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Parametric control in the problem of spacecraft stabilization in the geomagnetic field. / Antipov, K. A.; Tikhonov, A. A.

In: Automation and Remote Control, Vol. 68, No. 8, 08.2007, p. 1333-1344.

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Antipov, K. A. ; Tikhonov, A. A. / Parametric control in the problem of spacecraft stabilization in the geomagnetic field. In: Automation and Remote Control. 2007 ; Vol. 68, No. 8. pp. 1333-1344.

BibTeX

@article{0b2943462ad2430298978a8c6b82919e,
title = "Parametric control in the problem of spacecraft stabilization in the geomagnetic field",
abstract = "The spacecraft interacting with the geomagnetic field in electrodynamic mode is subject to parametric perturbations; parameters of the spacecraft are controlled quasi-periodic functions. Under some conditions, there exist control algorithms for spacecraft electrodynamic parameters that allow realizing systems of spacecraft angular position stabilization. Stability of the spacecraft stabilized orientation is proved both analytically and by PC computations.",
author = "Antipov, {K. A.} and Tikhonov, {A. A.}",
year = "2007",
month = aug,
doi = "10.1134/S000511790708005X",
language = "Английский",
volume = "68",
pages = "1333--1344",
journal = "Automation and Remote Control",
issn = "0005-1179",
publisher = "МАИК {"}Наука/Интерпериодика{"}",
number = "8",
note = "null ; Conference date: 31-05-2006 Through 02-06-2006",

}

RIS

TY - JOUR

T1 - Parametric control in the problem of spacecraft stabilization in the geomagnetic field

AU - Antipov, K. A.

AU - Tikhonov, A. A.

PY - 2007/8

Y1 - 2007/8

N2 - The spacecraft interacting with the geomagnetic field in electrodynamic mode is subject to parametric perturbations; parameters of the spacecraft are controlled quasi-periodic functions. Under some conditions, there exist control algorithms for spacecraft electrodynamic parameters that allow realizing systems of spacecraft angular position stabilization. Stability of the spacecraft stabilized orientation is proved both analytically and by PC computations.

AB - The spacecraft interacting with the geomagnetic field in electrodynamic mode is subject to parametric perturbations; parameters of the spacecraft are controlled quasi-periodic functions. Under some conditions, there exist control algorithms for spacecraft electrodynamic parameters that allow realizing systems of spacecraft angular position stabilization. Stability of the spacecraft stabilized orientation is proved both analytically and by PC computations.

UR - http://www.scopus.com/inward/record.url?scp=34548445554&partnerID=8YFLogxK

U2 - 10.1134/S000511790708005X

DO - 10.1134/S000511790708005X

M3 - статья

AN - SCOPUS:34548445554

VL - 68

SP - 1333

EP - 1344

JO - Automation and Remote Control

JF - Automation and Remote Control

SN - 0005-1179

IS - 8

Y2 - 31 May 2006 through 2 June 2006

ER -

ID: 29122103