@inproceedings{oai:jaxa.repo.nii.ac.jp:00007706, author = {中須賀, 真一 and 津田, 雄一 and 酒匂, 信匡 and Nakasuka, Shinichi and Tsuda, Yuichi and Sako, Nobutada}, book = {平成15年度アストロダイナミクスシンポジウム:講演後刷り集, ISAS Proceedings of 13th Workshop on Astrodynamics and Flight Mechanics 2003: A Collection of Technical Papers}, month = {Feb}, note = {東京大学ISSL(中須賀研究室)の学生チームは、超小型衛星CubeSat-11の開発を行い、2003年6月30日にロシアのロケットROCKOTで成功裡に軌道上に打ち上げた。衛星はその後順調に動作を続け、学生はその上で、予定された様々な実験を実施した。本論文では、CubeSatのコンセプトと意義、東大CubeSat-11の詳細および軌道上での運用成果を述べる。特に軌道推定と姿勢ダイナミクス、画像取得ミッションに焦点を当てる。, Students of University of Tokyo, ISSL (Intelligent Space Systems Laboratory), developed a nano satellite named 'CubeSat-11', which was successfully launched by Russian Rocket 'ROCKOT' on June 30, 2003. The satellite has been working well and the students have been performing various experiments using this satellite. This paper reviews the concept, significance, systems' descriptions of CubeSat-11, and reports the post-launch flight experiment results. Especially, orbit determination and estimation of the satellite attitude will be highlighted. Earth image mission will also be described., 資料番号: AA0046652005}, pages = {23--28}, 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 = {University of Tokyo's CubeSat launch results and its dynamics}, year = {2004} }