@inproceedings{oai:jaxa.repo.nii.ac.jp:00007503,
 author = {永井, 将貴 and 中須賀, 真一 and Nagai, Masaki and Nakasuka, Shinichi},
 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 = {衛星の小型化、高性能化が進む中、編隊飛行、母衛星監視飛行といった衛星協調ミッションが注目されている。そこで相対位置制御技術が必要となるが、その燃料消費が衛星重量やコスト、寿命に関わる重大な問題となっている。本研究では、特に衛星編隊に影響の大きいJ2摂動のみに注目し、任意の編隊形状に対して、必要な最小ΔVを数学的・理論的に算出した。編隊形状と理論的最小必要燃料との関係を導出できたことで、編隊形状に応じた衛星群アプリケーションの性能が分かれば、性能と消費燃料とのトレードオフ設計ができるようになる。, The technology of formation flying has great potential for the future of space engineering: unlimited formation size, flexibility of functions, reduced cost, easy system upgrade and so on. However the oblateness of the earth, the J2 effect, causes deterioration of formation shape. In order to keep the shape of a formation, which is usually necessary to accomplish missions, formation keeping control has to be done. This control should be efficient to minimize fuel consumption. This paper focuses on only J2 perturbation effect on satellites, and discusses theoretically how much fuel we need to keep formations. Once you know the fuel consumption dependent on certain parameters, you can design the parameters to reduce the fuel consumption as much as possible under your mission requirements. The purpose of this paper is to make a guideline for designing efficient formation., 資料番号: AA0063481002},
 pages = {7--12},
 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 = {Theoretical equation of minimal fuel consumption for satellites' formation keeping control under J2 perturbation},
 year = {2007}
}