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次期基幹ロケットを想定した大気中誘導の検討
https://jaxa.repo.nii.ac.jp/records/38614
https://jaxa.repo.nii.ac.jp/records/38614a885f7a6-3615-489b-a1fc-a61ca29c4c48
名前 / ファイル | ライセンス | アクション |
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AC1400030.pdf (566.4 kB)
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Item type | 会議発表論文 / Conference Paper(1) | |||||
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公開日 | 2015-03-26 | |||||
タイトル | ||||||
タイトル | 次期基幹ロケットを想定した大気中誘導の検討 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Launch Vehicle; Endoatomospheric Guidance; H-3 | |||||
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 | |||||
著者 |
服部, 和恵
× 服部, 和恵× 林, 健太郎× 横田, 清美× Hattori, Kazue× Hyashi, Kentaroh× Yokota, Kiyomi |
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著者所属 | ||||||
三菱スペース・ソフトウエア株式会社 | ||||||
著者所属 | ||||||
三菱スペース・ソフトウエア株式会社 | ||||||
著者所属 | ||||||
宇宙航空研究開発機構(JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Mitsubishi Space Software Co.,Ltd | ||||||
著者所属(英) | ||||||
en | ||||||
Mitsubishi Space Software Co.,Ltd | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency(JAXA) | ||||||
出版者 | ||||||
出版者 | 日本航空宇宙学会(JSASS) | |||||
出版者(英) | ||||||
出版者 | The Japan Society for Aeronautical and Space Sciences(JSASS) | |||||
書誌情報 |
第57回宇宙科学技術連合講演会講演集 en : Proceedings of 57th Space Sciences and Technology Conference 発行日 2013-10 |
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会議概要(会議名, 開催地, 会期, 主催者等) | ||||||
内容記述タイプ | Other | |||||
内容記述 | 第57回宇宙科学技術連合講演会(2013年10月9日-11日. 米子コンベンションセンター(BiG SHiP)), 米子市, 鳥取県 | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | The ascent guidance of a launch vehicle is generally applied in exo-atmospheric phase. Japanese next generation launchvehicle, H-3 is considered to fly in atmospheric phase relatively long time compared to current workhorse H-IIA rocket.This means that the first stage guidance duration of H-3 could be shorter than H-IIA, trajectory dispersion be bigger, morepropellant be used. To solve this problem, simplified endo-atmospheric guidance is proposed. This guidance can beapplied in atmospheric phase, and also execution time with on-board computer may well be reasonable. This paperdescribes the proposed guidance and simulation results. | |||||
権利 | ||||||
権利情報 | (C)2013 一般社団法人 日本航空宇宙学会 | |||||
著者版フラグ | ||||||
出版タイプ | VoR | |||||
出版タイプResource | http://purl.org/coar/version/c_970fb48d4fbd8a85 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AC1400030000 | |||||
レポート番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | レポート番号: JSASS-2013-4109 |