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静止衛星の軌道保持シミュレーションシステムの構成(Ⅰ): 地球の重力場による摂動
https://jaxa.repo.nii.ac.jp/records/43790
https://jaxa.repo.nii.ac.jp/records/437902da13ecc-b9ad-483a-9410-191186825d45
名前 / ファイル | ライセンス | アクション |
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naltm00206.pdf (1.6 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 | 静止衛星の軌道保持シミュレーションシステムの構成(Ⅰ): 地球の重力場による摂動 | |||||
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 | The Composition of Station-keeping Simulation Systems of Synchronous Satellite(I) - Perturbations due to the asphericity of the earth- | |||||
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 | ||||||
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資料 en : Technical Memorandum of National Aerospace Laboratory 巻 206, p. 33, 発行日 1971-08 |
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抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | This report describes the formulation of the disturbing motion of a synchronous satellite due to the asphericity of the earth. Accurate and efficient calculations of the ephemeris of a satellite about its primary body are essential with respect to the simulation of orbit control, so gravity potential was considered to the third order, and planetary equations which determine the osculating elements were integrated analytically by successive approximations. These results have been found to simulate the motion of Syncom H to a high degree of accuracy. Since they do not require long computation time, they are very useful for a longtime simulation of station-keeping systems. | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 0452-2982 | |||||
書誌レコードID | ||||||
収録物識別子タイプ | NCID | |||||
収録物識別子 | AN00314334 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: NALTM0206000 | |||||
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 TM-206 |