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Natural Magneto-velocity Coordinate System for Satellite Attitude Stabilization : The Concept and Kinematic Analysis. / Tikhonov, A. A.

в: Journal of Applied and Computational Mechanics, Том 7, № 4, 2021, стр. 2113-2119.

Результаты исследований: Научные публикации в периодических изданияхстатьяРецензирование

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Tikhonov, A. A. / Natural Magneto-velocity Coordinate System for Satellite Attitude Stabilization : The Concept and Kinematic Analysis. в: Journal of Applied and Computational Mechanics. 2021 ; Том 7, № 4. стр. 2113-2119.

BibTeX

@article{3cbdaacf64a1482288ad601186fbf682,
title = "Natural Magneto-velocity Coordinate System for Satellite Attitude Stabilization: The Concept and Kinematic Analysis",
abstract = "An artificial Earth satellite with an electric charge and an intrinsic magnetic moment is considered. Due to the geomagnetic field, the satellite experiences the influence of the Lorentz and magnetic torques. To set the angular position of the satellite, we introduce natural coordinate system associated with the directions of geomagnetic induction vector and Lorentz force vector which is orthogonal both to the geomagnetic induction and relative velocity of the satellite. It is shown that such a natural magneto-velocity coordinate system is convenient for attitude stabilization of a satellite operating in the mode of scanning the Earth's surface. The properties of the trajectory of the satellite axis on the Earth's surface are analysed. The rotation tensor connecting the natural magneto-velocity and the orbital coordinate systems is obtained. The angular velocity of the natural magneto-velocity trihedron is found. Kinematic differential equations for the unit vectors of the natural magneto-velocity coordinate system are derived.",
keywords = "artificial Earth satellite, attitude control, electric charge, geomagnetic field, intrinsic magnetic moment",
author = "Tikhonov, {A. A.}",
note = "Publisher Copyright: {\textcopyright} 2021 Published by Shahid Chamran University of Ahvaz. All Rights Reserved.",
year = "2021",
doi = "10.22055/JACM.2021.37817.3094",
language = "English",
volume = "7",
pages = "2113--2119",
journal = "Journal of Applied and Computational Mechanics",
issn = "2383-4536",
publisher = "Shahid Chamran University of Ahvaz",
number = "4",

}

RIS

TY - JOUR

T1 - Natural Magneto-velocity Coordinate System for Satellite Attitude Stabilization

T2 - The Concept and Kinematic Analysis

AU - Tikhonov, A. A.

N1 - Publisher Copyright: © 2021 Published by Shahid Chamran University of Ahvaz. All Rights Reserved.

PY - 2021

Y1 - 2021

N2 - An artificial Earth satellite with an electric charge and an intrinsic magnetic moment is considered. Due to the geomagnetic field, the satellite experiences the influence of the Lorentz and magnetic torques. To set the angular position of the satellite, we introduce natural coordinate system associated with the directions of geomagnetic induction vector and Lorentz force vector which is orthogonal both to the geomagnetic induction and relative velocity of the satellite. It is shown that such a natural magneto-velocity coordinate system is convenient for attitude stabilization of a satellite operating in the mode of scanning the Earth's surface. The properties of the trajectory of the satellite axis on the Earth's surface are analysed. The rotation tensor connecting the natural magneto-velocity and the orbital coordinate systems is obtained. The angular velocity of the natural magneto-velocity trihedron is found. Kinematic differential equations for the unit vectors of the natural magneto-velocity coordinate system are derived.

AB - An artificial Earth satellite with an electric charge and an intrinsic magnetic moment is considered. Due to the geomagnetic field, the satellite experiences the influence of the Lorentz and magnetic torques. To set the angular position of the satellite, we introduce natural coordinate system associated with the directions of geomagnetic induction vector and Lorentz force vector which is orthogonal both to the geomagnetic induction and relative velocity of the satellite. It is shown that such a natural magneto-velocity coordinate system is convenient for attitude stabilization of a satellite operating in the mode of scanning the Earth's surface. The properties of the trajectory of the satellite axis on the Earth's surface are analysed. The rotation tensor connecting the natural magneto-velocity and the orbital coordinate systems is obtained. The angular velocity of the natural magneto-velocity trihedron is found. Kinematic differential equations for the unit vectors of the natural magneto-velocity coordinate system are derived.

KW - artificial Earth satellite

KW - attitude control

KW - electric charge

KW - geomagnetic field

KW - intrinsic magnetic moment

UR - http://www.scopus.com/inward/record.url?scp=85119188795&partnerID=8YFLogxK

U2 - 10.22055/JACM.2021.37817.3094

DO - 10.22055/JACM.2021.37817.3094

M3 - Article

AN - SCOPUS:85119188795

VL - 7

SP - 2113

EP - 2119

JO - Journal of Applied and Computational Mechanics

JF - Journal of Applied and Computational Mechanics

SN - 2383-4536

IS - 4

ER -

ID: 88944925