Published January 1, 2018
| Version v1
Conference paper
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EFFECTS OF ROTOR GEOMERY ON THE PERFORMANCE OF VIBRATING MASS CONTROL MOMENT GYRPOSCOPES
- 1. Middle Tech Univ, Dept Mech Engn, TR-06800 Ankara, Turkey
- 2. Middle Tech Univ, Dept Aerosp Engn, TR-06800 Ankara, Turkey
Description
Elimination of unwanted oscillations on the satellite body that may be caused by the vibrating rotor control moment gyroscopes is addressed. It is mathematically shown that proper rotor inertia selection removes the unwanted oscillations on the output axis of the control moment gyroscope. Simulation results carried out using the ADAMS mechanical modeling and simulation software are given and discussed.
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