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 Conference Papers (Available on Advance Programs)  (Sort by: Date Descending)
 Results 1 - 15 of 15  /   
Committee Date Time Place Paper Title / Authors Abstract Paper #
EE 2020-01-16
14:25
Kagoshima HOUZAN HALL Experimental Study of MHz Switching Power Converter for Spacecraft
Minoru Iwasa, Hiromasa Kondo (JAXA) EE2019-74
 [more] EE2019-74
pp.147-150
EE, WPT, IEE-SPC 2018-07-03
10:15
Hokkaido Hokkaido University Application Study of Power Control System with Compound Semiconductor devices for Future Commercial Satellites
Minoru Iwasa, Hiromasa Kondo (JAXA) EE2018-14
In the commercial satellites, the orbit control systems are changed to the electoric propulsion from the chemical propul... [more] EE2018-14
pp.83-86
EE 2016-11-29
14:40
Tokyo Kikai-Shinko-Kaikan Bldg. The Fast MPPT Algorithm and Stability Analysis
Soichiro Nakamura (SEL), Minoru Iwasa (JAXA), Masatoshi Nakahara (Sojo Univ.) EE2016-46
Fast MPPT (maximum power point tracking) is required for the satellite. If the fast MPPT is realized, it is possible to ... [more] EE2016-46
pp.93-98
EE, WPT
(Joint)
2016-10-06
10:00
Kyoto   Study of MHz Switching Converter of Spacecraft for Lightweighting
Minoru Iwasa (JAXA) EE2016-19
 [more] EE2016-19
pp.1-5
EE 2016-01-29
14:50
Fukuoka KURUME HOTEL ESPRIT Study of Distributed and Cooperation Power Control System for Spacecraft
Minoru Iwasa, Hitoshi Naito, Hiroaki Kusawake (JAXA) EE2015-28
Spacecraft have many components required for existence in orbit, which are known as “BUS systems”. To increase the mass ... [more] EE2015-28
pp.115-120
EE 2015-01-29
16:30
Kumamoto Sakura-No-Baba JOSAIEN Study of Next-generation Power Control System for Spacecraft
Minoru Iwasa, Shuuhei Shimada, Hitoshi Naito, Hiroaki Kusawake (JAXA) EE2014-32
 [more] EE2014-32
pp.19-23
EE, IEE-SPC 2014-07-11
10:30
Hiroshima Hiroshima Institute of Technology A study of MPPT control algorithm based on the output current for spacecraft
Shuuhei Shimada, Minoru Iwasa, Hitoshi Naito, Hiroaki Kusawake (JAXA) EE2014-12
 [more] EE2014-12
pp.41-44
EE, CPM 2014-02-27
14:00
Tokyo Kikai-Shinko-Kaikan Bldg. The Simulation of Fast MPPT Algorithm by Newton's Method for a Satellite.
Soichiro Nakamura (Smart Energy Lab), Minoru Iwasa (JAXA), Masatoshi Nakahara (Sojo Univ.) EE2013-54 CPM2013-155
The solar power generation about the spin controlled satellite, it is required realizing a high speed MPPT because the m... [more] EE2013-54 CPM2013-155
pp.31-35
EE, IEE-SPC 2012-07-30
13:55
Nara   Study of Collaboration Power Control for Spacecraft
Minoru Iwasa, Hitoshi Naito, Hiroaki Kusawake (JAXA) EE2012-6
Spacecrafts have many components necessary for exsistence on orbit, for example, electrical power subsystem, thermal con... [more] EE2012-6
pp.5-8
EE 2011-01-28
14:15
Kumamoto   Study of Power Converter with Peak-Power-Tracking Function by Newton-method for Satellites
Minoru Iwasa (JAXA), Masatoshi Nakahara (Sojo Univ.), Hiroaki Kusawake, Koichi Kibe (JAXA) EE2010-38
JAXA works on a study of a digital power converter for future technology. Almost satellites don’t have a digital power c... [more] EE2010-38
pp.61-66
EE 2011-01-28
14:50
Kumamoto   Study of In-situ Observation System for Digital Source on Satellites
Shuuhei Shimada, Minoru Iwasa, Hiroaki Kusawake, Koichi Kibe (JAXA) EE2010-39
For the increase of the ratio of payloads at the satellites, a small-size and lightweight BUS system (electrical power s... [more] EE2010-39
pp.67-72
EE 2010-01-22
15:40
Fukuoka   Study of Control Algorithm for Digital Source on Satellites
Shuuhei Shimada, Minoru Iwasa, Hiroaki Kusawake, Koichi Kibe (JAXA) EE2009-52
For the increase of the ratio of payloads at the satellites, a small-size and lightweight BUS system (electrical power s... [more] EE2009-52
pp.93-97
EE 2009-07-30
13:50
Shimane   Study of digital source for satellites
Minoru Iwasa, Go Segami, Shuuhei Shimada, Hiroaki Kusawake, Koichi Kibe (JAXA) EE2009-9
For the increase of the ratio of payloads at the spacecraft, a small-size and lightweight BUS system (electrical power s... [more] EE2009-9
pp.13-18
EE 2008-07-24
16:30
Hokkaido   Study of the battery management for the spacecraft
Minoru Iwasa, Go Segami, Yuuta Horikawa, Shinichiro Takayama, Hiroaki Kusawake, Koichi Kibe (JAXA) EE2008-20
For the increase of the ratio of mission equipment at the spacecraft, a small-size and lightweight BUS system (electrica... [more] EE2008-20
pp.49-54
EE 2008-01-22
09:45
Fukuoka   Multistep Charge Method by Charge Arrays for Space Satellite
Go Segami, Hiroaki Kusawake, Yasuhiro Shimizu, Minoru Iwasa, Koichi Kibe (JAXA) EE2007-53
We studied the reduction in size and weight of Power Control Unit(PCU). In the study, we focused on the weight of Batter... [more] EE2007-53
pp.53-58
 Results 1 - 15 of 15  /   
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