NASA NTRS · 19740013997
CMG-induced LST dynamics
Abstract
The application of control moment gyroscopes to the pointing and control system of the large space telescope is discussed. The parameter plane analysis technique is used to present the nonlinearity representing the control moment gyroscope gimbal bearing friction. The technique affords both analytic and graphic portrayal of the effects of variations is selected system parameters. Diagrams of the systems involved in the tests are presented.
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Seltzer, S. M.. 1974-02-21. CMG-induced LST dynamics. https://ntrs.nasa.gov/citations/19740013997
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