@inproceedings{oai:jaxa.repo.nii.ac.jp:00007788,
 author = {張替, 正敏 and 山口, 功 and 葛西, 時雄 and 井川, 寛隆 and 早川, 絢 and Harigae, Masatoshi and Yamaguchi, Isao and Kasai, Tokio and Igawa, Hirotaka and Hayakawa, Jun},
 book = {平成14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 12th Workshop on Astrodynamics and Flight Mechanics 2002: A Collection of Technical Papers},
 month = {Feb},
 note = {本研究はキネマティックGPSを用いて、国際宇宙ステーションのような、大型な柔軟構造物のダイナミクス同定と姿勢変形推定の手法を提案することを目的とする。ダイナミクスに関してはERA法で同定を行い、その結果に基づいてカルマンフィルタを適応し構造物の姿勢変形推定を行う。この手法は、コンピューターシミュレーションおよび地上実験によって評価し、その有効性を確認した。, This paper proposes a method for identifying the modal parameter and estimating attitude and deformation of the large flexible structure such as the International Space Station by kinematic GPS. Eigensystem Realization Algorithm method is used for the modal parameter identification, and for attitude and deformation estimation, the Kalman filter is adopted based on its identified system dynamics. The proposed method was evaluated through the computer simulations and the ground-based experiments, and the results confirmed its feasibility., 資料番号: AA0045497026},
 pages = {153--158},
 publisher = {宇宙科学研究所, The Institute of Space and Astronautical Science (ISAS)},
 title = {Modal parameter identification and attitude and deformation estimation of the flexible structure by GPS},
 year = {2003}
}