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On a Satellite Stabilization in the Konig Frame. / Aleksandrov, A. Yu.; Antipov, K. A.; Platonov, A. V.; Tikhonov, A. A.

2015 International Conference on Mechanics-Seventh Polyakhov's Reading. ред. / AA Tikhonov. Institute of Electrical and Electronics Engineers Inc., 2015.

Результаты исследований: Публикации в книгах, отчётах, сборниках, трудах конференций › статья в сборнике материалов конференции › научная › Рецензирование

Harvard

Aleksandrov, AY, Antipov, KA, Platonov, AV & Tikhonov, AA 2015, On a Satellite Stabilization in the Konig Frame. в AA Tikhonov (ред.), 2015 International Conference on Mechanics-Seventh Polyakhov's Reading. Institute of Electrical and Electronics Engineers Inc., VII Поляховские чтения, Saint Petersburg, Российская Федерация, 2/02/15. https://doi.org/10.1109/POLYAKHOV.2015.7106711

APA

Aleksandrov, A. Y., Antipov, K. A., Platonov, A. V., & Tikhonov, A. A. (2015). On a Satellite Stabilization in the Konig Frame. в AA. Tikhonov (Ред.), 2015 International Conference on Mechanics-Seventh Polyakhov's Reading Institute of Electrical and Electronics Engineers Inc.. https://doi.org/10.1109/POLYAKHOV.2015.7106711

Vancouver

Aleksandrov AY, Antipov KA, Platonov AV, Tikhonov AA. On a Satellite Stabilization in the Konig Frame. в Tikhonov AA, Редактор, 2015 International Conference on Mechanics-Seventh Polyakhov's Reading. Institute of Electrical and Electronics Engineers Inc. 2015 https://doi.org/10.1109/POLYAKHOV.2015.7106711

Author

Aleksandrov, A. Yu. ; Antipov, K. A. ; Platonov, A. V. ; Tikhonov, A. A. / On a Satellite Stabilization in the Konig Frame. 2015 International Conference on Mechanics-Seventh Polyakhov's Reading. Редактор / AA Tikhonov. Institute of Electrical and Electronics Engineers Inc., 2015.

BibTeX

@inproceedings{086598063a884c9284056ae810f29fa9,
title = "On a Satellite Stabilization in the Konig Frame",
abstract = "A circular orbiting artificial Earth satellite is considered. The satellite is equipped with an electrodynamic attitude control system exploiting Lorentz and magnetic control torques. The perturbing influence of the gravity-gradient torque is taken into account. The problem of satellite stabilization in the Konig coordinate system with the use of electrodynamic attitude control system is investigated in nonlinear formulation. On the basis of the Lyapunov functions method, sufficient conditions for the asymptotic stability of the programmed satellite equilibrium position in the Konig frame are obtained.",
keywords = "GEOMAGNETIC-FIELD, ELECTRODYNAMIC STABILIZATION, ATTITUDE STABILIZATION, CHARGED SATELLITE, EARTH SATELLITE, ROTARY MOTION, SPACECRAFT, STABILITY, EVOLUTION, BODY",
author = "Aleksandrov, {A. Yu.} and Antipov, {K. A.} and Platonov, {A. V.} and Tikhonov, {A. A.}",
year = "2015",
doi = "10.1109/POLYAKHOV.2015.7106711",
language = "English",
isbn = "978-1-4799-6824-4",
editor = "AA Tikhonov",
booktitle = "2015 International Conference on Mechanics-Seventh Polyakhov's Reading",
publisher = "Institute of Electrical and Electronics Engineers Inc.",
address = "United States",
note = "2015 INTERNATIONAL CONFERENCE ON MECHANICS SEVENTH POLYAKHOV'S READING : SEVENTH POLYAKHOV'S READING ; Conference date: 02-02-2015 Through 06-02-2015",
url = "http://pol2015.math.spbu.ru/en/, http://pol2015.math.spbu.ru/en/about/, http://pol2015.math.spbu.ru/",

}

RIS

TY - GEN

T1 - On a Satellite Stabilization in the Konig Frame

AU - Aleksandrov, A. Yu.

AU - Antipov, K. A.

AU - Platonov, A. V.

AU - Tikhonov, A. A.

N1 - Conference code: 7

PY - 2015

Y1 - 2015

N2 - A circular orbiting artificial Earth satellite is considered. The satellite is equipped with an electrodynamic attitude control system exploiting Lorentz and magnetic control torques. The perturbing influence of the gravity-gradient torque is taken into account. The problem of satellite stabilization in the Konig coordinate system with the use of electrodynamic attitude control system is investigated in nonlinear formulation. On the basis of the Lyapunov functions method, sufficient conditions for the asymptotic stability of the programmed satellite equilibrium position in the Konig frame are obtained.

AB - A circular orbiting artificial Earth satellite is considered. The satellite is equipped with an electrodynamic attitude control system exploiting Lorentz and magnetic control torques. The perturbing influence of the gravity-gradient torque is taken into account. The problem of satellite stabilization in the Konig coordinate system with the use of electrodynamic attitude control system is investigated in nonlinear formulation. On the basis of the Lyapunov functions method, sufficient conditions for the asymptotic stability of the programmed satellite equilibrium position in the Konig frame are obtained.

KW - GEOMAGNETIC-FIELD

KW - ELECTRODYNAMIC STABILIZATION

KW - ATTITUDE STABILIZATION

KW - CHARGED SATELLITE

KW - EARTH SATELLITE

KW - ROTARY MOTION

KW - SPACECRAFT

KW - STABILITY

KW - EVOLUTION

KW - BODY

U2 - 10.1109/POLYAKHOV.2015.7106711

DO - 10.1109/POLYAKHOV.2015.7106711

M3 - Conference contribution

SN - 978-1-4799-6824-4

BT - 2015 International Conference on Mechanics-Seventh Polyakhov's Reading

A2 - Tikhonov, AA

PB - Institute of Electrical and Electronics Engineers Inc.

T2 - 2015 INTERNATIONAL CONFERENCE ON MECHANICS SEVENTH POLYAKHOV'S READING

Y2 - 2 February 2015 through 6 February 2015

ER -

ID: 3930393