@article{oai:jaxa.repo.nii.ac.jp:00032679,
 author = {二宮, 敬虔 and 上杉, 邦憲 and 川口, 淳一郎 and 横田, 博樹 and 村中, 昇 and 滑, 孝和 and 北出, 賢二 and 小笠原, 雅弘 and 木村, 雅文 and 土橋, 雅之 and NINOMIYA, Keiken and UESUGI, Kuninori and KAWAGUCHI, Junichiro and YOKOTA, Hiroki and MURANAKA, Noboru and NAMERA, Takakazu and KITADE, Kenji and OGASAWARA, Masahiro and KIMURA, Masahumi and DOBASHI, Masayuki},
 journal = {宇宙科学研究所報告},
 month = {Mar},
 note = {To support the operation of onboard AOCS (Attitude and Orbit Control System) of "SAKIGAKE" and "SUISEI", ground support software for attitude control and orbit correction was developed. The software, named POPS (PLANET-A AOCS Operation Software), has the function of (1) generating the commands for RCS thruster control and HGA (High Gain Antenna) despin control, (2) simulating spacecraft attitude dynamics to confirm the generated RCS control commands. (3) performing orbit correction analysis to provide the optimum ⊿V-maneuver under various maneuvering constraints, (4) estimating RCS fuel consumption, and (5) conducting the calibration of RCS thrusters. In this paper the functions of POPS are described in detail. The operational results of "SAKIGAKE" and "SUISEI" in orbit are also presented., 資料番号: SA0166110000},
 pages = {1--45},
 title = {"さきがけ(1985-001-A)"および"すいせい(1985-073 A)の姿勢・軌道制御},
 volume = {33},
 year = {1986}
}