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Design and Testing of a Lean Satellite Electrical Power Subsystem, HORYU-IV
https://doi.org/10.18997/00004744
https://doi.org/10.18997/00004744fdd172f0-adc4-4f60-868f-a521305c4c12
名前 / ファイル | ライセンス | アクション |
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Item type | 学位論文 = Thesis or Dissertation(1) | |||||||
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公開日 | 2016-12-27 | |||||||
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 | Design and Testing of a Lean Satellite Electrical Power Subsystem, HORYU-IV | |||||||
言語 | en | |||||||
その他のタイトル | ||||||||
その他のタイトル | 超小型衛星鳳龍四号の電源サブシステムの設計と試験 | |||||||
言語 | ja | |||||||
言語 | ||||||||
言語 | eng | |||||||
著者 |
Edries, Mohamed Yahia
× Edries, Mohamed Yahia
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抄録 | ||||||||
内容記述タイプ | Abstract | |||||||
内容記述 | HORYU-IV is a lean satellite weighing 12 kg designed at the Kyushu Institute of Technology. It is launched with the ASTRO-H in February 2016 as a piggyback on an H-IIA rocket. The main mission of HORYU-IV is to acquire on-orbit data of discharge phenomena occurring on high-voltage solar arrays. An electrical power subsystem (EPS) is one of the HORYU-IV bus subsystems. The function of the EPS is to provide uninterrupted power to all subsystems during the satellite’s lifetime. High reliability, high efficiency and simplicity are the main requirements to be considered in the design of an EPS. Generally, an EPS consists of solar arrays, rechargeable batteries, and a power control and distribution unit (PCDU). A peak power tracking topology is preferred to extract the maximum power generated by the solar arrays. The extra energy is stored in nickel-metal hydride batteries. The simple design and usage of available commercial-off-the-shelf components are the main features of the PCDU which controls the battery charging and load voltage regulation. Functional tests under different operating conditions were carried out on the designed EPS to qualify its performance. The aim of this research is to develop EPS with the “Lean” concepts and methods to achieve low cost and fast delivery subsystem. All design details have been explained and the test results have been analyzed. The in-orbit data have been analyzed to verify the design. | |||||||
目次 | ||||||||
内容記述タイプ | Other | |||||||
内容記述 | 1 Introduction||2 EPS design tools and fault analysis||3 Design of HORYU-IV Electrical Power Subsystem||4 Testing of HORYU-IV EPS||5 In-orbit data analysis of HORYU-IV Electrical Power Subsystem and conclusion | |||||||
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426号 学位授与年月日:平成28年9月23日 | |||||||
キーワード | ||||||||
主題Scheme | Other | |||||||
主題 | Lean Satellite | |||||||
キーワード | ||||||||
主題Scheme | Other | |||||||
主題 | Electrical Power Subsystem | |||||||
キーワード | ||||||||
主題Scheme | Other | |||||||
主題 | HORYU-IV | |||||||
キーワード | ||||||||
主題Scheme | Other | |||||||
主題 | Peak Power Tracking | |||||||
キーワード | ||||||||
主題Scheme | Other | |||||||
主題 | Nickel-Metal-Hydride Batteries | |||||||
キーワード | ||||||||
主題Scheme | Other | |||||||
主題 | Solar Arrays | |||||||
アドバイザー | ||||||||
趙, 孟佑 | ||||||||
学位授与番号 | ||||||||
学位授与番号 | 甲第426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 | 2016-09-23 | |||||||
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 | 平成28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 | 10.18997/00004744 | |||||||
ID登録タイプ | JaLC | |||||||
著者(ヨミ) | ||||||||
識別子Scheme | WEKO | |||||||
識別子 | 33920 | |||||||
姓名 | イドリス, モハメッド ヤヒア |