Electrodynamic Control with Distributed Delay for AES Stabilization in an Equatorial Orbit

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Electrodynamic Control with Distributed Delay for AES Stabilization in an Equatorial Orbit. / Alexandrov, A. Yu ; Tikhonov, A. A.

в: Cosmic Research, Том 60, № 5, 10.2022, стр. 366-374.

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

BibTeX

@article{fcbfe149ebfd436ea1d10cfa3ed3d02e,

title = "Electrodynamic Control with Distributed Delay for AES Stabilization in an Equatorial Orbit",

abstract = "Abstract: A satellite with an electrodynamic stabilization system is considered. To solve the problem of triaxial stabilization of an artificial satellite in an arbitrary position in the orbital coordinate system, the question is raised of the possibility of creating an electrodynamic control system for the angular motion of an artificial satellite according to the type of PID controller, which differs from the classical PID controller in that the restoring component of the control moment contains a distributed delay. A theorem concerning the asymptotic stability of the stabilized equilibrium position of an artificial satellite is proved, which confirms that it is possible to create the indicated system of electrodynamic control. The effectiveness of the proposed control system and the feasibility of its application for smoothing transient processes is confirmed by numerical simulation.",

author = "Alexandrov, {A. Yu} and Tikhonov, {A. A.}",

note = "Publisher Copyright: {\textcopyright} 2022, Pleiades Publishing, Ltd.",

year = "2022",

month = oct,

doi = "10.1134/s0010952522040013",

language = "English",

volume = "60",

pages = "366--374",

journal = "Cosmic Research",

issn = "0010-9525",

publisher = "МАИК {"}Наука/Интерпериодика{"}",

number = "5",

}

RIS

TY - JOUR

T1 - Electrodynamic Control with Distributed Delay for AES Stabilization in an Equatorial Orbit

AU - Alexandrov, A. Yu

AU - Tikhonov, A. A.

PY - 2022/10

Y1 - 2022/10

N2 - Abstract: A satellite with an electrodynamic stabilization system is considered. To solve the problem of triaxial stabilization of an artificial satellite in an arbitrary position in the orbital coordinate system, the question is raised of the possibility of creating an electrodynamic control system for the angular motion of an artificial satellite according to the type of PID controller, which differs from the classical PID controller in that the restoring component of the control moment contains a distributed delay. A theorem concerning the asymptotic stability of the stabilized equilibrium position of an artificial satellite is proved, which confirms that it is possible to create the indicated system of electrodynamic control. The effectiveness of the proposed control system and the feasibility of its application for smoothing transient processes is confirmed by numerical simulation.

AB - Abstract: A satellite with an electrodynamic stabilization system is considered. To solve the problem of triaxial stabilization of an artificial satellite in an arbitrary position in the orbital coordinate system, the question is raised of the possibility of creating an electrodynamic control system for the angular motion of an artificial satellite according to the type of PID controller, which differs from the classical PID controller in that the restoring component of the control moment contains a distributed delay. A theorem concerning the asymptotic stability of the stabilized equilibrium position of an artificial satellite is proved, which confirms that it is possible to create the indicated system of electrodynamic control. The effectiveness of the proposed control system and the feasibility of its application for smoothing transient processes is confirmed by numerical simulation.

UR - http://www.scopus.com/inward/record.url?scp=85139420724&partnerID=8YFLogxK

UR - https://www.mendeley.com/catalogue/83beafc6-927c-3535-8541-6d5141f470c2/

U2 - 10.1134/s0010952522040013

DO - 10.1134/s0010952522040013

M3 - Article

AN - SCOPUS:85139420724

VL - 60

SP - 366

EP - 374

JO - Cosmic Research

JF - Cosmic Research

SN - 0010-9525

IS - 5

ER -

ID: 99466499