High-Stability Attitude Control of Satellites by Magnetic Bearing Wheels.

SAWADA H; HASHIMOTO T; NINOMIYA K

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J-GLOBAL ID：200902175875177180 Reference number：02A0017717

High-Stability Attitude Control of Satellites by Magnetic Bearing Wheels.

磁気軸受ホイールを用いた衛星の高安定姿勢制御

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Material：
Volume： 44 Issue： 145 Page： 133-141 Publication year： Nov. 04, 2001
JST Material Number： F0167A ISSN： 0549-3811 CODEN： TJASA Document type： Article
Article type：原著論文 Country of issue： Japan (JPN) Language： ENGLISH (EN)

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Flight control systems

Reference (9)：

1) Suematsu, Y. and Solar-B Working Group: Scientific Objectives and Design Concepts of the OpticalTelescope and its Observing Instruments aboard Solar-B, ASP Conference Series, No. 183, 1999, pp. 198–205.
2) Heimel, H.: The Microvibration Characteristics of Momentum and Reaction Wheels, Presented at Second Space Microdynamics and Accurate Control Symposium (SMACS-2), CNES, Toulouse, France, May 1997.
3) Schauwecker, C. J., Shawger, S. L., Tung, F. C. and Nurre, G. S.: Imaging Pointing Control and Aspect Determination System for the NASA Advanced X-ray Astrophisics Facility, Adv. Astronaut. Sci. —Guid Control 1997, an AAS Publication, 92 (1997), pp. 567–581.
4) Nam, M. R., Hashimoto, T. and Ninomiya, K.: Design of H_∞ Attitude Controllers for Spacecraft Using a Magnetically Suspend Momentum Wheel, Eur. J. Control, 3 (1997), pp. 114–124.
5) Xie, Y. C., Sawada, H., Hashimoto, T. and Ninomiya, K.: Adaptive Model Following Control Method for Actively Controlled Magnetic Bearing Momentum Wheel, 5th International Symposium on Magnetic Suspension Technology, NASA/CP-2000-210291, July (2000), pp. 547–562.

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