Item type |
紀要論文 / Departmental Bulletin Paper(1) |
公開日 |
2015-03-26 |
タイトル |
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タイトル |
MUSES-A "飛天"の軌道と軌道決定プログラムISSOP |
言語 |
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言語 |
jpn |
資源タイプ |
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資源タイプ識別子 |
http://purl.org/coar/resource_type/c_6501 |
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資源タイプ |
departmental bulletin paper |
その他のタイトル(英) |
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その他のタイトル |
Tracking of MUSES-A 'HITEN' and description of software packageISSOP for orbit determination |
著者 |
西村, 敏充
市川, 勉
牛越, 淳雄
小坂, 裕
Nishimura, Toshimitsu
Ichikawa, Tsutomu
Ushikoshi, Atsuo
Kosaka, Hiroshi
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出版者 |
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出版者 |
宇宙科学研究所 |
書誌情報 |
宇宙科学研究所報告
巻 70,
p. 1-91,
発行日 1991-03
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抄録(英) |
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内容記述タイプ |
Other |
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内容記述 |
The first Japanese Lunar swing-by spacecraft called 'HITEN' was launched from Uchinoura launching site, located at about 1,500km south-west of Tokyo, respectively on January 25,1990. The four-stage solid propellant boosters called M3SII-V for this purpose. The spacecraft successfully performed first lunar swing-by in March 18,1990. Tracking and orbit determination of the spacecraft have been smoothly carried out throughout this period using Usuda 64 phi antenna. The major hardware modification for Usuda 64m phi antenna is the introduction of X band ranging and range-rate system (down link). As for the range-rate data, higher precision can be expected, at least theoretically, because of higher frequency than S band signals. In preparing for this mission, the software package ISSOP developed for 'SAKIGAKE' and 'SUISEI' mission in 1985 had been modified. The improvements were added to the rejection scheme of poor data, computation of the light-time equation and troposphere and ionosphere correction. In this report the structure and the improvements of ISSOP is first described. Then the result of orbit determination of 'HITEN' is discussed. In the future, this software package will be modified and used 'GEOTAIL' mission in 1992. |
ISSN |
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収録物識別子タイプ |
ISSN |
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収録物識別子 |
0285-2853 |
書誌レコードID |
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収録物識別子タイプ |
NCID |
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収録物識別子 |
AN00354474 |
資料番号 |
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内容記述タイプ |
Other |
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内容記述 |
資料番号: SA0166323000 |