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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
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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
  1. 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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