”. ed. Flerov YA, Moscow, CC RAS, pp 6–19

Download references

Funding

The authors have not disclosed any funding.

Author information

Authors and Affiliations

  1. Moscow Aviation Institute (National Research University), Volokolamskoe Shosse, 4, 125993, Moscow, Russia

    Sergei I. Skobelev & Dmitry Yu. Strelets

  2. Joint Stock Company «United Aircraft Corporation», Bolshaya Pionerskaya Str., 1, 115054, Moscow, Russia

    Mikhail K. Kuryanskii

  3. Federal Research Center «Informatics and Management» of the Russian Academy of Sciences, Vavilova, 44, b. 2, 119333, Moscow, Russia

    Leonid L. Vyshinskii

  4. Joint Stock Company «Universal Systems and Technologies», St. Gilyarovskogo, 57, b. 4, 129110, Moscow, Russia

    Igor L. Grinev

Authors
  1. Sergei I. Skobelev
    View author publications

    You can also search for this author in PubMed Google Scholar

  2. Dmitry Yu. Strelets
    View author publications

    You can also search for this author in PubMed Google Scholar

  3. Mikhail K. Kuryanskii
    View author publications

    You can also search for this author in PubMed Google Scholar

  4. Leonid L. Vyshinskii
    View author publications

    You can also search for this author in PubMed Google Scholar

  5. Igor L. Grinev
    View author publications

    You can also search for this author in PubMed Google Scholar

Corresponding author

Correspondence to Dmitry Yu. Strelets.

Ethics declarations

Conflicts of interest

Not applicable.

Rights and permissions

Reprints and permissions

About this article

Check for updates. Verify currency and authenticity via CrossMark

Cite this article

Skobelev, S.I., Strelets, D.Y., Kuryanskii, M.K. et al. Digital platform for aircraft weight design. AS 5, 577–589 (2022). https://doi.org/10.1007/s42401-022-00154-w

Download citation

  • Received:

  • Revised:

  • Accepted:

  • Published:

  • Issue Date:

  • DOI: https://doi.org/10.1007/s42401-022-00154-w

Keywords

Search

Navigation