@inproceedings{oai:jaxa.repo.nii.ac.jp:00007411,
 author = {山田, 克彦 and 島, 岳也 and 吉河, 章二 and Yamada, Katsuhiko and Shima, Takeya and Yoshikawa, Shoji},
 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, フォーメーションフライトの相対位置を高精度に制御する方法を考察する．もっとも簡単なアロングトラック方向に一定距離だけ離れた2 機の衛星のフォーメーションフライトを対象に，外乱としてJ2項や空力項を考えて，両者の相対位置制御精度と制御入力の関係を導く．, Position control of precise formation flying is considered in this paper. We focus on a simple case where the distance between two spacecraft is constant in the along-track direction. Major perturbations such as the J2 gravitational perturbation and the atmospheric drag are taken into account, and the control performance to maintain the relative position between the two spacecraft is analyzed. Numerical simulations are executed to validate the analytical results., 形態: カラー図版あり, Physical characteristics: Original contains color illustrations, 資料番号: AA0064733037},
 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 = {精密フォーメーションフライトの相対位置制御},
 volume = {2008},
 year = {2009}
}