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All Technical Committee Conferences (Searched in: All Years)
| 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 |
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