@inproceedings{oai:jaxa.repo.nii.ac.jp:00007294,
 author = {Yaglioglu, Burak and Wang, Jihe},
 book = {アストロダイナミクスシンポジウム講演後刷り集, The 20th Workshop on JAXA Astrodynamics and Flight Mechanics},
 month = {Mar},
 note = {第20回アストロダイナミクスシンポジウム (2010年7月26-27日. 宇宙航空研究開発機構宇宙科学研究所), 相模原市, 神奈川県, The 20th Workshop on JAXA Astrodynamics and Flight Mechanics 2010 (July 26-27, 2010. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS)), Sagamihara, Kanagawa Japan, Slightly different from the commonly used term formation flying, cluster flying requires less control effort but a collision free orbit design for a multiple satellite configuration. In addition, fractionating a spacecraft and letting the different subsystems fly separately leads to the cluster flying design with the constraints of inter-satellite distances and visibility due to inter-satellite power transfer link requirement. In this manner, parallel separation of eccentricity and inclination vector method was used to design collision free relative orbits for a network of more than two satellites. Based on this method, three configurations were identified in terms of safety, visibility and combination of those. In this orbit design study, the optimization and evaluations of these configurations were presented. It was concluded that a safe, fuel efficient and close proximity cluster flying can be realized for a fractionated spacecraft with respect to a given set of constraints., 形態: カラー図版あり, Physical characteristics: Original contains color illustrations, 資料番号: AA0065115047},
 pages = {284--301},
 publisher = {宇宙航空研究開発機構宇宙科学研究所 (JAXA)(ISAS), Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS)},
 title = {Cluster Flying Configuration Evaluation in the Case of Fractionated Spacecraft Architecture},
 volume = {20},
 year = {2011}
}