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Electrodynamic stabilization of earth-orbiting satellites in equatorial orbits. / Aleksandrov, A. Yu.; Tikhonov, A. A.

In: Cosmic Research, Vol. 50, No. 4, 07.2012, p. 313-318.

Research output: Contribution to journal › Article › peer-review

Harvard

Aleksandrov, AY & Tikhonov, AA 2012, 'Electrodynamic stabilization of earth-orbiting satellites in equatorial orbits', Cosmic Research, vol. 50, no. 4, pp. 313-318. https://doi.org/10.1134/S001095251203001X

APA

Aleksandrov, A. Y., & Tikhonov, A. A. (2012). Electrodynamic stabilization of earth-orbiting satellites in equatorial orbits. Cosmic Research, 50(4), 313-318. https://doi.org/10.1134/S001095251203001X

Vancouver

Aleksandrov AY, Tikhonov AA. Electrodynamic stabilization of earth-orbiting satellites in equatorial orbits. Cosmic Research. 2012 Jul;50(4):313-318. https://doi.org/10.1134/S001095251203001X

Author

Aleksandrov, A. Yu. ; Tikhonov, A. A. / Electrodynamic stabilization of earth-orbiting satellites in equatorial orbits. In: Cosmic Research. 2012 ; Vol. 50, No. 4. pp. 313-318.

BibTeX

@article{104902035cad4f96976aef2801b72183,
title = "Electrodynamic stabilization of earth-orbiting satellites in equatorial orbits",
abstract = "A satellite with electrodynamic stabilization system is considered. Based on the method of Lyapunov functions, sufficient conditions of the asymptotic stability of direct equilibrium position of this satellite in the orbital coordinate system under perturbing action of a gravitational moment are obtained. These conditions allow one to ensure a rational choice of parametric control coefficients depending on parameters of the satellite and its orbit.",
author = "Aleksandrov, {A. Yu.} and Tikhonov, {A. A.}",
year = "2012",
month = jul,
doi = "10.1134/S001095251203001X",
language = "Английский",
volume = "50",
pages = "313--318",
journal = "Cosmic Research",
issn = "0010-9525",
publisher = "МАИК {"}Наука/Интерпериодика{"}",
number = "4",

}

RIS

TY - JOUR

T1 - Electrodynamic stabilization of earth-orbiting satellites in equatorial orbits

AU - Aleksandrov, A. Yu.

AU - Tikhonov, A. A.

PY - 2012/7

Y1 - 2012/7

N2 - A satellite with electrodynamic stabilization system is considered. Based on the method of Lyapunov functions, sufficient conditions of the asymptotic stability of direct equilibrium position of this satellite in the orbital coordinate system under perturbing action of a gravitational moment are obtained. These conditions allow one to ensure a rational choice of parametric control coefficients depending on parameters of the satellite and its orbit.

AB - A satellite with electrodynamic stabilization system is considered. Based on the method of Lyapunov functions, sufficient conditions of the asymptotic stability of direct equilibrium position of this satellite in the orbital coordinate system under perturbing action of a gravitational moment are obtained. These conditions allow one to ensure a rational choice of parametric control coefficients depending on parameters of the satellite and its orbit.

U2 - 10.1134/S001095251203001X

DO - 10.1134/S001095251203001X

M3 - статья

VL - 50

SP - 313

EP - 318

JO - Cosmic Research

JF - Cosmic Research

SN - 0010-9525

IS - 4

ER -

ID: 5333492