Electrodynamical compensation of disturbing torque and attitude stabilization of a satellite in J(2) perturbed orbit

A. A. Tikhonov, K. A. Antipov, D. G. Korytnikov, D. Yu Nikitin

Результат исследований: Научные публикации в периодических изданияхстатья

Выдержка

The paper deals with a satellite in a circular near-Earth orbit, perturbed due to J(2) Earth's oblateness. The satellite interacts with the geomagnetic field by the moments of Lorentz and magnetic forces. The octupole approximation of the Earths magnetic field is used. The possibility of electrodynamical attitude control for the satellites 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.

Язык оригиналаАнглийский
Страницы (с-по)219-227
Число страниц9
ЖурналActa Astronautica
Том141
DOI
СостояниеОпубликовано - дек 2017

Цитировать

Tikhonov, A. A. ; Antipov, K. A. ; Korytnikov, D. G. ; Nikitin, D. Yu. / Electrodynamical compensation of disturbing torque and attitude stabilization of a satellite in J(2) perturbed orbit. В: Acta Astronautica. 2017 ; Том 141. стр. 219-227.
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title = "Electrodynamical compensation of disturbing torque and attitude stabilization of a satellite in J(2) perturbed orbit",
abstract = "The paper deals with a satellite in a circular near-Earth orbit, perturbed due to J(2) Earth's oblateness. The satellite interacts with the geomagnetic field by the moments of Lorentz and magnetic forces. The octupole approximation of the Earths magnetic field is used. The possibility of electrodynamical attitude control for the satellites 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 = "Satellite, Attitude stabilization, Geomagnetic field, Perturbed orbit, Electrodynamic attitude control system, SLIDING MODE CONTROL, GEOMAGNETIC-FIELD, COORDINATE SYSTEM, EARTH SATELLITE, ROTARY MOTION, SPACECRAFT, EVOLUTION, ALGORITHMS, DYNAMICS",
author = "Tikhonov, {A. A.} and Antipov, {K. A.} and Korytnikov, {D. G.} and Nikitin, {D. Yu}",
year = "2017",
month = "12",
doi = "10.1016/j.actaastro.2017.101009",
language = "Английский",
volume = "141",
pages = "219--227",
journal = "Acta Astronautica",
issn = "0094-5765",
publisher = "Elsevier",

}

Electrodynamical compensation of disturbing torque and attitude stabilization of a satellite in J(2) perturbed orbit. / Tikhonov, A. A.; Antipov, K. A.; Korytnikov, D. G.; Nikitin, D. Yu.

В: Acta Astronautica, Том 141, 12.2017, стр. 219-227.

Результат исследований: Научные публикации в периодических изданияхстатья

TY - JOUR

T1 - Electrodynamical compensation of disturbing torque and attitude stabilization of a satellite in J(2) perturbed orbit

AU - Tikhonov, A. A.

AU - Antipov, K. A.

AU - Korytnikov, D. G.

AU - Nikitin, D. Yu

PY - 2017/12

Y1 - 2017/12

N2 - The paper deals with a satellite in a circular near-Earth orbit, perturbed due to J(2) Earth's oblateness. The satellite interacts with the geomagnetic field by the moments of Lorentz and magnetic forces. The octupole approximation of the Earths magnetic field is used. The possibility of electrodynamical attitude control for the satellites 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 J(2) Earth's oblateness. The satellite interacts with the geomagnetic field by the moments of Lorentz and magnetic forces. The octupole approximation of the Earths magnetic field is used. The possibility of electrodynamical attitude control for the satellites 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 - Satellite

KW - Attitude stabilization

KW - Geomagnetic field

KW - Perturbed orbit

KW - Electrodynamic attitude control system

KW - SLIDING MODE CONTROL

KW - GEOMAGNETIC-FIELD

KW - COORDINATE SYSTEM

KW - EARTH SATELLITE

KW - ROTARY MOTION

KW - SPACECRAFT

KW - EVOLUTION

KW - ALGORITHMS

KW - DYNAMICS

U2 - 10.1016/j.actaastro.2017.101009

DO - 10.1016/j.actaastro.2017.101009

M3 - статья

VL - 141

SP - 219

EP - 227

JO - Acta Astronautica

JF - Acta Astronautica

SN - 0094-5765

ER -