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Mathematical model of spinning of a small spacecraft by engines - Flywheels. / Lamotkin, Alexey; Misyura, Natalia; Mityushov, Evgenij.
в: AIP Conference Proceedings, Том 2549, № 1, 060005, 2023.

Результаты исследований: Вклад в журналМатериалы конференцииРецензирование

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Lamotkin A, Misyura N, Mityushov E. Mathematical model of spinning of a small spacecraft by engines - Flywheels. AIP Conference Proceedings. 2023;2549(1):060005. doi: 10.1063/5.0109776

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BibTeX

@article{d1b95257918a42648468e1961f2989d7,
title = "Mathematical model of spinning of a small spacecraft by engines - Flywheels",
abstract = "An algorithm is proposed for constructing the programmed rotation of a small spacecraft in an orbital coordinate system using flywheel motors for a fixed time. The considered method makes it possible to build program control of flywheel motors, as a result of which the spacecraft is stabilized in rotational motion around the axis of dynamic symmetry, and this axis is oriented along the local vertical. {\textcopyright} 2023 American Institute of Physics Inc.. All rights reserved.",
author = "Alexey Lamotkin and Natalia Misyura and Evgenij Mityushov",
year = "2023",
doi = "10.1063/5.0109776",
language = "English",
volume = "2549",
journal = "AIP Conference Proceedings",
issn = "0094-243X",
publisher = "American Institute of Physics Publising LLC",
number = "1",

}

RIS

TY - JOUR

T1 - Mathematical model of spinning of a small spacecraft by engines - Flywheels

AU - Lamotkin, Alexey

AU - Misyura, Natalia

AU - Mityushov, Evgenij

PY - 2023

Y1 - 2023

N2 - An algorithm is proposed for constructing the programmed rotation of a small spacecraft in an orbital coordinate system using flywheel motors for a fixed time. The considered method makes it possible to build program control of flywheel motors, as a result of which the spacecraft is stabilized in rotational motion around the axis of dynamic symmetry, and this axis is oriented along the local vertical. © 2023 American Institute of Physics Inc.. All rights reserved.

AB - An algorithm is proposed for constructing the programmed rotation of a small spacecraft in an orbital coordinate system using flywheel motors for a fixed time. The considered method makes it possible to build program control of flywheel motors, as a result of which the spacecraft is stabilized in rotational motion around the axis of dynamic symmetry, and this axis is oriented along the local vertical. © 2023 American Institute of Physics Inc.. All rights reserved.

UR - http://www.scopus.com/inward/record.url?partnerID=8YFLogxK&scp=85176762735

U2 - 10.1063/5.0109776

DO - 10.1063/5.0109776

M3 - Conference article

VL - 2549

JO - AIP Conference Proceedings

JF - AIP Conference Proceedings

SN - 0094-243X

IS - 1

M1 - 060005

ER -

ID: 48512752