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Electrodynamic stabilization of artificial earth satellites in the Konig coordinate system. / Aleksandrov, A. Yu.; Antipov, K. A.; Platonov, A. V.; Tikhonov, A. A.

In: Journal of Computer and Systems Sciences International, Vol. 55, No. 2, 03.2016, p. 296-309.

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

Harvard

Aleksandrov, AY, Antipov, KA, Platonov, AV & Tikhonov, AA 2016, 'Electrodynamic stabilization of artificial earth satellites in the Konig coordinate system', Journal of Computer and Systems Sciences International, vol. 55, no. 2, pp. 296-309. https://doi.org/10.1134/S1064230716010020

APA

Aleksandrov, A. Y., Antipov, K. A., Platonov, A. V., & Tikhonov, A. A. (2016). Electrodynamic stabilization of artificial earth satellites in the Konig coordinate system. Journal of Computer and Systems Sciences International, 55(2), 296-309. https://doi.org/10.1134/S1064230716010020

Vancouver

Aleksandrov AY, Antipov KA, Platonov AV, Tikhonov AA. Electrodynamic stabilization of artificial earth satellites in the Konig coordinate system. Journal of Computer and Systems Sciences International. 2016 Mar;55(2):296-309. https://doi.org/10.1134/S1064230716010020

Author

Aleksandrov, A. Yu. ; Antipov, K. A. ; Platonov, A. V. ; Tikhonov, A. A. / Electrodynamic stabilization of artificial earth satellites in the Konig coordinate system. In: Journal of Computer and Systems Sciences International. 2016 ; Vol. 55, No. 2. pp. 296-309.

BibTeX

@article{d541fcfc496b4234bc632cafbc9078f5,
title = "Electrodynamic stabilization of artificial earth satellites in the Konig coordinate system",
abstract = "An artificial Earth satellite in a circular equatorial orbit is considered. We analyze the possibility of a satellite's three-axis stabilization in the Konig coordinate system using an electrodynamic control system exploiting Lorentz and magnetic control torques. Conditions allowing the electromagnetic control to solve the problem for a gravitational torque disturbance are obtained. In the nonlinear formulation, sufficient conditions for the asymptotic stability of the satellite equilibrium position are obtained.",
keywords = "POLE-PLACEMENT, SPACECRAFT",
author = "Aleksandrov, {A. Yu.} and Antipov, {K. A.} and Platonov, {A. V.} and Tikhonov, {A. A.}",
year = "2016",
month = mar,
doi = "10.1134/S1064230716010020",
language = "Английский",
volume = "55",
pages = "296--309",
journal = "Journal of Computer and Systems Sciences International",
issn = "1064-2307",
publisher = "МАИК {"}Наука/Интерпериодика{"}",
number = "2",

}

RIS

TY - JOUR

T1 - Electrodynamic stabilization of artificial earth satellites in the Konig coordinate system

AU - Aleksandrov, A. Yu.

AU - Antipov, K. A.

AU - Platonov, A. V.

AU - Tikhonov, A. A.

PY - 2016/3

Y1 - 2016/3

N2 - An artificial Earth satellite in a circular equatorial orbit is considered. We analyze the possibility of a satellite's three-axis stabilization in the Konig coordinate system using an electrodynamic control system exploiting Lorentz and magnetic control torques. Conditions allowing the electromagnetic control to solve the problem for a gravitational torque disturbance are obtained. In the nonlinear formulation, sufficient conditions for the asymptotic stability of the satellite equilibrium position are obtained.

AB - An artificial Earth satellite in a circular equatorial orbit is considered. We analyze the possibility of a satellite's three-axis stabilization in the Konig coordinate system using an electrodynamic control system exploiting Lorentz and magnetic control torques. Conditions allowing the electromagnetic control to solve the problem for a gravitational torque disturbance are obtained. In the nonlinear formulation, sufficient conditions for the asymptotic stability of the satellite equilibrium position are obtained.

KW - POLE-PLACEMENT

KW - SPACECRAFT

U2 - 10.1134/S1064230716010020

DO - 10.1134/S1064230716010020

M3 - статья

VL - 55

SP - 296

EP - 309

JO - Journal of Computer and Systems Sciences International

JF - Journal of Computer and Systems Sciences International

SN - 1064-2307

IS - 2

ER -

ID: 7558235