Development of Modular and Flexible Nano Satellite Flight Software
碩士 === 國立成功大學 === 電機工程學系碩博士班 === 101 === This thesis describes the development of the flight software for the Platform for Attitude Control Experiments (PACE) nano satellite with two design concepts: modularity and flexibility. The PACE satellite is a 2U CubeSat under developed at National Cheng Kun...
Main Authors: | , |
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Other Authors: | |
Format: | Others |
Language: | en_US |
Published: |
2013
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Online Access: | http://ndltd.ncl.edu.tw/handle/59181131690260747278 |