Art

J-GLOBAL ID：201202223693047923   Reference number：12A0112341

High Efficiency Control Method for the Hall Thruster System through Constant Flow Rate Control by Power Supply Control

電源制御による一定流速度制御によるホール型推進システムのための高効率制御法

Author (5)： OSUGA Hiroyuki (Mitsubishi Electric Corp., Kamakura Works) ,  OSUGA Hiroyuki (Graduate School of Eng., Nagasaki Univ.) ,  KUROKAWA Fujio (Graduate School of Eng., Nagasaki Univ.) ,  TAMIDA Taichiro (Mitsubishi Electric Corp., Advanced Technol. R&D Center) ,  YAMAMOTO Naoji (Graduate School of Eng., Kyushu Univ.)
Material： IEICE Transactions on Communications (Institute of Electronics, Information and Communication Engineers)  (IEICE Trans Commun (Inst Electron Inf Commun Eng))
Volume： E95-B  Issue： 1  Page： 133-142 (J-STAGE)  Publication year： 2012 
JST Material Number： L1369A  ISSN： 0916-8516  Document type： Article
Article type： 原著論文  Country of issue： Japan (JPN)  Language： ENGLISH (EN)

Thesaurus term： efficiency ,  magnetic flux density ,  anode ,  control ,  equipment ,  speed control ,  *artificial satellite
Semi thesaurus term： high efficiency ,  *thruster ,  *power distribution control ,  positive electrode

JST classification (1)： Space crafts  (QK08000Y)

Reference (20)：

• [1] A. Noda, M. Honma, and M. Utashima, “The study of a super low altitude satellite,” Proc. 26th International Symposium on Space Technology and Science, Hamamatsu, Japan, 2008-f-05, 2008.
• [2] H. Nagano, K. Kajiwara, H. Osuga, T. Ozaki, and F. Nakagawa, “Research and development of a new power processing unit of ion engine system for the super low altitude test satellite,” Proc. 27th International Symposium on Space Technology and Science, Tsukuba, Japan, 2009-b-55, 2009.
• [3] H. Nagano, K. Kajiwara, H. Osuga, T. Ozaki, F. Nakagawa, and K. Shuto, “Development status of a new power processing unit of ion engine system for the super low altitude test satellite,” Proc. 31st International Electric Propulsion Conference 2009, Ann Arbor, USA, IEPC2009-9, 2009.
• [4] H. Osuga and F. Kurokawa, “Power processing unit for the next generation satellite,” Proc. 13th European Conference on Power Electronics and Applications, EPE2009, Barcelona, Spain, 2009.
• [5] C.E. Garner, J.R. Brophy, J.E. Polk, A.V. Semenkin, V.I. Garlusha, S.O. Tverdokhlebov, and C. Marrese, “Experimental evaluation of Russian anode layer thrusters,” AIAA Paper 94-3010, 1994.

Terms in the title (6)： 定流 ,  速度制御 ,  ホール ,  推進システム ,  高効率 ,  制御法