@inproceedings{oai:jaxa.repo.nii.ac.jp:00007520,
 author = {成田, 伸一郎 and 太刀川, 純孝 and 森田, 泰弘 and 広川, 英治 and Narita, Shinichiro and Tachikawa, Sumitaka and Morita, Yasuhiro and Hirokawa, Eiji},
 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 = {スピン型飛翔体の姿勢決定において、太陽角を高精度かつ広視野で検出することが要求される。一方で、高信頼性を確保するためミッション要求に合わせて簡易なシステム構成とすることが要求される。今回視野120度、精度0.5度のセンサと共に、動作確認を行う姿勢決定地上システムを開発し、M-V-8号機飛翔試験を通して動作確認を行った。その結果を報告する。, In the case of spinning spacecraft attitude determination, detection of sun angle in high resolution and wide field of view is needed. We have developed the Rocket Sun Aspect Sensor (RSAS) with a field of view of 128 degree and resolution of 0.5 degree. Furthermore, in order attitude determination of the spacecraft, two reference vectors and angles between the reference objects and spacecraft are needed, for example, sun and geomagnetic angle. Therefore, we developed the attitude determination system on the ground and software to receive rocket telemetry data, and calculate sun and geomagnetic angle. In this flight test, we verified the motion of RSAS and this attitude determination system by M-V-8 launch., 資料番号: AA0063481019},
 pages = {107--110},
 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 = {Flight test of rocket sun aspect sensor and attitude determination system on the ground by M-V-8 launch},
 year = {2007}
}