Spacecraft attitude control via mixed H2/H method
碩士 === 國立交通大學 === 電機與控制工程學系 === 86 === This thesis investigates the attitude control design problem of spacecraft systems considering external disturbances based on the linear , , and mixed / approach. It has been shown by Limebeer [33]...
| Main Authors: | , |
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| Format: | Others |
| Language: | zh-TW |
| Published: |
1998
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| Online Access: | http://ndltd.ncl.edu.tw/handle/71716477433372698115 |