@inproceedings{oai:jaxa.repo.nii.ac.jp:00007415,
 author = {坂東, 麻衣 and 市川, 朗 and Bando, Mai and Ichikawa, Akira},
 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, 摘要: 円軌道上の宇宙機近傍での線形化された相対運動の方程式（Hill-Clohessy-Whiltshire方程式）は、制御時間を十分長く取ることにより、制御入力の2 乗積分を任意に小さくできるNCVEと呼ばれる性質をもつ。本研究では，元の非線形方程式の周期解を利用した相対軌道移行においても、NCVEを利用した設計が有効であることを示す。, Initial conditions of the nonlinear relative dynamics along a circular orbit, which yield periodic solutions, are characterized, and a formation problem based on them is formulated. Using the property of null controllability with vanishing energy of the Hill-Clohessy-Wiltshire equations, L1 suboptimal feedback controllers are designed. By simulation results, the effectiveness of the designed controllers are illustrated., 形態: カラー図版あり, Physical characteristics: Original contains color illustrations, 資料番号: AA0064733041},
 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 = {円軌道近傍の周期軌道間の移行},
 volume = {2008},
 year = {2009}
}