Standard

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 POLYAKHOVS READING. ed. / AA Tikhonov. IEEE Canada, 2015.

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › Research › peer-review

Harvard

Aleksandrov, AY, Antipov, KA, Platonov, AV & Tikhonov, AA 2015, On a Satellite Stabilization in the Konig Frame. in AA Tikhonov (ed.), 2015 INTERNATIONAL CONFERENCE ON MECHANICS SEVENTH POLYAKHOVS READING. IEEE Canada, 2015 INTERNATIONAL CONFERENCE ON MECHANICS SEVENTH POLYAKHOV'S READING, Saint Petersburg, Russian Federation, 2/02/15.

APA

Aleksandrov, A. Y., Antipov, K. A., Platonov, A. V., & Tikhonov, A. A. (2015). On a Satellite Stabilization in the Konig Frame. In AA. Tikhonov (Ed.), 2015 INTERNATIONAL CONFERENCE ON MECHANICS SEVENTH POLYAKHOVS READING IEEE Canada.

Vancouver

Aleksandrov AY, Antipov KA, Platonov AV, Tikhonov AA. On a Satellite Stabilization in the Konig Frame. In Tikhonov AA, editor, 2015 INTERNATIONAL CONFERENCE ON MECHANICS SEVENTH POLYAKHOVS READING. IEEE Canada. 2015

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 POLYAKHOVS READING. editor / AA Tikhonov. IEEE Canada, 2015.

BibTeX

@inproceedings{b76ede3aad3a49eba4d63f619b4e4ea5,
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",
language = "Английский",
editor = "AA Tikhonov",
booktitle = "2015 INTERNATIONAL CONFERENCE ON MECHANICS SEVENTH POLYAKHOVS READING",
publisher = "IEEE Canada",
address = "Канада",
note = "null ; 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

M3 - статья в сборнике материалов конференции

BT - 2015 INTERNATIONAL CONFERENCE ON MECHANICS SEVENTH POLYAKHOVS READING

A2 - Tikhonov, AA

PB - IEEE Canada

Y2 - 2 February 2015 through 6 February 2015

ER -

ID: 74112477