| Presentation | 2008-10-31 Flexible Capacity Battery System Using Auxiliary Cells and Bidirectional Converter Masatoshi UNO, Akio KUKITA, |
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| PDF Download Page |  PDF download Page Link |
| Abstract(in Japanese) | (See Japanese page) |
| Abstract(in English) | Existing line-up of capacity of battery for aerospace is limited, so it is difficult to flexibly fulfill a various electrical power demand of a spacecraft if required. In some cases, this results in increasing the cost and the weight of the spacecraft because of equipping with a battery of surplus capacity. In this paper, to solve this problem, we propose a new satellite battery system using both auxiliary cells and a bidirectional converter, which enables to flexibly design battery capacity for spacecrafts. |
| Keyword(in Japanese) | (See Japanese page) |
| Keyword(in English) | Battery / Bidirectional Converter / Charge/Discharge / PWM Control |
| Paper # | SANE2008-58 |
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| Committee | SANE |
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| Conference Date | 2008/10/24(1days) |
| Place (in Japanese) | (See Japanese page) |
| Place (in English) | |
| Topics (in Japanese) | (See Japanese page) |
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| Paper Information | |
| Registration To | Space, Aeronautical and Navigational Electronics (SANE) |
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| Language | JPN |
| Title (in Japanese) | (See Japanese page) |
| Sub Title (in Japanese) | (See Japanese page) |
| Title (in English) | Flexible Capacity Battery System Using Auxiliary Cells and Bidirectional Converter |
| Sub Title (in English) | |
| Keyword(1) | Battery |
| Keyword(2) | Bidirectional Converter |
| Keyword(3) | Charge/Discharge |
| Keyword(4) | PWM Control |
| 1st Author's Name | Masatoshi UNO |
| 1st Author's Affiliation | Japan Aerospace Exploration Agency() |
| 2nd Author's Name | Akio KUKITA |
| 2nd Author's Affiliation | Japan Aerospace Exploration Agency |
| Date | 2008-10-31 |
| Paper # | SANE2008-58 |
| Volume (vol) | vol.108 |
| Number (no) | 267 |
| Page | pp.pp.- |
| #Pages | 5 |
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