@inproceedings{oai:jaxa.repo.nii.ac.jp:00007566,
 author = {歌島, 昌由 and Utashima, Masayoshi},
 book = {第15回アストロダイナミクスシンポジウム講演後刷り集　2005, Proceedings of 15th Workshop on JAXA Astrodynamics and Flight Mechanics},
 month = {Mar},
 note = {リサジュ軌道やハロー軌道は不安定なために数ヶ月間隔の軌道保持制御が必須であり、正確な摂動モデルの下でΔVゼロの基準軌道を前もって設計しておき、それに追従する様に保持制御が行なわれている。欧米では、3次以上の高次解析解を初期値として基準軌道が作成されているが、本論文では、線型解だけを使用してリサジュ基準軌道を作成する新しい方法を述べる。, Since both Lissajous and halo orbits are unstable, orbital maintenance maneuvers at several month intervals are necessary. In order to perform orbital maintenance, a reference trajectory with zero Delta V is designed in advance under a precise model of perturbations. Orbital maintenance maneuvers are then performed such that the reference orbit is maintained. In Europe and the United States, a third- or higher-order analytical solution is used as an initial trajectory for obtaining a reference orbit. In this paper, we present a new method for reference Lissajous orbits which does not need higher-order solutions., 資料番号: AA0063480001},
 pages = {1--6},
 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 = {Design of reference Lissajous trajectories around the L2 point in the Sun-Earth system},
 year = {2006}
}