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自機搭載型軌道保持システムのための軌道決定と制御
https://jaxa.repo.nii.ac.jp/records/44539
https://jaxa.repo.nii.ac.jp/records/445397217b019-e3b6-4a8d-975f-8876c6d7a9d6
名前 / ファイル | ライセンス | アクション |
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naltr00295.pdf (1.3 MB)
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Item type | テクニカルレポート / Technical Report(1) | |||||
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公開日 | 2015-03-26 | |||||
タイトル | ||||||
タイトル | 自機搭載型軌道保持システムのための軌道決定と制御 | |||||
言語 | ||||||
言語 | jpn | |||||
資源タイプ | ||||||
資源タイプ識別子 | http://purl.org/coar/resource_type/c_18gh | |||||
資源タイプ | technical report | |||||
その他のタイトル(英) | ||||||
その他のタイトル | Orbit Determination and Control Methods for Self-contained Station-keeping Systems | |||||
著者 |
松島, 弘一
× 松島, 弘一× MATSUSHIMA, Koichi |
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著者所属 | ||||||
航空宇宙技術研究所計測部 | ||||||
著者所属(英) | ||||||
en | ||||||
Instrumentation and Control Division, National Aerospace Laboratory(NAL) | ||||||
出版者 | ||||||
出版者 | 航空宇宙技術研究所 | |||||
出版者(英) | ||||||
出版者 | National Aerospace Laboratory(NAL) | |||||
書誌情報 |
航空宇宙技術研究所報告 en : Technical Report of National Aerospace Laboratory TR-295 巻 295, p. 21, 発行日 1972-08 |
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抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Orbit determination method for self-contained station-keeping systems, using observational data of only on-board sensors is formulated, and the general equations of motion which determine the motion of a satellite due to control forces in the Earth’s gravitational field is derived from Lagrange’s planetary equations and the mechanism of orbit control is discussed from the dynamical point of view using the equations. Then the effects of the perturbations of the Earth’s gravitational field on the longitudinal drift of synchronous satellite are cleared up and it is showed that the station-keeping of synchronous satellite in the Earth’s gravitational field, having no consideration for the effects of other perturbative forces, result in the control of only two parameters α and L. | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 0389-4010 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: NALTR0295000 | |||||
レポート番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | レポート番号: NAL TR-295 |