Spacecraft Line-of-Sight Control Using a Single Variable-Speed Control Moment Gyro

Complete attitude control of a spacecraft is not possible with only one single-gimbal variable-speed control moment gyro due to the conservation of angular momentum. However, partial attitude control without violating the angular momentum conservation principle is still possible. In this paper feedb...

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Veröffentlicht in:	Journal of guidance, control, and dynamics control, and dynamics, 2006-11, Vol.29 (6), p.1295-1308
Hauptverfasser:	Yoon, Hyungjoo, Tsiotras, Panagiotis
Format:	Artikel
Sprache:	eng
Schlagworte:	Antennas Applied sciences Cameras Computer science control theory systems Control system synthesis Control theory. Systems Exact sciences and technology Fundamental areas of phenomenology (including applications) Physics Solid dynamics (ballistics, collision, multibody system, stabilization...) Solid mechanics Velocity Wheels
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