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...

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Bibliographic Details
Main Authors: Yun-PengTsai, 蔡雲鵬
Other Authors: Jyh-Ching Juang
Format: Others
Language:en_US
Published: 2013
Online Access:http://ndltd.ncl.edu.tw/handle/59181131690260747278