Satellite attitude performance during the momentum dumping mode.
In this paper, the active magnetic control technique is applied for controlling the attitude and nutation of roll/yaw ares as well as unloading the excess wheel angular momentum for a small biased-momentum satellite in a nominal operation. Two control structures are configured using 2 and 3 magnetic...
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| Main Authors: | , |
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| Format: | Article |
| Language: | English English |
| Published: |
Praise Worthy Prize
2009
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| Online Access: | http://psasir.upm.edu.my/id/eprint/16620/1/Satellite%20attitude%20performance%20during%20the%20momentum%20dumping%20mode.pdf http://psasir.upm.edu.my/id/eprint/16620/ |
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