Study of the normal and clamped modes of operation and dynamic response characteristics of the gimbaled control moment gyro (CMG) designed to fulfill the stringent pointing requirements of the Skylab telescope mount when the spacecraft is under the influence of both external and internal torques. The results indicate that the clamped mode of operation provides a feasible approach for significantly improving the system characteristics.
Attitude control of an orbiting space vehicle.
1971-11-01
Miscellaneous
No indication
English
Attitude control of an orbiting space vehicle.
AIAA | 1971
|On the attitude control of a high precision orbiting space interferometer
British Library Conference Proceedings | 1993
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