@inproceedings{oai:jaxa.repo.nii.ac.jp:00005896,
 author = {小川, 美奈 and 岩名, 泰典 and 谷口, 正 and 中嶋, 憲 and 堀田, 学 and 広田, 正夫 and Ogawa, Mina and Iwana, Yasunori and Taniguchi, Sho and Nakajima, Ken and Hotta, Manabu and Hirota, Masao},
 book = {宇宙航空研究開発機構特別資料: 先進的軌道計測・決定技術に関する研究会論文集, JAXA Special Publication: Proceedings of Advanced Orbit Measurement and Orbit Calculation Technologies},
 month = {Mar},
 note = {The Real Time Trajectory Estimation Program (RTEP) is JAXA's system for estimating a satellite's trajectory and thrust acceleration based on the Kalman filter during the Apogee Engine Firing (AEF). RTEP has been used during the AEFs of, ETS (Engineering Test Satellite)-6 (1994), COMETS (Communications and broadcasting Engineering Test Satellite) (1998), DRTS (Data Relay Test Satellite) (2002), OICETS (Optical Inter-orbit Communications Engineering Test Satellite) (2005) and ALOS (Advanced Land Observing Satellite) (2006). This paper presents the overview of RTEP, the results of the estimation using Space network data., 資料番号: AA0063223010, レポート番号: JAXA-SP-06-015},
 pages = {59--68},
 publisher = {宇宙航空研究開発機構, Japan Aerospace Exploration Agency (JAXA)},
 title = {地球周回衛星の実時間軌道推定:概要と成果},
 volume = {JAXA-SP-06-015},
 year = {2007}
}