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 Conference Papers (Available on Advance Programs)  (Sort by: Date Descending)
 Results 1 - 11 of 11  /   
Committee Date Time Place Paper Title / Authors Abstract Paper #
EE 2016-11-28
11:30
Tokyo Kikai-Shinko-Kaikan Bldg. Proposal and Operation Analysis for PWM Converters Integrating PV Equalizer for Small Space Probes
Toshiki Shinohara, Masatoshi Uno (Ibaraki Univ.), Akio Kukita (JAXA) EE2016-32
Partial shading often appears on photovoltaic (PV) strings installed in small space probes representing moon exploration... [more] EE2016-32
pp.11-16
SANE 2015-05-29
16:50
Kanagawa JAXA Sagamihara Campus Demonstrations of Lunar Pinpoint Landing and Low Resource Spacecraft Technology by SLIM
Seisuke Fukuda, Shujiro Sawai, Shin-ichiro Sakai, Eiichi Sato, Takahide Mizuno, Takanao Saiki, Akio Kukita, Yu Miyazawa, Shun Okazaki, Jun-ichi Nakatsuka (JAXA), Hiroyuki Kamata (Meiji Univ.), Keiki Takadama (Univ. of Electro-Communications) SANE2015-15
 [more] SANE2015-15
pp.51-55
EE, IEE-HCA 2014-05-29
10:30
Tokyo The Kikai Shinko Kaikan building Two-Switch Cell Voltage Equalizer Using Series-Resonant Voltage Multiplier for Series-Connected Energy Storage Cells -- Consideration to Optimum Operation Mode for Integration with Charge-Discharge Regulator --
Masatoshi Uno, Akio Kukita (JAXA) EE2014-2
Cell voltage equalizers are a necessary component for series-connected energy storage cells, such as lithium-ion batteri... [more] EE2014-2
pp.7-12
EE 2013-10-11
11:15
Hokkaido Hokkaido University Clark Memorial Student Center Two-Switch Cell Voltage Equalizer Using a Half-Bridge Converter with Multi-Stacked Current Doublers
Masatoshi Uno, Akio Kukita (JAXA) EE2013-24
Voltage imbalance originating from nonuniformity of cell/module characteristics of energy storage devices, such as elect... [more] EE2013-24
pp.23-28
SANE 2012-10-11
12:00
Overseas The SONGDO CONVENSIA, Incheon Korea Development Status of Electrical Power Subsystem for X-ray Astronomy Satellite "ASTRO-H"
Takanobu Shimada, Kazuyuki Hirose, Akio Kukita, Hirokazu Ikeda, Yoshio Ohgushi, Masanobu Ozaki, Tadayasu Dotani, Tsuyoshi Okazaki, Tadayuki Takahashi (JAXA), Yukishige Nozaki, Takeshi Muramatsu (NTSpace), Kazuyo Mizushima (NEC) SANE2012-58
Japan Aerospace Exploration Agency (JAXA) has been developing an X-ray astronomy satellite named “ASTRO-H,” which will b... [more] SANE2012-58
pp.17-22
SANE 2012-06-28
14:55
Ibaraki Tsukuba Space Center, JAXA Feasibility Study on Spacecraft Power System Using Lithium-Ion Capacitor
Masatoshi Uno, Akio Kukita (JAXA) SANE2012-26
The feasibility of the spacecraft power system using lithium-ion capacitors (LICs) as its energy storage source is discu... [more] SANE2012-26
pp.31-36
SANE 2011-10-17
15:30
Overseas Udayana University, Bali, Indonesia SPRINT-A and SPRINT-Series in ISAS/JAXA
Munetaka Ueno, Seisuke Fukuda, Koji Nakaya, Shin-ichiro Sakai, Kazunori Uemizu, Shinsuke Takeuchi, Hiroyuki Toyota, Akio Kukita, Tomohiko Sakai, Shun Okazaki (JAXA), Ichiro Yoshikawa (Univ. of Tokyo), Atsushi Yamazaki, Takeshi Takashima, Kazushi Asamura, Shujiro Sawai (JAXA) SANE2011-73
 [more] SANE2011-73
pp.53-56
SANE 2009-08-28
10:55
Kanagawa JAXA Sagamihara campus Low Noise and Low Heat Generation Space Power Systems Using Flexible I-V Curve Control of Solar Array
Akio Kukita, Masatoshi Uno, Hiroyuki Toyota, Takanobu Shimada (JAXA)
For surplus electric power control of spacecrafts, shunt methods are mainly employed. The shunt methods are classified i... [more]
SANE 2009-08-28
11:20
Kanagawa JAXA Sagamihara campus A High-Reliable Charge Equalizer for Series-Connected Energy Storage Devices
Masatoshi Uno, Akio Kukita (JAXA) SANE2009-53
 [more] SANE2009-53
pp.5-8
SANE 2008-10-31
14:50
Kanagawa ISAS:Sagamihara campus (JAXA) Study of Supercapacitor-Based Spacecraft Power Subsystem
Masatoshi Uno, Hiroyuki Toyota, Akio Kukita (JAXA) SANE2008-57
 [more] SANE2008-57
pp.23-28
SANE 2008-10-31
15:15
Kanagawa ISAS:Sagamihara campus (JAXA) Flexible Capacity Battery System Using Auxiliary Cells and Bidirectional Converter
Masatoshi Uno, Akio Kukita (JAXA) SANE2008-58
Existing line-up of capacity of battery for aerospace is limited, so it is difficult to flexibly fulfill a various elect... [more] SANE2008-58
pp.29-33
 Results 1 - 11 of 11  /   
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