Profile Information
- Affiliation
- Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency
- Degree
- 博士（工学）(Mar, 1998, 東京工業大学大学院)
- Contact information
- fukushima
isas.jaxa.jp - J-GLOBAL ID
- 201901001368573053
- researchmap Member ID
- B000358393
Research Interests
5Research Areas
1Research History
2Papers
10-
AEROSPACE TECHNOLOGY JAPAN, THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, 23 36-48, Oct, 2024 Peer-reviewedLead author
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Aerospace Technology Japan, 20 142-153, Dec, 2021 Peer-reviewedLead authorCorresponding author
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E3S Web of Conferences, 16, May 23, 2017© The Authors, published by EDP Sciences, 2017. The lithium-ion secondary batteries have been widely used for the space programs, today. Among them, REIMEI was one of the first satellites using lithium-ion secondary battery. In 2005, the satellite was launched, and injected into the low earth polar orbit. Eleven years has passed since the launch and over 60,000 cycles of charge and discharge was experienced in space. The lithium-ion secondary cell of the REIMEI battery was designed using spinel manganese oxide type material for the positive electrode, and the graphitized type carbon for the negative electrode. The cell case was made of aluminium laminated film and the structure was reinforced by the epoxy resin and aluminium housing. After the operation of eleven years, the cells still maintain the appropriate uniform balance and operative. In order to identify the internal condition of the battery/cell, we calculated the ac impedance by the pulse duration to the on-board battery.
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計測自動制御学会論文集, 48(7), 2012 Peer-reviewedLead author
Misc.
79-
宇宙航空研究開発機構研究開発資料 JAXA-RM-(Web), (20-002), 2021
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Jul, 2018 Lead author1st Sounding Rocket Symposium (July 17-18, 2018. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS)), Sagamihara, Kanagawa Japan
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Jul, 20181st Sounding Rocket Symposium (July 17-18, 2018. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS)), Sagamihara, Kanagawa Japan
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Jul, 2018 Lead author1st Sounding Rocket Symposium (July 17-18, 2018. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS)), Sagamihara, Kanagawa Japan
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IEEE Conference Proceedings, 2018(AMC), 2018 Lead author
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宇宙科学技術連合講演会講演集(CD-ROM), 61st, 2017 Lead author
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Nov, 2016 Lead authorBalloon Symposium 2016 (November 1-2, 2016. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS)), Sagamihara, Kanagawa Japan
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The 26th Workshop on JAXA Astrodynamics and Flight Mechanics (SA6000088031), Jul, 2016 Lead author
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Nov, 2015Balloon Symposium 2015 (November 5-6, 2015. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS)), Sagamihara, Kanagawa Japan
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大気球シンポジウム: 平成27年度 = Balloon Symposium: 2015, Nov, 2015大気球シンポジウム 平成27年度（2015年11月5-6日. 宇宙航空研究開発機構宇宙科学研究所 (JAXA)(ISAS)）, 相模原市, 神奈川県資料番号: SA6000044014レポート番号: isas15-sbs-014
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The 25th Workshop on JAXA Astrodynamics and Flight Mechanics (SA6000054060), 235-240, Jul, 2015 Lead author
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Nov, 2014 Lead authorBalloon Symposium 2014 (November 6-7, 2014. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS)), Sagamihara, Kanagawa Japan
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International Symposium on Artificial Intelligence, Robotics and Automation in Space i-SAIRAS, Sep, 2012 Lead author
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Proceedings - 4th IEEE International Conference on Space Mission Challenges for Information Technology, SMC-IT 2011, 2011 Lead author
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日本航空宇宙学会論文集, 56(650), 2008
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European Space Agency, (Special Publication) ESA SP, (660 SP), 2008 Lead author
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International Astronautical Federation - 59th International Astronautical Congress 2008, IAC 2008, 6, 2008 Lead author
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(6) 27-34, Mar 30, 2007Miniature space GPS (Global Positioning System) receivers have been developed by means of automobile-navigation technology. The weight and power consumption of the GPS receiver are 35 g and 1 W, respectively. We expanded the frequency sweep range in order to cover large Doppler shift in orbit. We tested the performance in low earth orbits by means of a GPS simulator. The GSP receiver succeeded in cold start acquisition in less than 30 minutes. This GPS receiver was on-boarded on INDEX satellite launched in August 2005. The performances of cold start acquisition and position accuracy was verified in orbit.
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International Astronautical Federation - 58th International Astronautical Congress 2007, 6, 2007
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IEICE technical report, 106(217) 17-22, Aug 18, 2006Miniature space GPS receivers have been developed by means of automobile-navigation technology. The weight and power consumption of the GPS receiver are 35g and 1W, respectively. We expanded the frequency sweep range in order to cover large Doppler shift in orbit. We tested the performance in low earth orbits by means of a GPS simulator. The GSP receiver succeeded in cold start acquisition in less than 30 minutes. This GPS receiver was on-boarded on INDEX satellite launched in August 2005. The performances of cold start acquisition and position accuracy was verified in orbit.
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宇宙科学技術連合講演会講演集(CD-ROM), 50th, 2006
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宇宙科学技術連合講演会講演集(CD-ROM), 50th, 2006
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Collection of Technical Papers. AIAA Guidance, Navigation and Control Conference, 2006(Vol.5), 2006
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European Space Agency, (Special Publication) ESA SP, 625 SP, 2006 Lead author
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宇宙科学技術連合講演会講演集(CD-ROM), 50th, 2006
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宇宙科学技術連合講演会講演集(CD-ROM), 50th, 2006 Lead author
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International Astronautical Federation - 56th International Astronautical Congress 2005, 4, 2005
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電子情報通信学会技術研究報告, 105(438(SANE2005 76-81)), 2005
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宇宙航空研究開発機構研究開発資料 JAXA-RM-, (04-011), 2004
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宇宙科学シンポジウム 平成14年度 第3回, 2003 Lead author
Presentations
25-
68th Space Sciences and Technology Conference, Nov 5, 2024
Professional Memberships
2-
Oct, 2011 - Present
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Apr, 1998 - Present
