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Алгоритмы аэродинамического управления относительным движением двух спутников по околокруговой орбите. / Andrievsky, B.; Kuznetsov, N. V.; Popov, A. M.

в: Differencialnie Uravnenia i Protsesy Upravlenia, № 4, 2020, стр. 28-58.

Результаты исследований: Научные публикации в периодических изданиях › Обзорная статья › Рецензирование

Harvard

Andrievsky, B, Kuznetsov, NV & Popov, AM 2020, 'Алгоритмы аэродинамического управления относительным движением двух спутников по околокруговой орбите', Differencialnie Uravnenia i Protsesy Upravlenia, № 4, стр. 28-58.

APA

Andrievsky, B., Kuznetsov, N. V., & Popov, A. M. (2020). Алгоритмы аэродинамического управления относительным движением двух спутников по околокруговой орбите. Differencialnie Uravnenia i Protsesy Upravlenia, (4), 28-58.

Vancouver

Andrievsky B, Kuznetsov NV, Popov AM. Алгоритмы аэродинамического управления относительным движением двух спутников по околокруговой орбите. Differencialnie Uravnenia i Protsesy Upravlenia. 2020;(4):28-58.

Author

Andrievsky, B. ; Kuznetsov, N. V. ; Popov, A. M. / Алгоритмы аэродинамического управления относительным движением двух спутников по околокруговой орбите. в: Differencialnie Uravnenia i Protsesy Upravlenia. 2020 ; № 4. стр. 28-58.

BibTeX

@article{035410027b9a42faa9145cf26556f05a,
title = "Алгоритмы аэродинамического управления относительным движением двух спутников по околокруговой орбите",
abstract = "In the recent years, there has been a growing interest in using aerodynamics drag force to eliminate relative drift between satellites moving in a group. This article is devoted to the development and study of some algorithms for decentalize stabilizing the relative position of two satellites moving in a near-circular Earth orbit. A brief review of approaches and results on methods of controlling a satellite group by changing the aerodynamic drag force is given. Control algorithms based on the modal (pole placement) approach, the passification-based and variable-structure control methods, linear and time-optimal partial stabilization are developed and studied. The robustness of control systems with respect to plant model parameters is examined. The possibility of the appearance of sustained oscillations as a consequence of the control action (the aerodynamic drag) boundedness is demonstrated.",
keywords = "Aerodynamic drag, Control, Modal control, Optimal performance, Oscillations, Partial stabilization, Passification, Relative position, Robustness, Stabilization, Swarm of nanosatellites",
author = "B. Andrievsky and Kuznetsov, {N. V.} and Popov, {A. M.}",
note = "Funding Information: Acknowledgements. This study was financially supported by the Ministry of Science and Higher Education of Russian Federation (project No. FZWF-2020-0015). Publisher Copyright: {\textcopyright} 2020 Saint-Petersburg State University. All rights reserved. Copyright: Copyright 2021 Elsevier B.V., All rights reserved.",
year = "2020",
language = "русский",
pages = "28--58",
journal = "ДИФФЕРЕНЦИАЛЬНЫЕ УРАВНЕНИЯ И ПРОЦЕССЫ УПРАВЛЕНИЯ",
issn = "1817-2172",
publisher = "Электронный журнал {"}Дифференциальные уравнения и процессы управления{"}",
number = "4",

}

RIS

TY - JOUR

T1 - Алгоритмы аэродинамического управления относительным движением двух спутников по околокруговой орбите

AU - Andrievsky, B.

AU - Kuznetsov, N. V.

AU - Popov, A. M.

N1 - Funding Information: Acknowledgements. This study was financially supported by the Ministry of Science and Higher Education of Russian Federation (project No. FZWF-2020-0015). Publisher Copyright: © 2020 Saint-Petersburg State University. All rights reserved. Copyright: Copyright 2021 Elsevier B.V., All rights reserved.

PY - 2020

Y1 - 2020

N2 - In the recent years, there has been a growing interest in using aerodynamics drag force to eliminate relative drift between satellites moving in a group. This article is devoted to the development and study of some algorithms for decentalize stabilizing the relative position of two satellites moving in a near-circular Earth orbit. A brief review of approaches and results on methods of controlling a satellite group by changing the aerodynamic drag force is given. Control algorithms based on the modal (pole placement) approach, the passification-based and variable-structure control methods, linear and time-optimal partial stabilization are developed and studied. The robustness of control systems with respect to plant model parameters is examined. The possibility of the appearance of sustained oscillations as a consequence of the control action (the aerodynamic drag) boundedness is demonstrated.

AB - In the recent years, there has been a growing interest in using aerodynamics drag force to eliminate relative drift between satellites moving in a group. This article is devoted to the development and study of some algorithms for decentalize stabilizing the relative position of two satellites moving in a near-circular Earth orbit. A brief review of approaches and results on methods of controlling a satellite group by changing the aerodynamic drag force is given. Control algorithms based on the modal (pole placement) approach, the passification-based and variable-structure control methods, linear and time-optimal partial stabilization are developed and studied. The robustness of control systems with respect to plant model parameters is examined. The possibility of the appearance of sustained oscillations as a consequence of the control action (the aerodynamic drag) boundedness is demonstrated.

KW - Aerodynamic drag

KW - Control

KW - Modal control

KW - Optimal performance

KW - Oscillations

KW - Partial stabilization

KW - Passification

KW - Relative position

KW - Robustness

KW - Stabilization

KW - Swarm of nanosatellites

UR - http://www.scopus.com/inward/record.url?scp=85106384265&partnerID=8YFLogxK

M3 - Обзорная статья

AN - SCOPUS:85106384265

SP - 28

EP - 58

JO - ДИФФЕРЕНЦИАЛЬНЫЕ УРАВНЕНИЯ И ПРОЦЕССЫ УПРАВЛЕНИЯ

JF - ДИФФЕРЕНЦИАЛЬНЫЕ УРАВНЕНИЯ И ПРОЦЕССЫ УПРАВЛЕНИЯ

SN - 1817-2172

IS - 4

ER -

ID: 78768668