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Optimization of three axis control of two wheel satellite with initial angular momentum
https://jaxa.repo.nii.ac.jp/records/7612
https://jaxa.repo.nii.ac.jp/records/761269923d1a-585f-4fea-b7c6-cd7d6b679bce
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 | Optimization of three axis control of two wheel satellite with initial angular momentum | |||||
言語 | ||||||
言語 | eng | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 姿勢制御 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 姿勢安定性 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | ホイール衛星 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | リアクションホイール | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | バイアスモーメンタム衛星 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 衛星制御 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 最適制御 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 角運動量 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | ニューテーション | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 角速度 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 制御則 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 最小エネルギー軌道 | |||||
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 | attitude control | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | attitude stability | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | wheel satellite | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | reaction wheel | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | bias momentum satellite | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | satellite control | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | optimal control | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | angular momentum | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | nutation | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | angular velocity | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | control law | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | minimum energy trajectory | |||||
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 | 初期角運動量を持つ衛星の2ホイールによる最小エネルギー姿勢変更 | |||||
著者 |
遠藤, 達也
× 遠藤, 達也× Endo, Tatsuya |
|||||
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. 296-299, 発行日 2006-03 |
|||||
抄録 | ||||||
内容記述タイプ | Abstract | |||||
内容記述 | 筆者らはこれまでに、2ホイール衛星の姿勢変更について、エネルギ最小制御則を議論してきた。これらは、姿勢変更をホイールの存在しない軸周りの姿勢変更に限定して検討を行ってきた。本論では、3軸の慣性モーメント比が2軸対称、1軸非対称の初期角運動量を持つ衛星(バイアスモーメンタム衛星を含む)の3軸姿勢制御について角運動量保存の観点から安定化可能な姿勢について議論するため、数値最適解をニューテーション周期と比較した。結果、最適解とニューテーション周期の相関は見られなかった。 | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Authors have been discussing the energy minimum control low about the satellite maneuver with only two reaction wheel. The maneuver is limited around the axis where the wheel doesn't exist and these have been being examined. This paper discuss about the energy minimum control low of satellite having initial angular momentum. That is included the bias momentum satellite. The satellite's moment of inertia is axisymmetric. The attitude stability of satellite on three-axis pointing control is discussed from the point of angular momentum preservation rule. Moreover, a numerical solution is compared with the Nutation cycle. | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA0063480047 |