@inproceedings{oai:jaxa.repo.nii.ac.jp:00007425,
 author = {市川, 勉 and 吉川, 真 and 加藤, 隆二 and 竹内, 央 and Ichikawa, Tsutomu and Yoshikawa, Makoto and Kato, Takaji and Takeuchi, Hiroshi},
 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, 現在、巡航中の「はやぶさ」ミッション及び今後の「IKAROS」ミッションにおいては連続微小加速度による軌道制御が実施される。軌道決定としてはこのような加速度に対しいかに精度を劣化させずに実施するかということを解析的に考察してみたので本論で紹介する。, There are interplanetary mission by using continuously Low-thrust system instead of impulse thrust system. This paper is described Earth-based orbit determination capability for the low-thrust spacecraft in the light of recent developments both in a few station tracking concepts and in the thrust subsystem error modeling. Both suboptimal and optimal orbit determination performance are determined for a wide range of process noise parameter values. The tracking techniques are found to be extremely effective, reducing orbit determination errors by orders of magnitude over that obtained with conventional single-station tracking., 形態: カラー図版あり, Physical characteristics: Original contains color illustrations, 資料番号: AA0064733051},
 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 = {低推力下での軌道決定についての一考察},
 volume = {2008},
 year = {2009}
}