Standard

Electrodynamic Control for Spacecraft Attitude Stability in the Geomagnetic Field. / Antipov, K.A.; Tikhonov, A.A.

In: Cosmic Research, Vol. 52, No. 6, 2014, p. 472-480.

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

Harvard

Antipov, KA & Tikhonov, AA 2014, 'Electrodynamic Control for Spacecraft Attitude Stability in the Geomagnetic Field', Cosmic Research, vol. 52, no. 6, pp. 472-480. https://doi.org/10.1134/S001095251406001X, https://doi.org/10.1134/S001095251406001X

APA

Antipov, K. A., & Tikhonov, A. A. (2014). Electrodynamic Control for Spacecraft Attitude Stability in the Geomagnetic Field. Cosmic Research, 52(6), 472-480. https://doi.org/10.1134/S001095251406001X, https://doi.org/10.1134/S001095251406001X

Vancouver

Antipov KA, Tikhonov AA. Electrodynamic Control for Spacecraft Attitude Stability in the Geomagnetic Field. Cosmic Research. 2014;52(6):472-480. https://doi.org/10.1134/S001095251406001X, https://doi.org/10.1134/S001095251406001X

Author

Antipov, K.A. ; Tikhonov, A.A. / Electrodynamic Control for Spacecraft Attitude Stability in the Geomagnetic Field. In: Cosmic Research. 2014 ; Vol. 52, No. 6. pp. 472-480.

BibTeX

@article{aa30e1d88ecc474a8ff6e6f62a34a654,
title = "Electrodynamic Control for Spacecraft Attitude Stability in the Geomagnetic Field",
abstract = "The electrodynamic method of spacecraft attitude control is studied in an octupole geomagnetic field approximation. An analytical derivation is given for refined laws of control over spacecraft electrodynamic parameters, which ensure the required spacecraft guidance. Spacecraft equilibrium position is proved to be stable under continually acting disturbances. The effectiveness and practical feasibility of the proposed spacecraft attitude control method is confirmed by numerical analysis.",
keywords = "STABILIZATION",
author = "K.A. Antipov and A.A. Tikhonov",
year = "2014",
doi = "10.1134/S001095251406001X",
language = "English",
volume = "52",
pages = "472--480",
journal = "Cosmic Research",
issn = "0010-9525",
publisher = "МАИК {"}Наука/Интерпериодика{"}",
number = "6",

}

RIS

TY - JOUR

T1 - Electrodynamic Control for Spacecraft Attitude Stability in the Geomagnetic Field

AU - Antipov, K.A.

AU - Tikhonov, A.A.

PY - 2014

Y1 - 2014

N2 - The electrodynamic method of spacecraft attitude control is studied in an octupole geomagnetic field approximation. An analytical derivation is given for refined laws of control over spacecraft electrodynamic parameters, which ensure the required spacecraft guidance. Spacecraft equilibrium position is proved to be stable under continually acting disturbances. The effectiveness and practical feasibility of the proposed spacecraft attitude control method is confirmed by numerical analysis.

AB - The electrodynamic method of spacecraft attitude control is studied in an octupole geomagnetic field approximation. An analytical derivation is given for refined laws of control over spacecraft electrodynamic parameters, which ensure the required spacecraft guidance. Spacecraft equilibrium position is proved to be stable under continually acting disturbances. The effectiveness and practical feasibility of the proposed spacecraft attitude control method is confirmed by numerical analysis.

KW - STABILIZATION

U2 - 10.1134/S001095251406001X

DO - 10.1134/S001095251406001X

M3 - Article

VL - 52

SP - 472

EP - 480

JO - Cosmic Research

JF - Cosmic Research

SN - 0010-9525

IS - 6

ER -

ID: 7029002