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

ISSN Imprimir: 1064-2315
ISSN En Línea: 2163-9337

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Journal of Automation and Information Sciences

DOI: 10.1615/JAutomatInfScien.v30.i2-3.60
pages 39-51

Control of the Spherical Motion of a Spacecraft in the Earth Magnetic Field. Part II. Orientation and Stabilization

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

SINOPSIS

This paper continues the study of the problem on determination of parameters of the spherical motion of a spacecraft and control of this motion using only the Earth magnetic field. The problem of damping the angular velocity of this spacecraft and construction of three-axis orientation regime is solved. An algorithm for estimation of parameters of the spherical motion, which has a wide region of convergence, is proposed.


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