@inproceedings{oai:jaxa.repo.nii.ac.jp:00038767,
 author = {長野, 寛 and 今村, 俊介 and 早川, 幸男 and 照喜名, 勲 and 大須賀, 弘行 and 首藤, 和雄 and Nagano, Hiroshi and Imamura, Shunsuke and Hayakawa, Yukio and Terukina, Isao and Osuga, Hiroyuki and Shuto, Kazuo},
 book = {第59回宇宙科学技術連合講演会講演集, Proceedings of 59th Space Sciences and Technology Conference},
 month = {Oct},
 note = {第59回宇宙科学技術連合講演会（2015年10月7日-9日. かごしま県民交流センター), 鹿児島市, 鹿児島県, JAXA plans to launch the first satellite that flights in super-low altitude called the SLATS in 2017. The SLATS uses an ion engine system to compensate for air drag and keep its altitude. A power processing control unit (PPCU) in this ion engine system (IES) has been developed in three phases of BBM, partial EM and PFM. The PPCU is a power supply that includes sequence control function of an ion thruster. The integration reduces the IES cost, volume and mass. The control algorithm is considerably different from that in the Kiku-8 geostationary satellite. A highly autonomous control is utilized for the IES as the communication time between the SLATS and a ground station is very short. The BBM and partial EM tests have finished. The test results show that the PPCU has been developed successfully., 形態: カラー図版あり, Physical characteristics: Original contains color illustrations, 資料番号: AC1600023000, レポート番号: JSASS-2015-4547},
 publisher = {日本航空宇宙学会(JSASS), The Japan Society for Aeronautical and Space Sciences (JSASS)},
 title = {SLATS用イオンエンジン電源装置の開発試験},
 year = {2015}
}