Implementation of Attitude Determination and Control System into PACE Nanosatellite
碩士 === 國立成功大學 === 航空太空工程學系碩博士班 === 101 === The thesis describes the implementation of an active attitude determination and control system (ADCS) for the PACE nanosatellite. PACE satellite is a 2U cubesat under developed at National Cheng Kung University (NCKU) with a mass less than 2 kg and dimensio...
| Main Authors: | , |
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| Format: | Others |
| Language: | en_US |
| Published: |
2013
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| Online Access: | http://ndltd.ncl.edu.tw/handle/77308633372031690952 |