@inproceedings{oai:jaxa.repo.nii.ac.jp:00007699,
 author = {西山, 和孝 and 津田, 雄一 and 森, 治 and Nishiyama, Kazutaka and Tsuda, Yuichi and Mori, Osamu},
 book = {平成16年度アストロダイナミクスシンポジウム:講演後刷り集, ISAS proceedings of 14th Workshop on Astrodynamics and Flight Mechanics 2004: A Collection of Technical Papers},
 month = {Mar},
 note = {2003年5月に打上げた小惑星探査機「はやぶさ」はミッション期間のほとんどにおいて、イオンエンジンによる増速を継続的に行う必要がある。運用に必要な人手、時間、費用を削減ししかも安全確実な探査機の運行を実現するための運用システムの構築と完了に取り組んでいる。, The MUSES-C spacecraft was launched on May 9, 2003 and has been propelled by microwave discharge ion engines. The mission duration is four years in total and most of it is the cruising phase driven by ion propulsion. After one-year acceleration it succeeded the Earth swing-by on May 19, 2004 and still on the way to the asteroid ITOKAWA. A ground operation system that integrates all the process required for ion engine operations such as orbit synthesis, orbit determination, operation scheduling, command generation and telemetry data analysis has been developed. Automation of on-board and ground operations saves the operation cost and time, and makes the operation stable and reliable., 資料番号: AA0047897066},
 pages = {381--386},
 publisher = {宇宙航空研究開発機構宇宙科学研究本部, Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA/ISAS)},
 title = {HAYABUSA cruise operation},
 year = {2005}
}