Approximate Feedback Linearization of Spacecraft with Momentum Exchange Devices
碩士 === 國立海洋大學 === 機械與輪機工程學系 === 84 === Spacecraft attitude control and momentum management is a highly nonlinearcontrol problem. The first objective of this thesis is to extend the result ofthe feedback linearization for spacecraft at...
| Main Authors: | , |
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| Other Authors: | |
| Format: | Others |
| Language: | zh-TW |
| Published: |
1996
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| Online Access: | http://ndltd.ncl.edu.tw/handle/78632488755136644379 |