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Journal of Automation and Information Sciences
SJR: 0.232 SNIP: 0.464 CiteScore™: 0.27

ISSN Imprimer: 1064-2315
ISSN En ligne: 2163-9337

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Journal of Automation and Information Sciences

DOI: 10.1615/JAutomatInfScien.v33.i1.90
7 pages

Spacecraft Attitude Control Using the Magnetic-GPS Dataware System. Part I

Dmitriy V. Lebedev
International Research and Training Center of Information Technologies and Systems of National Academy of Sciences of Ukraine and Ministry of Education and Science of Ukraine, Kyiv
Alexander I. Tkachenko
International Research and Training Center of Information Technologies and Systems of National Academy of Sciences of Ukraine and Ministry of Education and Science of Ukraine, Kyiv

RÉSUMÉ

In this paper the attitude control system of a small spacecraft is considered. Reads of airborne magnetometers and satellite global positioning system (GPS) data are used for determination of the parameters of object motion. Such choice of measurements aims to raise estimations stability against disturbances of the magnetic storm type. At considerably undefined initial conditions for estimation of the desired parameters of motion we use the algorithm with an extended convergence domain.


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