Standard

Application of a PID-like control to the problem of triaxial electrodynamic attitude stabilization of a satellite in the orbital frame. / Aleksandrov, A. Yu; Tikhonov, A. A.

в: Aerospace Science and Technology, Том 127, 107720, 01.08.2022.

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

Harvard

Aleksandrov, AY & Tikhonov, AA 2022, 'Application of a PID-like control to the problem of triaxial electrodynamic attitude stabilization of a satellite in the orbital frame', Aerospace Science and Technology, Том. 127, 107720. https://doi.org/10.1016/j.ast.2022.107720

APA

Aleksandrov, A. Y., & Tikhonov, A. A. (2022). Application of a PID-like control to the problem of triaxial electrodynamic attitude stabilization of a satellite in the orbital frame. Aerospace Science and Technology, 127, [107720]. https://doi.org/10.1016/j.ast.2022.107720

Vancouver

Aleksandrov AY, Tikhonov AA. Application of a PID-like control to the problem of triaxial electrodynamic attitude stabilization of a satellite in the orbital frame. Aerospace Science and Technology. 2022 Авг. 1;127. 107720. https://doi.org/10.1016/j.ast.2022.107720

Author

Aleksandrov, A. Yu ; Tikhonov, A. A. / Application of a PID-like control to the problem of triaxial electrodynamic attitude stabilization of a satellite in the orbital frame. в: Aerospace Science and Technology. 2022 ; Том 127.

BibTeX

@article{40e7c181466d4a49b1299afd1ba6a704,
title = "Application of a PID-like control to the problem of triaxial electrodynamic attitude stabilization of a satellite in the orbital frame",
abstract = "The problem of triaxial attitude stabilization of a satellite in the orbital frame is considered. The problem is raised about the possibility of implementing such a system of electrodynamic attitude control by the type of a PID controller in which the restoring component of the control torque contains a distributed delay. A constructive analytical approach to the nonlinear stability analysis in the problem of triaxial attitude stabilization of a satellite is presented. A theorem on the asymptotic stability of the stabilized angular position of the satellite is proved. The theorem substantiates the possibility of constructing the indicated control system. Nonlinear analysis is based on the Lyapunov direct method and an original construction of Lyapunov–Krasovskii functional. The effectiveness of the designed attitude control with a distributed delay is confirmed by a computer modeling.",
keywords = "Asymptotic stability, Distributed delay, Electrodynamic attitude control, Lyapunov–Krasovskii functional, PID controller, Satellite",
author = "Aleksandrov, {A. Yu} and Tikhonov, {A. A.}",
note = "Publisher Copyright: {\textcopyright} 2022 Elsevier Masson SAS",
year = "2022",
month = aug,
day = "1",
doi = "10.1016/j.ast.2022.107720",
language = "English",
volume = "127",
journal = "Aerospace Science and Technology",
issn = "1270-9638",
publisher = "Elsevier",

}

RIS

TY - JOUR

T1 - Application of a PID-like control to the problem of triaxial electrodynamic attitude stabilization of a satellite in the orbital frame

AU - Aleksandrov, A. Yu

AU - Tikhonov, A. A.

N1 - Publisher Copyright: © 2022 Elsevier Masson SAS

PY - 2022/8/1

Y1 - 2022/8/1

N2 - The problem of triaxial attitude stabilization of a satellite in the orbital frame is considered. The problem is raised about the possibility of implementing such a system of electrodynamic attitude control by the type of a PID controller in which the restoring component of the control torque contains a distributed delay. A constructive analytical approach to the nonlinear stability analysis in the problem of triaxial attitude stabilization of a satellite is presented. A theorem on the asymptotic stability of the stabilized angular position of the satellite is proved. The theorem substantiates the possibility of constructing the indicated control system. Nonlinear analysis is based on the Lyapunov direct method and an original construction of Lyapunov–Krasovskii functional. The effectiveness of the designed attitude control with a distributed delay is confirmed by a computer modeling.

AB - The problem of triaxial attitude stabilization of a satellite in the orbital frame is considered. The problem is raised about the possibility of implementing such a system of electrodynamic attitude control by the type of a PID controller in which the restoring component of the control torque contains a distributed delay. A constructive analytical approach to the nonlinear stability analysis in the problem of triaxial attitude stabilization of a satellite is presented. A theorem on the asymptotic stability of the stabilized angular position of the satellite is proved. The theorem substantiates the possibility of constructing the indicated control system. Nonlinear analysis is based on the Lyapunov direct method and an original construction of Lyapunov–Krasovskii functional. The effectiveness of the designed attitude control with a distributed delay is confirmed by a computer modeling.

KW - Asymptotic stability

KW - Distributed delay

KW - Electrodynamic attitude control

KW - Lyapunov–Krasovskii functional

KW - PID controller

KW - Satellite

UR - http://www.scopus.com/inward/record.url?scp=85132890944&partnerID=8YFLogxK

UR - https://www.mendeley.com/catalogue/5ec9de20-5ade-37a3-818a-5f42bd5e178a/

U2 - 10.1016/j.ast.2022.107720

DO - 10.1016/j.ast.2022.107720

M3 - Article

AN - SCOPUS:85132890944

VL - 127

JO - Aerospace Science and Technology

JF - Aerospace Science and Technology

SN - 1270-9638

M1 - 107720

ER -

ID: 96819201