@inproceedings{oai:jaxa.repo.nii.ac.jp:00007421,
 author = {大谷, 宏三 and 田中, 貴美恵 and 加藤, 貴昭 and 神川, えりか and 寺田, 博 and 小川, 美奈 and 井上, 高広 and 小西, 久弘 and 松本, 秀一 and 川勝, 康弘 and 広田, 正夫 and Otani, Kozo and Tanaka, Kimie and Kato, Takaaki and Kamikawa, Erika and Terada, Hiroshi and Ogawa, Mina and Inoue, Takahiro and Konishi, Hisahiro and Matsumoto, Shuichi and Kawakatsu, Yasuhiro and Hirota, Masao},
 book = {アストロダイナミクスシンポジウム講演後刷り集, Proceedings of 18th workshop on JAXA Astrodynamics and flight mechanics},
 month = {Mar},
 note = {Symposium on Flight Mechanics and Astrodynamics 2008 (July 28-29, 2008. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)), Sagamihara, Kanagawa Japan, 2007年12月に月周回衛星「かぐや(SELENE)」は1年間の定常運用を開始し、現在も高度100kmの極軌道を周回している。定常運用では、開発初期に検討・決定した高度維持方式を用いた軌道制御を約2ヶ月毎に実施している。また、2008年2月の月食では、電力的に最も安全な軌道位相への調整のための軌道制御を高度維持制御に合わせて実施した。本報告では、これらの軌道制御方式及び実施結果評価について報告する。, In October 2007, "KAGUYA (SELENE)" has started the routine mission for 1 year. Still now, "KAGUYA" has been orbiting the lunar lower polar orbit with the altitude of 100km. In nominal operations, the orbital maneuver has been executed every two months by altitude maintenance control method; the method had been examined and decided at the early stage of the development of "KAGUYA". And in lunar eclipse on February 2008, the orbit maneuver for the adjustment to the orbit which gives more saving of the battery power is performed with the altitude maintenance control. In this paper, these orbital maneuver control method and the operation results are reported., 形態: カラー図版あり, 著者人数: 13人, Physical characteristics: Original contains color illustrations, 資料番号: AA0064733047},
 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)},
 title = {「かぐや(SELENE)」定常運用における軌道制御},
 volume = {2008},
 year = {2009}
}