WEKO3
アイテム
生存性向上と迅速な開発を実現できる集中型と分散型アーキテクチャを組み合わせた小型宇宙機電力システムに関する研究
https://doi.org/10.18997/00007681
https://doi.org/10.18997/000076811c508135-a231-4d5b-8341-fe4452ecfe20
| 名前 / ファイル | ライセンス | アクション |
|---|---|---|
kou_k_484.pdf (9.5 MB)
|
|
| アイテムタイプ | 学位論文 = Thesis or Dissertation(1) | |||||||
|---|---|---|---|---|---|---|---|---|
| 公開日 | 2020-03-31 | |||||||
| 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 | Study on Electrical Power System combining centralized and distributed architectures to promote rapid development and survival improvement in Small Spacecraft | |||||||
| 言語 | en | |||||||
| タイトル | ||||||||
| タイトル | 生存性向上と迅速な開発を実現できる集中型と分散型アーキテクチャを組み合わせた小型宇宙機電力システムに関する研究 | |||||||
| 言語 | ja | |||||||
| 言語 | ||||||||
| 言語 | eng | |||||||
| 著者 |
Gonzalez Llorente, Jesus David
× Gonzalez Llorente, Jesus David
|
|||||||
| 抄録 | ||||||||
| 内容記述タイプ | Abstract | |||||||
| 内容記述 | Small spacecraft have been adopted by private companies and universities becoming more widespread in space applications. These programs do not have the same resources of traditional space programs; thus, low cost and fast delivery have been encouraged known as lean satellite programs. The delivery time of most of the small satellites is still more than two years and the failure rate of the small spacecraft is still a concern. Small satellites have the highest infant mortality rate and the Electrical Power System （EPS） is one the subsystems that contribute the most to the failure of CubeSats. To achieve fast delivery and low cost without compromise the reliability it is necessary to redefine the systems engineering of small spacecraft. Improvement in the development of EPS will contribute significantly to achieve the goals of low-cost and fast delivery of small spacecraft. The methods and guidelines for rapid development of electrical power systems have been proposed in this thesis. The architecture of EPS has been analyzed to diminish the failure rate that is related to the small spacecraft. In addition, a modular approach has been proposed to achieve rapid development and reliable systems. The module integrates the solar cells and the power condition units. Then, the EPS is designed integrating the required number of modules as it is demonstrated in Ten-Koh satellite. | |||||||
| 言語 | en | |||||||
| 目次 | ||||||||
| 内容記述タイプ | TableOfContents | |||||||
| 内容記述 | 1 Introduction||2 Analysis of EPS to improve mission assurance||3 Modular approach for power generation in EPS||4 Results of EPS in small spacecrafts: Ten-Koh case||5 Experimental results of ultracapacitor in Low Earth Orbit onboard Ten-Koh||6 Conclusions | |||||||
| 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484号 学位授与年月日：令和元年9月20日 | |||||||
| キーワード | ||||||||
| 主題Scheme | Other | |||||||
| 主題 | Small satellite | |||||||
| キーワード | ||||||||
| 主題Scheme | Other | |||||||
| 主題 | Micro-Satellite | |||||||
| キーワード | ||||||||
| 主題Scheme | Other | |||||||
| 主題 | Power Systems | |||||||
| キーワード | ||||||||
| 主題Scheme | Other | |||||||
| 主題 | Modular design | |||||||
| キーワード | ||||||||
| 主題Scheme | Other | |||||||
| 主題 | Spacecraft testing | |||||||
| キーワード | ||||||||
| 主題Scheme | Other | |||||||
| 主題 | Lean Satellite | |||||||
| アドバイザー | ||||||||
| 奥山, 圭一 | ||||||||
| 学位授与番号 | ||||||||
| 学位授与番号 | 甲第484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 | 2019-09-20 | |||||||
| 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 | 令和元年度 | |||||||
| 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 | 10.18997/00007681 | |||||||
| ID登録タイプ | JaLC | |||||||
