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次世代型宇宙輸送機の機体設計と飛行経路の統合的最適化
https://jaxa.repo.nii.ac.jp/records/17370
https://jaxa.repo.nii.ac.jp/records/1737041a3e605-290f-4f09-8332-eff2648f4198
Item type | 会議発表論文 / Conference Paper(1) | |||||
---|---|---|---|---|---|---|
公開日 | 2015-03-26 | |||||
タイトル | ||||||
タイトル | 次世代型宇宙輸送機の機体設計と飛行経路の統合的最適化 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 最適化 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 機体設計 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | スペースプレーン | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 宇宙輸送系 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 遺伝的アルゴリズム | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | Runge-Kutta法 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 空気吸込み式エンジン | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | SSTO宇宙機 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 研究開発 | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | optimization | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | airframe design | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | spaceplane | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | space transportation system | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | genetic algorithm | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Runge-Kutta method | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | air breathing engine | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | SSTO vehicle | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | research and development | |||||
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(英) | ||||||
その他のタイトル | Integrated optimization of airframe design and flight trajectory for advanced space transportation vehicle | |||||
著者 |
本橋, 和宏
× 本橋, 和宏× 関, 建× 山口, 雄仁× 吉田, 洋明× 石川, 芳男× Motohashi, Kazuhiro× Seki, Takeshi× Yamaguchi, Katsuhito× Yoshida, Hiroaki× Ishikawa, Yoshio |
|||||
著者所属 | ||||||
日本大学 大学院理工学研究科 | ||||||
著者所属 | ||||||
日本大学 大学院理工学研究科 | ||||||
著者所属 | ||||||
日本大学 短期大学部 | ||||||
著者所属 | ||||||
日本大学 理工学部 | ||||||
著者所属 | ||||||
日本大学 理工学部 | ||||||
著者所属(英) | ||||||
en | ||||||
Nihon University Graduate School of Science and Technology | ||||||
著者所属(英) | ||||||
en | ||||||
Nihon University Graduate School of Science and Technology | ||||||
著者所属(英) | ||||||
en | ||||||
Nihon University Junior College | ||||||
著者所属(英) | ||||||
en | ||||||
Nihon University College of Science and Technology | ||||||
著者所属(英) | ||||||
en | ||||||
Nihon University College of Science and Technology | ||||||
書誌情報 |
宇宙輸送シンポジウム 平成14年度 en : Proceedings of Space Transportation Symposium FY2002 p. 137-140, 発行日 2003-04 |
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抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | It has been attempted to develop a multidisciplinary design optimization tool for a large-scale system using Genetic Algorithm (GA), and to apply this results of the latest calculation for the problem above obtained by the developed tool showed that airframes (solutions) converged on four areas in the solution space and sensitivity of design variables of the airframe shape was remarkably different in each convergence area. Although high-ranking solutions having good value of the performance index have various airframe configurations, those flight trajectories hardly changed. The best solution showed that it is necessary to reduce the weight of airframe components and to improve the performance of air-breathing engine for realizing a feasible airframe size. It is suggested that this tool is absolutely useful for searching a solution at the conceptual designing phase of a spaceplane. | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA0045426034 |