@article{oai:jaxa.repo.nii.ac.jp:00022703,
 author = {山元, 透 and 有川, 善久 and 植田, 泰士 and 伊藤, 寛行 and 西田, 義崇 and 鵜川, 晋一 and 水流, 弘達 and 山本, 昌幸 and Yamamoto, Toru and Arikawa, Yoshihisa and Ueda, Yasushi and Itoh, Hiroyuki and Nishida, Yoshitaka and Ukawa, Shinichi and Tsuru, Hiroyoshi and Yamamoto, Masayuki},
 issue = {6},
 journal = {Journal of Guidance, Control, and Dynamics},
 month = {Jun},
 note = {Earth-observation satellites carrying synthetic aperture radar instruments have stringent requirements on control of Earth-referenced repeat-track orbits. This precision control leads to frequent orbital maneuvers, thus burdening daily ground operations. To achieve high accuracy with minimal ground-based workload, we propose a novel autonomous orbit control method that allows both in-plane and out-of-plane maneuvers to be planned and performed autonomously. Furthermore, a maneuver slot concept is proposed to prevent conflicts with payload data-take opportunities. The proposed method has been implemented on the Advanced Land Observing Satellite-2 and has been in practical use since August 2014. This is the first attempt to apply autonomous precision orbit control within a tube-shaped control window for regular operation of an Earth-observation satellite. Details of the proposed method and Advanced Land Observing Satellite-2 flight results are presented in this paper, and experiences and lessons learned from the operation are discussed., 形態: 図版あり, Physical characteristics: Original contains illustrations, 資料番号: PA1610093000},
 pages = {1244--1264},
 title = {Autonomous Precision Orbit Control Considering Observation Planning: ALOS 2 Flight Results},
 volume = {39},
 year = {2016}
}