@inproceedings{oai:jaxa.repo.nii.ac.jp:00007505,
 author = {山田, 克彦 and 吉河, 章二 and 島, 岳也 and Yamada, Katsuhiko and Yoshikawa, Shoji and Shima, Takeya},
 book = {第16回アストロダイナミクスシンポジウム講演後刷り集　2006, Proceedings of 16th Workshop on JAXA Astrodynamics and Flight Mechanics},
 month = {Mar},
 note = {本稿では楕円軌道における宇宙機の編隊飛行制御について検討する。相対的なフォーメーション軌道において、楕円軌道と同じ対称性を仮定することによってフォーメーションの初期条件を導く。この初期条件から従宇宙機が主宇宙機の周りを少ない距離変動で周回するような軌道や、従宇宙機が局所水平面内で周回する軌道など、いくつかの特徴的な軌道を求めることができる。, Formation flight of spacecraft in eccentric orbits is considered in this paper. Symmetry of the eccentric orbits is assumed in a relative formation trajectory, and under this assumption, relations of initial conditions in formation flight are derived. Some characteristic trajectories are obtained from these relations, such as a trajectory where a deputy spacecraft rotates around a chief spacecraft with relatively small variation in the distance between the two spacecraft, or a trajectory where the deputy spacecraft moves on a local horizontal plane on which the chief spacecraft exists. Formation flight by plural spacecraft is possible by combining these relative trajectories., 資料番号: AA0063481004},
 pages = {22--27},
 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 = {Spacecraft formation flying in eccentric orbits},
 year = {2007}
}