地球の人工衛星の運動におよぼす微小な推力の影響に関する研究

Material type: 文書・図像類

Author: 武内, 澄夫ほか

Publisher: 航空宇宙技術研究所

Publication date: 1982-11

Material Format: Digital

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Note (General)：: Perturbative effects of small thrust on the motion of an artificial earth satellite are investigated. The Lagrange planetary equations in Gaussian for...

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Material Type: 文書・図像類
Title: 地球の人工衛星の運動におよぼす微小な推力の影響に関する研究
Author/Editor: 武内, 澄夫
TAKEUCHI, Sumio
Author Heading: 武内, 澄夫
TAKEUCHI, Sumio
Publication, Distribution, etc.: 航空宇宙技術研究所
Publication Date: 1982-11
Publication Date (W3CDTF): 1982-11
Alternative Title: EFFECTS OF SMALL THRUST ON THE MOTION OF AN ARTIFICIAL EARTH SATELLITE
Periodical title: 航空宇宙技術研究所報告 = Technical Report of National Aerospace Laboratory TR-744
No. or year of volume/issue: 744
Volume: 744
Pages: 19-
ISSN (Periodical Title): ISSN : 0389-4010
Text Language Code: jpn
Target Audience: 一般
Note (General): Perturbative effects of small thrust on the motion of an artificial earth satellite are investigated. The Lagrange planetary equations in Gaussian form are applied to determine the variations of the orbital elements. Also, equations of motion expressed in terms of different components of the thrust acceleration are used. It is assumed that the small thrust acceleration is a function of time and expressible as a linear combination of a polynomial and a composite set of all sines and cosines. By the method of linear perturbations the equations are solved and the perturbative effects on satellite orbital elements are obtained. The terms in variations of orbital elements are of three types. They are purely secular, periodic and mixed secular types. Considering the gravitational disturbing function of the earth and the luni-solar disturbing function to deal with the combined effect, the theory is applied to the orbit of the geostationary satellite. Then the variations of orbital elements, the longitude, the latitude and the height based on the standard earth-ellipsoid are calculated. In addition there is a discussion of the method of determining the components of the thrust that maintains the longitude and the latitude of the satellite within a given tolerance band about a prespecified station.
資料番号: NALTR0744000
レポート番号: NAL TR-744
Access Restrictions: 限定公開
Data Provider (Database): 国立情報学研究所 : 学術機関リポジトリデータベース（IRDB）（機関リポジトリ）
https://irdb.nii.ac.jp
Original Data Provider (Database): 宇宙航空研究開発機構 : 宇宙航空研究開発機構リポジトリ