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Design of reference Lissajous trajectories around the L2 point in the Sun-Earth system
https://jaxa.repo.nii.ac.jp/records/7566
https://jaxa.repo.nii.ac.jp/records/7566fcdedd05-ae4c-4105-9d0e-47a8834ee1fd
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 | Design of reference Lissajous trajectories around the L2 point in the Sun-Earth system | |||||
言語 | ||||||
言語 | eng | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | リサジュ基準軌道 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 軌道解析 | |||||
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 | ラグランジュ平衡点 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 逐次2次計画法 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | SQP | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | L2点 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 軌道 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 2次計画法 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 3体問題 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 軌道決定 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 摂動 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 拘束条件 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 軌道 | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | reference Lissajous trajectory | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | trajectory analysis | |||||
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 | Lagrangian equilibrium point | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | sequential quadratic programming | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | SQP | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | L2 point | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | trajectory | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | quadratic programming | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | three body problem | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | orbit determination | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | perturbation | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | constraint | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | trajectory | |||||
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 | |||||
その他のタイトル | ||||||
その他のタイトル | 太陽-地球系L2点周りのリサジュ基準軌道の設計 | |||||
著者 |
歌島, 昌由
× 歌島, 昌由× Utashima, Masayoshi |
|||||
著者所属 | ||||||
宇宙航空研究開発機構 総合技術研究本部 | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency Institute of Space Technology and Aeronautics | ||||||
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. 1-6, 発行日 2006-03 |
|||||
抄録 | ||||||
内容記述タイプ | Abstract | |||||
内容記述 | リサジュ軌道やハロー軌道は不安定なために数ヶ月間隔の軌道保持制御が必須であり、正確な摂動モデルの下でΔVゼロの基準軌道を前もって設計しておき、それに追従する様に保持制御が行なわれている。欧米では、3次以上の高次解析解を初期値として基準軌道が作成されているが、本論文では、線型解だけを使用してリサジュ基準軌道を作成する新しい方法を述べる。 | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Since both Lissajous and halo orbits are unstable, orbital maintenance maneuvers at several month intervals are necessary. In order to perform orbital maintenance, a reference trajectory with zero Delta V is designed in advance under a precise model of perturbations. Orbital maintenance maneuvers are then performed such that the reference orbit is maintained. In Europe and the United States, a third- or higher-order analytical solution is used as an initial trajectory for obtaining a reference orbit. In this paper, we present a new method for reference Lissajous orbits which does not need higher-order solutions. | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA0063480001 |