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On relative position control between two spacecraft
https://jaxa.repo.nii.ac.jp/records/7747
https://jaxa.repo.nii.ac.jp/records/7747295f407c-d2bb-41bb-9e7c-d5d0a40d49b0
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 | On relative position control between two spacecraft | |||||
言語 | ||||||
言語 | eng | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 宇宙機軌道 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 編隊飛行 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | フィードバック制御 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 位置制御 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 速度制御 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 燃料消費 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | DOF | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 数値解析 | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | spacecraft trajectory | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | formation flying | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | feedback control | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | position control | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | velocity control | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | fuel consumption | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | DOF | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | numerical analysis | |||||
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 | 宇宙機間の相対位置の制御について | |||||
著者 |
山田, 克彦
× 山田, 克彦× 吉河, 章二× 西山, 岳宏× Yamada, Katsuhiko× Yoshikawa, Shoji× Nishiyama, Takehiro |
|||||
著者所属 | ||||||
三菱電機 | ||||||
著者所属 | ||||||
三菱電機 | ||||||
著者所属 | ||||||
三菱電機 | ||||||
著者所属(英) | ||||||
en | ||||||
Mitsubishi Electric Corporation | ||||||
著者所属(英) | ||||||
en | ||||||
Mitsubishi Electric Corporation | ||||||
著者所属(英) | ||||||
en | ||||||
Mitsubishi Electric Corporation | ||||||
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 |
平成15年度アストロダイナミクスシンポジウム:講演後刷り集 en : ISAS Proceedings of 13th Workshop on Astrodynamics and Flight Mechanics 2003: A Collection of Technical Papers p. 282-289, 発行日 2004-02 |
|||||
抄録 | ||||||
内容記述タイプ | Abstract | |||||
内容記述 | 本稿では2機の宇宙機の編隊飛行制御について検討する。推薬消費が最小となるような相対的な軌道変更軌道をHill方程式に基づいて導出し、そのときの推薬量を求める。また軌道変更軌道を実現するような離散的な2自由度制御則を求める。この制御則はデッドビートの特性を有しており、ゲイン低下に対してロバストである。これらの軌道設計および制御を数値的に検証する。 | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | The formation flight control of two spacecraft is considered in this paper. The trajectory of the relative position change in one spacecraft with respect to the other is designed on the basis of the Hill's equation from the viewpoint of minimum fuel consumption. The total fuel consumed along the trajectory is obtained analytically. Discrete two-degree-of-freedom control law is also proposed in order to realize the designed trajectory. The controller achieves the deadbeat property of the closed loop system and guarantees the robustness to the controller gain decrease. Numerical studies are conducted in order to verify the trajectory generation and the discrete control. | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 0918-8053 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA0046652046 |