Journal of Automation and Information Sciences
Publicou 12 edições por ano
ISSN Imprimir: 1064-2315
ISSN On-line: 2163-9337
SJR:
0.173
SNIP:
0.588
CiteScore™::
2
Indexed in
Mathematical Models of Rotational Motion of Spacecrafts with Superfluous Systems of Gyrodins and Flywheels and Problems of Control of Their Attitude. Part I
Volume 35,
Edição 2, 2003,
13 pages
DOI: 10.1615/JAutomatInfScien.v35.i2.30
RESUMO
Mathematical models of rotational motion of a rigid body controlled by superfluous gyrodin systems are considered. Algorithms of magnetic unloading and control of gyrosystems are suggested. These algorithms ensure prescribed attitude of a spacecraft and are optimal with respect to damping of the gyrosystem state function.
CITADO POR
-
Volosov V.V., Shevchenko V.M., Synthesis of control of the angular motion of a spacecraft on the basis of generalization of the direct Lyapunov method, Kosmìčna nauka ì tehnologìâ, 24, 4, 2018. Crossref
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