Development of a Control Moment Gyroscope controlled, three axis satellite simulator, with active balancing for the bifocal relay mirror initiative

Development of a Control Moment Gyroscope controlled, three axis satellite simulator, with active balancing for the bifocal relay mirror initiative

Approved for public release; distribution in unlimited. === This thesis develops and implements a Control Moment Gyroscope (CMG) steering law, controller and active balancing system for a three-axis satellite simulator (TASS). The CMGs are configured in a typical pyramid configuration (the fourth CM...

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Bibliographic Details
Main Author: Kulick, Wayne J.
Other Authors: Agrawal, Brij N.
Format: Others
Published: Monterey, California. Naval Postgraduate School 2012
Subjects:
Artificial satellites
Rotation
Attitude
Gyroscopic instruments
Astronautical instruments
Satellite Simulator
Active Balancing
Auto Balancing
Control Moment Gyroscope
CMG
Air Bearing
Online Access:http://hdl.handle.net/10945/1229

Internet

http://hdl.handle.net/10945/1229

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