Mathematical Models of Rotational Motion of Spacecrafts with Superfluous Systems of Gyrodins and Flywheels and Problems of Control of Their Attitude. Part I

Victor V. Volosov; Igor A. Kutsenko; Vasiliy I. Popadinets

doi:10.1615/JAutomatInfScien.v35.i2.30

自动化与信息科学期刊

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每年出版 12 期

ISSN 打印: 1064-2315

ISSN 在线: 2163-9337

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

卷 35, 册 2, 2003, 13 pages

DOI: 10.1615/JAutomatInfScien.v35.i2.30

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Victor V. Volosov
Institute of Space Research of National Academy of Sciences of Ukraine and National Space Agency of Ukraine, Kyiv

Igor A. Kutsenko
Kyiv National Taras Shevchenko University, Kyiv, Ukraine

Vasiliy I. Popadinets
Kyiv National Taras Shevchenko University, Kyiv, Ukraine

摘要

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.

对本文的引用

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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