Design and Simulation of the Attitude Controller for Gravity Gradient Satellite
碩士 === 國立成功大學 === 航空太空工程學系碩博士班 === 97 === In this thesis﹐the design and simulation of the attitude control system of the gravity gradient satellite are presented﹐The designed satellite requirement is to use the gravity gradient boom and the magnetic coils controlling the attitude of a satellite at 5...
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| Format: | Others |
| Language: | zh-TW |
| Published: |
2009
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| Online Access: | http://ndltd.ncl.edu.tw/handle/52283616904727155616 |