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月と太陽の引力の作用下にある地球の人工衛星の運動に関する研究
https://jaxa.repo.nii.ac.jp/records/44569
https://jaxa.repo.nii.ac.jp/records/4456978ae2101-5804-4d99-af0b-51f6094b288c
名前 / ファイル | ライセンス | アクション |
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naltr00323.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 | 月と太陽の引力の作用下にある地球の人工衛星の運動に関する研究 | |||||
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 Study on the Motion of an Artificial Earth Satellite under the Gravitational Attractions of the Sun and Moon | |||||
著者 |
武内, 澄夫
× 武内, 澄夫× 松島, 弘一× TAKEUCHI, Sumio× MATSUSHIMA, Koichi |
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著者所属 | ||||||
航空宇宙技術研究所宇宙研究グループ | ||||||
著者所属 | ||||||
航空宇宙技術研究所宇宙研究グループ | ||||||
著者所属(英) | ||||||
en | ||||||
Space Technology Research Group, National Aerospace Laboratory(NAL) | ||||||
著者所属(英) | ||||||
en | ||||||
Space Technology Research Group, 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-323 巻 323, p. 26, 発行日 1973-07 |
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抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | The effects of the gravitational attractions of the sun and moon on the motion of an artificial earth satellite are investigated using Lagrange’s planetary equations. The complete gravitational disturbing function expressed in osculating elliptic elements is used. As regards the orbital elements of the disturbing body, it is assumed that the semimajor axis, the eccentricity and the inclination of the orbital plane are constants and that the longitude of the ascending node, the argument of the perigee and the mean anomaly are linear functions of time. Neglecting the coupling effects between the oblateness of the earth and the attraction of the disturbing body, perturbations of the first order are determined. The theory is applied to the orbit of a geostationary satellite and the variations of orbirtal elements are calculated. On the basis of the results of computations, the initial conditions giving orbits that have inclination variations amounting to a few degrees for two or three years are determined. | |||||
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: NALTR0323000 | |||||
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-323 |