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Analysis of high-frequency oscillations on infrared astrometric nano-class satellite, Nano-JASMINE
https://jaxa.repo.nii.ac.jp/records/7631
https://jaxa.repo.nii.ac.jp/records/76313cac3f9c-8350-445c-af22-e70a5d5ce163
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 | Analysis of high-frequency oscillations on infrared astrometric nano-class satellite, Nano-JASMINE | |||||
言語 | ||||||
言語 | eng | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | Nano-JASMINE | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | ナノ衛星 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 天文衛星 | |||||
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 | 柔軟体 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 曲げ | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | ヒンジ | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 構造振動 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 柔軟多様体システム | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | フッカーの方法 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 数学モデル | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 運動方程式 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 計算機シミュレーション | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Nano-JASMINE | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | nanosatellite | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | astronomical satellite | |||||
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 | flexible body | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | bending | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | hinge | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | structural oscillation | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | flexible multi-body system | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Hooker's method | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | mathematical model | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | equation of motion | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | computerized simulation | |||||
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 | 超小型赤外線位置天文衛星Nano-JASMINEにおける、高精度姿勢安定の研究 | |||||
著者 |
小野, 雅裕
× 小野, 雅裕× 中須賀, 真一× Ono, Masahiro× Nakasuka, Shinichi |
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著者所属 | ||||||
東京大学 | ||||||
著者所属 | ||||||
東京大学 | ||||||
著者所属(英) | ||||||
en | ||||||
University of Tokyo | ||||||
著者所属(英) | ||||||
en | ||||||
University of Tokyo | ||||||
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. 424-428, 発行日 2006-03 |
|||||
抄録 | ||||||
内容記述タイプ | Abstract | |||||
内容記述 | 本研究では、ガタを含む柔軟多体システムのモデルの定式化を行い、超小型衛星に発生する振動を解析した。その結果は、東京大学中須賀研究室および国立天文台が計画している超小型赤外線位置天文観測衛星プロジェクトNano-JASMINE(Japan Astrometry Satellite Mission for Infrared Exploration)における、姿勢安定性の面での実行可能性分析に用いられた。本論文では、先ず、Nano-JASMINEプロジェクトにおける実現可能性分析において、ガタを含む柔軟多体システムのモデルの定式化が必要となった背景を説明する。次いで、定式化の方法を説明し、最後に得られたモデルを用いた振動のシミュレーションの結果を述べる。 | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | The flexible multi-body system model combined with the model of backlash was formulated in this study. Using the model the oscillation on the nano-class satellite was simulated. The result of the simulation was used for the feasibility analysis of the nano-class astrometric satellite project Nano-JASMINE (Japan Astrometry Satellite Mission for Infrared Exploration) in terms of its attitude stability. The first part of this paper explains the necessity of the flexible multi-body system model and the model of backlash for the feasibility analysis of Nano-JASMINE mission. The second part describes the formulation the model. The third part shows the result of the oscillation analysis in Nano-JASMINE. | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA0063480066 |