@inproceedings{oai:jaxa.repo.nii.ac.jp:00007543,
 author = {根田, 康美 and 臼田, 武史 and 相模, 毅 and 尾曲, 邦之 and 柏, 宗孝 and 松永, 三郎 and Konda, Yasumi and Usuda, Takeshi and Sagami, Tsuyoshi and Omagari, Kuniyuki and Kashiwa, Munetaka and Matsunaga, Saburo},
 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 = {現在超小型衛星による、リモートセンシングや天体観測などの高度ミッションが期待されるようになり、姿勢決定制御が必要不可欠となってきている。著者らは超小型衛星に搭載しうる最小限の複合センサシステムによる姿勢決定系、磁気トルカを用いた姿勢制御系を設計し、軌道上での評価を目的として超小型衛星Cute(CUbical Tokyo Tech Engineering satellite)-1.7+APD(Avalanche Photo Diode)に搭載する姿勢制御・決定系の開発を行った。本研究では、設計した姿勢系のシステムを扱い、特徴や各種シミュレーション結果、Cute-1.7+APD2号機に向けた設計方針を述べる。, Today, techniques of attitude determination and control are required for pico-satellite to achieve advanced missions, remote sensing, astronomic observation, and so on. We developed an Attitude determination and control system for Cute (CUbical Tokyo Tech Engineering satellite) -1.7 + APD (Avalanche Photo Diode) was developed to demonstrate its performance on orbit. This system is composed of various sensors and three magnetic torquers. This paper mainly deals with this system, describing its features and the results of simulation and on-orbit experiments. In addition, this ADC system will be improved and used for the follow on satellite, Cute-1.7 + APD 2. The outline of this new design is thus also described., 資料番号: AA0063481042},
 pages = {242--247},
 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 = {Development of attitude determination and control system for pico-satellite Cute-1.7 + APD},
 year = {2007}
}