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 Conference Papers (Available on Advance Programs)  (Sort by: Date Descending)
 Results 1 - 19 of 19  /   
Committee Date Time Place Paper Title / Authors Abstract Paper #
EE, IEE-HCA 2022-05-27
13:00
Online Online [Special Talk] Research and development in power processing units for plasma propulsion
Yoshiki Matsunaga (JAXA), Toru Takahashi (TDS), Kazuhiro Kajiwara, Fujio Kurokawa (NiAS), Hiroaki Kusawake (JAXA) EE2022-3
The purpose of this paper is to describe power processing units (PPUs) for a space plasma propulsion called a Hall thrus... [more] EE2022-3
pp.12-17
EE 2022-01-28
11:20
Online Online Basic Experiment of Anode Power Supply using LLC Resonant Converter for Hall Thruster Systems
Hiromasa Kondo, Shinatora Choh, Hiroki Watanabe, Hiroaki Kusawake (JAXA) EE2021-44
JAXA is studying an anode power supply for realizing lightweight Hall thruster systems. The anode power supply has criti... [more] EE2021-44
pp.74-78
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
13:30
Tokyo Kikai-Shinko-Kaikan Bldg. Cycle Life Evaluation for Lithium Ion Cells for Space Application
Hitoshi Naito, Makoto Kawase, Tetsuya Ojima, Hiroaki Kusawake (JAXA) EE2013-53 CPM2013-154
The specific advantages of lithium-ion technology in energy density and working voltage offer the possibility of huge re... [more] EE2013-53 CPM2013-154
pp.27-30
SANE 2013-06-21
11:10
Ibaraki Tsukuba Space Center, JAXA Current Status of Development for Lithium-ion Cell Applied to Spacecraft
Makoto Kawase, Hitoshi Naito, Tetsuya Ojima, Hiroaki Kusawake (JAXA) SANE2013-26
Rechargeable batteries are used as energy storage devices in spacecraft. The specific advantages of lithium-ion battery ... [more] SANE2013-26
pp.63-66
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
EE 2007-07-20
11:10
Yamaguchi   The Development of The Battery Simulator
Go Segami, Hiroaki Kusawake, Yasuhiro Shimizu, Koichi Kibe (JAXA), Akira Utsumi (KIKUSUI) EE2007-19
When we test a power system of the satellite, we connect the power control unit, solar cells, batteries, loads and so on... [more] EE2007-19
pp.67-72
EE 2007-01-26
10:40
Nagasaki Nagasaki prefectural art museum Development of the balance circuit for the spacecraft
Go Segami, Hiroaki Kusawake, Yasuhiro Shimizu, Hitoshi Naito, Chisa Yamada, Koichi Kibe (JAXA), Hiroshi Sakamoto (Sojo Univ.) EE2006-48
To increase the ratio of the mission equipment at the spacecraft, small-size and lightweight electric power system is ex... [more] EE2006-48
pp.65-70
EE 2006-07-13
15:40
Tokyo   Failure Analysis and Simulation of Electrical Power System for Satellite
Go Segami, Hiroaki Kusawake, Yasuhiro Shimizu, Koichi Kibe (JAXA) EE2006-15
Fault tolerant desigen is necessary for satellite because we can’t repair anything in space if there is something wrong ... [more] EE2006-15
pp.35-39
EE, CPM 2006-01-20
13:55
Tokyo   Ground and Orbital Performance of OICETS Ni-MH Batteries
Chisa Yamada, Hiroaki Kusawake, Kohei Takagi, Hitoshi Naito, Koichi Kibe (JAXA)
The Optical Inter-orbit Communications Engineering Test Satellite (OICETS or Kirari) was launched on August 24, 2005, by... [more] EE2005-53 CPM2005-177
pp.37-42
EE, IEE-IEA 2004-07-23
11:30
Hokkaido Hokkaido University Orbital Performance of MDS-1 Ni-MH Battery
Chisa Yamada, Hiroaki Kusawake, Saburo Kuwajima (JAXA)
The Mission Demonstration Test Satellite-1 (MDS-1 or Tsubasa) has 2 batteries, which consist of 32 series of 20 Ah Ni-MH... [more] EE2004-24
pp.31-35
 Results 1 - 19 of 19  /   
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