Natural Magneto-velocity Coordinate System for Satellite Attitude Stabilization: Dynamics and Stability Analysis

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Natural Magneto-velocity Coordinate System for Satellite Attitude Stabilization: Dynamics and Stability Analysis. / Aleksandrov, A.Yu. ; Tikhonov, A. A. .

в: Journal of Applied and Computational Mechanics, Том 9, № 2, 2023, стр. 513-520.

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

BibTeX

@article{718e8cb64cee4c27b42fe8bcd8365bf7,

title = "Natural Magneto-velocity Coordinate System for Satellite Attitude Stabilization: Dynamics and Stability Analysis",

abstract = "The paper addresses the problem of attitude stabilization of an artificial Earth satellite with the aid of an electrodynamic control system. Our objective is to stabilize the satellite in a special coordinate system, whose axes are directed along the Lorentz force vector and the geomagnetic induction vector. Thus, natural magneto-velocity coordinate system (NMVCS) is used. We consider the general case of the satellite mass distribution. Therefore, the disturbing action of the gravitation torque is taken into account. The satellite moves along a circular near-Earth orbit. The nonlinear stability analysis based on the Lyapunov direct method is applied in the paper. The proposed approach gives us admissible domains of control parameters for which attitude stabilization in NMVCS is guaranteed without restrictions on the Earth{\textquoteright}s magnetic field model. Stabilization conditions are formulated in the form of explicit inequalities for the control parameters. As a result, a control strategy for the satellite attitude stabilization in the NMVCS is elaborated.",

keywords = "Satellite, attitude stabilization, natural magneto-velocity coordinate system, geomagnetic field, asymptotic ‎stability, asymptotic stability",

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

note = "Aleksandrov, A., & Tikhonov, A. (2022). Natural Magneto-velocity Coordinate System for Satellite ‎Attitude Stabilization: Dynamics and Stability Analysis. Journal of Applied and Computational Mechanics, (), -. doi: 10.22055/jacm.2022.41942.3842",

year = "2023",

doi = "10.22055/jacm.2022.41942.3842",

language = "English",

volume = "9",

pages = "513--520",

journal = "Journal of Applied and Computational Mechanics",

issn = "2383-4536",

publisher = "Shahid Chamran University of Ahvaz",

number = "2",

}

RIS

TY - JOUR

T1 - Natural Magneto-velocity Coordinate System for Satellite Attitude Stabilization: Dynamics and Stability Analysis

AU - Aleksandrov, A.Yu.

AU - Tikhonov, A. A.

N1 - Aleksandrov, A., & Tikhonov, A. (2022). Natural Magneto-velocity Coordinate System for Satellite ‎Attitude Stabilization: Dynamics and Stability Analysis. Journal of Applied and Computational Mechanics, (), -. doi: 10.22055/jacm.2022.41942.3842

PY - 2023

Y1 - 2023

N2 - The paper addresses the problem of attitude stabilization of an artificial Earth satellite with the aid of an electrodynamic control system. Our objective is to stabilize the satellite in a special coordinate system, whose axes are directed along the Lorentz force vector and the geomagnetic induction vector. Thus, natural magneto-velocity coordinate system (NMVCS) is used. We consider the general case of the satellite mass distribution. Therefore, the disturbing action of the gravitation torque is taken into account. The satellite moves along a circular near-Earth orbit. The nonlinear stability analysis based on the Lyapunov direct method is applied in the paper. The proposed approach gives us admissible domains of control parameters for which attitude stabilization in NMVCS is guaranteed without restrictions on the Earth’s magnetic field model. Stabilization conditions are formulated in the form of explicit inequalities for the control parameters. As a result, a control strategy for the satellite attitude stabilization in the NMVCS is elaborated.

AB - The paper addresses the problem of attitude stabilization of an artificial Earth satellite with the aid of an electrodynamic control system. Our objective is to stabilize the satellite in a special coordinate system, whose axes are directed along the Lorentz force vector and the geomagnetic induction vector. Thus, natural magneto-velocity coordinate system (NMVCS) is used. We consider the general case of the satellite mass distribution. Therefore, the disturbing action of the gravitation torque is taken into account. The satellite moves along a circular near-Earth orbit. The nonlinear stability analysis based on the Lyapunov direct method is applied in the paper. The proposed approach gives us admissible domains of control parameters for which attitude stabilization in NMVCS is guaranteed without restrictions on the Earth’s magnetic field model. Stabilization conditions are formulated in the form of explicit inequalities for the control parameters. As a result, a control strategy for the satellite attitude stabilization in the NMVCS is elaborated.

KW - Satellite

KW - attitude stabilization

KW - natural magneto-velocity coordinate system

KW - geomagnetic field

KW - asymptotic ‎stability

KW - asymptotic stability

UR - https://www.mendeley.com/catalogue/4cdb7cb4-e340-305f-ba20-d18fc156b1f5/

U2 - 10.22055/jacm.2022.41942.3842

DO - 10.22055/jacm.2022.41942.3842

M3 - Article

VL - 9

SP - 513

EP - 520

JO - Journal of Applied and Computational Mechanics

JF - Journal of Applied and Computational Mechanics

SN - 2383-4536

IS - 2

ER -

ID: 99922748