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A Lean Satellite Electrical Power System with Direct Energy Transfer and Bus Voltage Regulation Based on a Bi-Directional Buck Converter
http://hdl.handle.net/10228/00008059
http://hdl.handle.net/10228/0000805912ecb04e-a5c3-479f-8654-83a9328e8ad2
名前 / ファイル | ライセンス | アクション |
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LaSEINE-2020_04.pdf (2.2 MB)
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Item type | 学術雑誌論文 = Journal Article(1) | |||||||||||
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公開日 | 2021-03-11 | |||||||||||
資源タイプ | ||||||||||||
資源タイプ識別子 | http://purl.org/coar/resource_type/c_6501 | |||||||||||
資源タイプ | journal article | |||||||||||
タイトル | ||||||||||||
タイトル | A Lean Satellite Electrical Power System with Direct Energy Transfer and Bus Voltage Regulation Based on a Bi-Directional Buck Converter | |||||||||||
言語 | ||||||||||||
言語 | eng | |||||||||||
著者 |
Rojas, Juan J.
× Rojas, Juan J.× Yamauchi, Takashi× 趙, 孟佑
WEKO
754
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抄録 | ||||||||||||
内容記述タイプ | Abstract | |||||||||||
内容記述 | The lean satellite approach requires aggressive measures for cutting development time and resource utilization; therefore, the power system should be simple, with a low part count, high reliability, and good electrical performance. The fully-regulated bus direct energy transfer (FRDET) architecture is considered the most common solution for big satellites; however, it is rarely used in lean satellite designs because of its complexity and the lack of commercial off-the-shelf solutions. Based on this, a new implementation of the FRDET architecture was proposed, prototyped, and evaluated. The system was based on a bidirectional converter that charges and discharges the battery while maintaining the bus voltage regulation. The system was evaluated by comparing it with the prevailing architectures in the field, in terms of efficiency and average harvested solar power per orbit. The proposed system was superior in both aspects which made it more suitable for its application in lean satellite designs. | |||||||||||
書誌情報 |
Aerospace 巻 7, 号 7, p. 94, 発行日 2020-07-05 |
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出版社 | ||||||||||||
出版者 | MDPI | |||||||||||
DOI | ||||||||||||
関連タイプ | isIdenticalTo | |||||||||||
識別子タイプ | DOI | |||||||||||
関連識別子 | https://doi.org/10.3390/aerospace7070094 | |||||||||||
日本十進分類法 | ||||||||||||
主題Scheme | NDC | |||||||||||
主題 | 538 | |||||||||||
ISSN | ||||||||||||
収録物識別子タイプ | ISSN | |||||||||||
収録物識別子 | 2226-4310 | |||||||||||
著作権関連情報 | ||||||||||||
権利情報 | Copyright (c) 2020 by the authors. Licensee MDPI, Basel, Switzerland. This article is an open access article distributed under the terms and conditions of the Creative Commons Attribution (CC BY) license (http://creativecommons.org/licenses/by/4.0/). | |||||||||||
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 system | |||||||||||
キーワード | ||||||||||||
主題Scheme | Other | |||||||||||
主題 | bi-directional converter | |||||||||||
出版タイプ | ||||||||||||
出版タイプ | VoR | |||||||||||
出版タイプResource | http://purl.org/coar/version/c_970fb48d4fbd8a85 | |||||||||||
査読の有無 | ||||||||||||
値 | yes | |||||||||||
連携ID | ||||||||||||
8593 | ||||||||||||
資料タイプ | ||||||||||||
内容記述タイプ | Other | |||||||||||
内容記述 | Journal Article | |||||||||||
著者所属 | ||||||||||||
Kyushu Institute of Technology, Instituto Tecnológico de Costa Rica | ||||||||||||
著者所属 | ||||||||||||
Kyushu Institute of Technology | ||||||||||||
著者所属 | ||||||||||||
Kyushu Institute of Technology |