Vibration Suppression of Large Space Structures Using an Optimized Distribution of Control Moment Gyros
Many space vehicles have been launched with large flexible components such as booms and solar panels. These large space structures (LSSs) have the potential to make attitude control unstable due to their lightly damped vibration. These vibrations can be controlled using a collection of control mome...
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| Language: | en_ca |
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2011
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| Online Access: | http://hdl.handle.net/1807/30543 |