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碩士 === 國立中央大學 === 太空科學研究所 === 103 === Advanced Ionosphere Probe (AIP), a science payload aboard the FORMORSAT-5 satellite, is combined with a sensor head and a control unit, Science Payload Electronics Unit (SPEU). The SPEU is used to control AIP operation and to communicate with Command and Data M...

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Main Authors: Feng-ming Cai, 蔡豐名
Other Authors: Chi-kuang Chao
Format: Others
Language:zh-TW
Published: 2015
Online Access:http://ndltd.ncl.edu.tw/handle/67266844536464984946
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spelling ndltd-TW-103NCU050690102016-05-22T04:41:04Z http://ndltd.ncl.edu.tw/handle/67266844536464984946 none 先進電離層探測儀數位控制單元之研製 Feng-ming Cai 蔡豐名 碩士 國立中央大學 太空科學研究所 103 Advanced Ionosphere Probe (AIP), a science payload aboard the FORMORSAT-5 satellite, is combined with a sensor head and a control unit, Science Payload Electronics Unit (SPEU). The SPEU is used to control AIP operation and to communicate with Command and Data Management Unit (CDMU). Under the current configuration, the AIP is difficult to be installed inside a CubeSat or a MicroSat due to volume and mass. In this thesis, a Digital Control Unit (DCU) is developed to replace the SPEU and can be installed inside the AIP sensor head compatibly. The new configuration simplifies communication difficulties and results in extremely reduction in the physical property but the same capabilities. The DCU uses Xilinx Spartan-6 Field Programmable Gate Array (FPGA) and is programmed in VerilogHDL. The schematic of the DCU is designed by NI Multism and the layout finished by NI Ultiboard under standard designs of the Xilinx Spartan-6 FPGA. All the DCU functions have been verified by an in-house Electrical Ground Segment Equipment which is constructed by NI CompatctRIO with in-house modules and programmed in NI LabVIEW. Chi-kuang Chao 趙吉光 2015 學位論文 ; thesis 106 zh-TW
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description 碩士 === 國立中央大學 === 太空科學研究所 === 103 === Advanced Ionosphere Probe (AIP), a science payload aboard the FORMORSAT-5 satellite, is combined with a sensor head and a control unit, Science Payload Electronics Unit (SPEU). The SPEU is used to control AIP operation and to communicate with Command and Data Management Unit (CDMU). Under the current configuration, the AIP is difficult to be installed inside a CubeSat or a MicroSat due to volume and mass. In this thesis, a Digital Control Unit (DCU) is developed to replace the SPEU and can be installed inside the AIP sensor head compatibly. The new configuration simplifies communication difficulties and results in extremely reduction in the physical property but the same capabilities. The DCU uses Xilinx Spartan-6 Field Programmable Gate Array (FPGA) and is programmed in VerilogHDL. The schematic of the DCU is designed by NI Multism and the layout finished by NI Ultiboard under standard designs of the Xilinx Spartan-6 FPGA. All the DCU functions have been verified by an in-house Electrical Ground Segment Equipment which is constructed by NI CompatctRIO with in-house modules and programmed in NI LabVIEW.
author2 Chi-kuang Chao
author_facet Chi-kuang Chao
Feng-ming Cai
蔡豐名
author Feng-ming Cai
蔡豐名
spellingShingle Feng-ming Cai
蔡豐名
none
author_sort Feng-ming Cai
title none
title_short none
title_full none
title_fullStr none
title_full_unstemmed none
title_sort none
publishDate 2015
url http://ndltd.ncl.edu.tw/handle/67266844536464984946
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AT fengmingcai xiānjìndiànlícéngtàncèyíshùwèikòngzhìdānyuánzhīyánzhì
AT càifēngmíng xiānjìndiànlícéngtàncèyíshùwèikòngzhìdānyuánzhīyánzhì
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