| Item type |
紀要論文 / Departmental Bulletin Paper(1) |
| 公開日 |
2015-03-26 |
| タイトル |
|
|
タイトル |
Trajectory Program for Interplanetary Missions |
|
言語 |
en |
| 言語 |
|
|
言語 |
eng |
| 資源タイプ |
|
|
資源タイプ識別子 |
http://purl.org/coar/resource_type/c_6501 |
|
資源タイプ |
departmental bulletin paper |
| その他のタイトル |
|
|
その他のタイトル |
惑星間軌道生成プログラム |
| 著者 |
西村, 敏充
松尾, 弘毅
加藤, 隆二
三上, 龍男
NISHIMURA, Toshimitsu
MATSUO, Hiroki
KATO, Takaji
MIKAMI, Tatsuo
|
| 著者所属 |
|
|
|
富士通株式会社 |
| 著者所属 |
|
|
|
富士通株式会社 |
| 出版者 |
|
|
出版者 |
宇宙科学研究所 |
| 書誌情報 |
宇宙科学研究所報告
巻 14,
p. 1-49,
発行日 1983-07
|
| 抄録（英） |
|
|
内容記述タイプ |
Other |
|
内容記述 |
The Planet-A and MS-T5 missions are the first deep-space missions not only for ISAS, but also for Japan. Escaping the gravity field of the Earth, the spacecrafts travel around the Sun for 8 months for the former and 14 months for the latter until the encounter with Halley's comet. During these periods, ISAS is planning to perform its own tracking using the 64 mφ antenna which is under construction at Usuda, Nagano prefecture. For this purpose, precise trajectory of the spacecrafts must be computed, taking into account all the accelerations such as gravity of Sun, Moon, 9 planets, solar pressure, general relativity effect, etc. A large scale software called TRIP has been developed based on such mathematical model, taking advantage of the advanced numerical integration techniques and the basic concept as well as the software structre are described in this report. |
| ISSN |
|
|
収録物識別子タイプ |
ISSN |
|
収録物識別子 |
0285-2853 |
| 書誌レコードID |
|
|
収録物識別子タイプ |
NCID |
|
収録物識別子 |
AN00354474 |
| 資料番号 |
|
|
内容記述タイプ |
Other |
|
内容記述 |
資料番号: SA0166004000 |
SA0166004.pdf (2.0 MB)
