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  1. 学位論文
  2. 学位論文

CubeSatプラットホームとペイロード間の再構成可能なインターフェースボード

https://doi.org/10.18997/00009155
https://doi.org/10.18997/00009155
5d9862c3-d732-4a5d-a9ce-b7023c77ade1
名前 / ファイル ライセンス アクション
kou_k_559.pdf kou_k_559.pdf (2.7 MB)
アイテムタイプ 学位論文 = Thesis or Dissertation(1)
公開日 2023-03-31
資源タイプ
資源タイプ識別子 http://purl.org/coar/resource_type/c_db06
資源タイプ doctoral thesis
タイトル
タイトル Reconfigurable Interface Board Between CubeSat Platform and Payload
言語 en
タイトル
タイトル CubeSatプラットホームとペイロード間の再構成可能なインターフェースボード
言語 ja
言語
言語 eng
著者 Sejera, Marloun Pelayo

× Sejera, Marloun Pelayo

en Sejera, Marloun Pelayo

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内容記述タイプ Abstract
内容記述 The CubeSat design specifications have played a major role in the increasing trend in CubeSat launches. Not only it defines the size and form factor, but it also sets baseline requirements for developers to design their satellites to be compatible with as many CubeSat dispensers and launch opportunities as possible. However, it does not cover how the components in a CubeSat, both the bus and the payload, are interfaced. This could cause incompatibility issues between components and solving these issues could considerably consume time that could be used for other verification activities to ensure mission success. Furthermore, CubeSat projects can be developed by multiple collaborators, and clearly defining an interface standard between developers during the initial phase could prevent project delays, compatibility issues, and increased costs while improving overall mission success. The BIRDS satellite program of Kyushu Institute of Technology (Kyutech) has developed a standardized bus system for 1U CubeSats that uses a backplane board as the mechanical and electrical interface between bus subsystems and mission payloads. The backplane has a complex programmable logic device (CPLD) that manages digital routes between the bus and the payload by software configuration. This allows the backplane to be re-used in different projects resulting to lower cost and less development time. As a result, resources could be directed more toward developing the mission payload and instruments. Finally, it provides more time for integration and system-level verification, both of which are critical for a reliable and successful mission. The demand for launching CubeSats is on a continuous uptrend, and most CubeSats being launched are in 3U and 6U platforms mainly because they can accommodate multiple and complex payloads. Implementing a configurable interface board on larger CubeSat platforms could provide benefits similar to those in the 1U platform, such as a reduction in development throughput and cost.
目次
内容記述タイプ TableOfContents
内容記述 1. Introduction||2. BIRDS 1U Standard Bus||3. Reconfigurable 3U Backplane Prototype||4. Reconfigurable Backplane for W6U CubeSat||5. KITSUNE On-Orbit Test Results||6. Summary, Conclusions, and Recommendations
備考
内容記述タイプ Other
内容記述 九州工業大学博士学位論文 学位記番号:工博甲第559号 学位授与年月日:令和4年12月27日
キーワード
主題Scheme Other
主題 electrical interface
キーワード
主題Scheme Other
主題 backplane
キーワード
主題Scheme Other
主題 CubeSat
キーワード
主題Scheme Other
主題 bus system
キーワード
主題Scheme Other
主題 reconfigurable
アドバイザー
趙, 孟佑
学位授与番号
学位授与番号 甲第559号
学位名
学位名 博士(工学)
学位授与年月日
学位授与年月日 2022-12-27
学位授与機関
学位授与機関識別子Scheme kakenhi
学位授与機関識別子 17104
学位授与機関名 九州工業大学
学位授与年度
内容記述タイプ Other
内容記述 令和4年度
出版タイプ
出版タイプ VoR
出版タイプResource http://purl.org/coar/version/c_970fb48d4fbd8a85
アクセス権
アクセス権 open access
アクセス権URI http://purl.org/coar/access_right/c_abf2
ID登録
ID登録 10.18997/00009155
ID登録タイプ JaLC
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