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Orbit design and simulation for ASTROD 1 for the 2012 and 2013 launch windows
https://jaxa.repo.nii.ac.jp/records/7580
https://jaxa.repo.nii.ac.jp/records/7580e950cd19-0191-429c-999b-70d5d26c8f44
Item type | 会議発表論文 / Conference Paper(1) | |||||
---|---|---|---|---|---|---|
公開日 | 2015-03-26 | |||||
タイトル | ||||||
言語 | en | |||||
タイトル | Orbit design and simulation for ASTROD 1 for the 2012 and 2013 launch windows | |||||
言語 | ||||||
言語 | eng | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | ASTROD 1 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 軌道計算 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 衛星軌道 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 中国宇宙プログラム | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 打上げウィンドウ | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 金星 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 太陽軌道 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | フライバイミッション | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 測距 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 軌道 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | シミュレーション | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | シャピロ効果 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 相対論的パラメータ | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | ASTROD 1 | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | orbit calculation | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | satellite orbit | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Chinese space program | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | launch window | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Venus | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | solar orbit | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | flyby mission | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | rangefinding | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | orbit | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | simulation | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Shapiro effect | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | relativistic parameter | |||||
資源タイプ | ||||||
資源タイプ識別子 | http://purl.org/coar/resource_type/c_5794 | |||||
資源タイプ | conference paper | |||||
アクセス権 | ||||||
アクセス権 | metadata only access | |||||
アクセス権URI | http://purl.org/coar/access_right/c_14cb | |||||
著者 |
Xia, Yan
× Xia, Yan× Li, Guangyu× Ni, Wei-Tou |
|||||
著者所属 | ||||||
Chinese Academy of Sciences Purple Mountain Observatory | ||||||
著者所属 | ||||||
Chinese Academy of Sciences Purple Mountain Observatory | ||||||
著者所属 | ||||||
Chinese Academy of Sciences Purple Mountain Observatory | ||||||
著者所属(英) | ||||||
en | ||||||
Chinese Academy of Sciences Purple Mountain Observatory | ||||||
著者所属(英) | ||||||
en | ||||||
Chinese Academy of Sciences Purple Mountain Observatory | ||||||
著者所属(英) | ||||||
en | ||||||
Chinese Academy of Sciences Purple Mountain Observatory | ||||||
出版者 | ||||||
出版者 | 宇宙航空研究開発機構宇宙科学研究本部 | |||||
出版者(英) | ||||||
出版者 | Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA/ISAS) | |||||
書誌情報 |
第15回アストロダイナミクスシンポジウム講演後刷り集 2005 en : Proceedings of 15th Workshop on JAXA Astrodynamics and Flight Mechanics p. 92-99, 発行日 2006-03 |
|||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | ASTROD 1 (Astrodynamical Space Test of Relativity using Optical Devices 1) is to have one spacecraft launched to a solar orbit to range optically with ground stations to meet important scientific goals. The spacecraft is designed to enter the solar orbit from a low earth-orbit and to encounter Venus twice to receive gravity-assistance for achieving shorter periods for making the relativistic Shapiro time delay sooner. In this paper, we first present the orbit design for the 2012 and 2013 launch windows based on our previous method of the 2008 and 2010 orbit design. With a simple noise model, we then present our orbit simulation for the 2012 orbit using 25 parameters of relativistic parameters, celestial-body masses, solar quadrupole parameter, and spacecraft initial position and velocity parameters. We generate five hundred sets of simulated orbit data. From these simulation data, we estimate the uncertainties of the determination of the relativistic parameters gamma and beta to be about 10(exp -7). The uncertainties of other parameters and masses of the celestial bodies including the three big asteroids can be improved considerably. | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA0063480015 |