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Avtomatika i Telemekhanika, 2023, Issue 4, Pages 3–18
DOI: https://doi.org/10.31857/S0005231023040013 (Mi at15993) 		 
This article is cited in 1 scientific paper (total in 1 paper)

Nonlinear Systems

Aircraft cruise altitude and speed profile optimization in a real atmosphere

V. A. Aleksandrova, E. Yu. Zybina, V. V. Kos'yanchukb, N. I. Sel'vesyukb, E. A. Stefanyukac, A. A. Trembaca, M. V. Khlebnikovac

a Trapeznikov Institute of Control Sciences, Russian Academy of Sciences, Moscow, Russia
b State Research Institute of Aviation Systems, Moscow, Russia
c Moscow Institute of Physics and Technology (National Research University), Dolgoprudny, Russia
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DOI: https://doi.org/10.31857/S0005231023040013
Abstract: This paper considers subsonic turbojet aircraft fuel consumption minimization problem during cruise phase, assuming fixed time of arrival. The problem takes into account real atmosphere data. We utilize tailwind/headwind component values at various flight levels, as well as air temperatures and atmospheric pressures at various altitudes. The solution to the altitude and speed flight profile optimization problem is through constrained coordinate descent method. The paper considers optimizing the fuel consumption of a medium-haul aircraft during the cruise phase using sample data set on temperature, pressure, and wind speed. The proposed approach achieves a decrease in fuel consumption of 1.2
Keywords: optimization, subsonic turbojet aircraft, fuel consumption, air temperature, wind speed, flight modeling.
Funding agency Grant number
Russian Science Foundation 21-71-30005
The research was partially financially supported by Russian Science Foundation (project No. 21-71-30005), https://rscf.ru/en/project/21-71-30005/.
Presented by the member of Editorial Board: A. A. Galyaev

Received: 03.07.2022
Revised: 11.11.2022
Accepted: 30.11.2022
English version:
Automation and Remote Control, 2023, Volume 84, Issue 4, Pages 327–336
DOI: https://doi.org/10.1134/S0005117923040021
Bibliographic databases:
Document Type: Article
Language: Russian
Citation: V. A. Aleksandrov, E. Yu. Zybin, V. V. Kos'yanchuk, N. I. Sel'vesyuk, E. A. Stefanyuk, A. A. Tremba, M. V. Khlebnikov, “Aircraft cruise altitude and speed profile optimization in a real atmosphere”, Avtomat. i Telemekh., 2023, no. 4, 3–18; Autom. Remote Control, 84:4 (2023), 327–336
Citation in format AMSBIB
\Bibitem{AleZybKos23}
\by V.~A.~Aleksandrov, E.~Yu.~Zybin, V.~V.~Kos'yanchuk, N.~I.~Sel'vesyuk, E.~A.~Stefanyuk, A.~A.~Tremba, M.~V.~Khlebnikov
\paper Aircraft cruise altitude and speed profile optimization in a real atmosphere
\jour Avtomat. i Telemekh.
\yr 2023
\issue 4
\pages 3--18
\mathnet{http://mi.mathnet.ru/at15993}
\crossref{https://doi.org/10.31857/S0005231023040013}
\edn{https://elibrary.ru/QHPVML}
\transl
\jour Autom. Remote Control
\yr 2023
\vol 84
\issue 4
\pages 327--336
\crossref{https://doi.org/10.1134/S0005117923040021}
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    • This publication is cited in the following 1 articles:
    Citing articles in Google Scholar: Russian citations, English citations
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