NONLINEAR ATTITUDE CONTROL OF RIGID SPACECRAFT WITH FLEXIBLE STRUCTURE
博士 === 國立成功大學 === 航空太空工程學系 === 88 === Two methods of adaptive damping and variable structure control incorporating the stable vibration control are applied in this dissertation for the simultaneous multi-axis reorientation of a rigid spacecraft with flexible structur...
| Main Authors: | , |
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| Other Authors: | |
| Format: | Others |
| Language: | zh-TW |
| Published: |
2000
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| Online Access: | http://ndltd.ncl.edu.tw/handle/64511678074665389524 |