Slewing Control of Flexible Structure Via Momentum Wheel and Piezoelectric Actuator
碩士 === 國立成功大學 === 航空太空工程學系 === 85 === To study the attitude control algorithms for the spacecraft with flexible structures ,this research first designed and constructed a simple experimental system for the study. The main part of the experimental system i...
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| Format: | Others |
| Language: | zh-TW |
| Online Access: | http://ndltd.ncl.edu.tw/handle/15426331906458715900 |