Rapid Spacecraft Attitude Tracking Maneuvers Using Sliding-Mode Control
碩士 === 國立交通大學 === 電機與控制工程系 === 89 === The thesis described the study of the practical spacecraft attitude guidance maneuvers to design useful rapid spacecraft attitude controller. We will derive the dynamic equation of the satellite and build its control law according to the different dir...
| Main Authors: | , |
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| Format: | Others |
| Language: | zh-TW |
| Published: |
2001
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| Online Access: | http://ndltd.ncl.edu.tw/handle/20695600784647080796 |