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Electrodynamical compensation of disturbing torque and attitude stabilization of a satellite in J2 perturbed orbit. / Tikhonov, A. A.; Antipov, K. A.; Korytnikov, D. G.; Nikitin, D. Yu.

In: Acta Astronautica, Vol. 141, 01.12.2017, p. 219-227.

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

Harvard

Tikhonov, AA, Antipov, KA, Korytnikov, DG & Nikitin, DY 2017, 'Electrodynamical compensation of disturbing torque and attitude stabilization of a satellite in J2 perturbed orbit', Acta Astronautica, vol. 141, pp. 219-227. https://doi.org/10.1016/j.actaastro.2017.10.009, https://doi.org/10.1016/j.actaastro.2017.101009

APA

Tikhonov, A. A., Antipov, K. A., Korytnikov, D. G., & Nikitin, D. Y. (2017). Electrodynamical compensation of disturbing torque and attitude stabilization of a satellite in J2 perturbed orbit. Acta Astronautica, 141, 219-227. https://doi.org/10.1016/j.actaastro.2017.10.009, https://doi.org/10.1016/j.actaastro.2017.101009

Vancouver

Tikhonov AA, Antipov KA, Korytnikov DG, Nikitin DY. Electrodynamical compensation of disturbing torque and attitude stabilization of a satellite in J2 perturbed orbit. Acta Astronautica. 2017 Dec 1;141:219-227. https://doi.org/10.1016/j.actaastro.2017.10.009, https://doi.org/10.1016/j.actaastro.2017.101009

Author

Tikhonov, A. A. ; Antipov, K. A. ; Korytnikov, D. G. ; Nikitin, D. Yu. / Electrodynamical compensation of disturbing torque and attitude stabilization of a satellite in J2 perturbed orbit. In: Acta Astronautica. 2017 ; Vol. 141. pp. 219-227.

BibTeX

@article{abcaf02a3ff84bc1933546c0546fdb99,
title = "Electrodynamical compensation of disturbing torque and attitude stabilization of a satellite in J2 perturbed orbit",
abstract = "The paper deals with a satellite in a circular near-Earth orbit, perturbed due to J2 Earth's oblateness. The satellite interacts with the geomagnetic field by the moments of Lorentz and magnetic forces. The octupole approximation of the Earth's magnetic field is used. The possibility of electrodynamical attitude control for the satellite's stabilization in the orbital frame is analyzed. Once the problem of electrodynamical compensation of disturbing torque is solved, we can obtain the control algorithms for the satellite electromagnetic parameters which allows to stabilize the satellite attitude position in the orbital frame in the presence of disturbing gravity gradient torque. The total stability of the satellite programmed motion is proved analytically and verified by computer modeling.",
keywords = "Attitude stabilization, Electrodynamic attitude control system, Geomagnetic field, Perturbed orbit, Satellite",
author = "Tikhonov, {A. A.} and Antipov, {K. A.} and Korytnikov, {D. G.} and Nikitin, {D. Yu}",
year = "2017",
month = dec,
day = "1",
doi = "10.1016/j.actaastro.2017.10.009",
language = "English",
volume = "141",
pages = "219--227",
journal = "Acta Astronautica",
issn = "0094-5765",
publisher = "Elsevier",

}

RIS

TY - JOUR

T1 - Electrodynamical compensation of disturbing torque and attitude stabilization of a satellite in J2 perturbed orbit

AU - Tikhonov, A. A.

AU - Antipov, K. A.

AU - Korytnikov, D. G.

AU - Nikitin, D. Yu

PY - 2017/12/1

Y1 - 2017/12/1

N2 - The paper deals with a satellite in a circular near-Earth orbit, perturbed due to J2 Earth's oblateness. The satellite interacts with the geomagnetic field by the moments of Lorentz and magnetic forces. The octupole approximation of the Earth's magnetic field is used. The possibility of electrodynamical attitude control for the satellite's stabilization in the orbital frame is analyzed. Once the problem of electrodynamical compensation of disturbing torque is solved, we can obtain the control algorithms for the satellite electromagnetic parameters which allows to stabilize the satellite attitude position in the orbital frame in the presence of disturbing gravity gradient torque. The total stability of the satellite programmed motion is proved analytically and verified by computer modeling.

AB - The paper deals with a satellite in a circular near-Earth orbit, perturbed due to J2 Earth's oblateness. The satellite interacts with the geomagnetic field by the moments of Lorentz and magnetic forces. The octupole approximation of the Earth's magnetic field is used. The possibility of electrodynamical attitude control for the satellite's stabilization in the orbital frame is analyzed. Once the problem of electrodynamical compensation of disturbing torque is solved, we can obtain the control algorithms for the satellite electromagnetic parameters which allows to stabilize the satellite attitude position in the orbital frame in the presence of disturbing gravity gradient torque. The total stability of the satellite programmed motion is proved analytically and verified by computer modeling.

KW - Attitude stabilization

KW - Electrodynamic attitude control system

KW - Geomagnetic field

KW - Perturbed orbit

KW - Satellite

UR - http://www.scopus.com/inward/record.url?scp=85032392055&partnerID=8YFLogxK

U2 - 10.1016/j.actaastro.2017.10.009

DO - 10.1016/j.actaastro.2017.10.009

M3 - Article

AN - SCOPUS:85032392055

VL - 141

SP - 219

EP - 227

JO - Acta Astronautica

JF - Acta Astronautica

SN - 0094-5765

ER -

ID: 18083423