{"created":"2023-06-20T15:09:06.463095+00:00","id":38614,"links":{},"metadata":{"_buckets":{"deposit":"2f501818-8125-45a6-b91d-35f8096910c5"},"_deposit":{"created_by":1,"id":"38614","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"38614"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00038614","sets":["1887:1891"]},"author_link":["434946","434944","434942","434943","434947","434945"],"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2013-10","bibliographicIssueDateType":"Issued"},"bibliographic_titles":[{"bibliographic_title":"第57回宇宙科学技術連合講演会講演集"},{"bibliographic_title":"Proceedings of 57th Space Sciences and Technology Conference","bibliographic_titleLang":"en"}]}]},"item_5_description_14":{"attribute_name":"会議概要（会議名, 開催地, 会期, 主催者等）","attribute_value_mlt":[{"subitem_description":"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","subitem_description_type":"Other"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"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.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AC1400030000","subitem_description_type":"Other"}]},"item_5_description_33":{"attribute_name":"レポート番号","attribute_value_mlt":[{"subitem_description":"レポート番号: JSASS-2013-4109","subitem_description_type":"Other"}]},"item_5_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"日本航空宇宙学会(JSASS)"}]},"item_5_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"The Japan Society for Aeronautical and Space Sciences(JSASS)"}]},"item_5_rights_28":{"attribute_name":"権利","attribute_value_mlt":[{"subitem_rights":"(C)2013 一般社団法人 日本航空宇宙学会"}]},"item_5_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"三菱スペース・ソフトウエア株式会社"},{"subitem_text_value":"三菱スペース・ソフトウエア株式会社"},{"subitem_text_value":"宇宙航空研究開発機構(JAXA)"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Mitsubishi Space Software Co.,Ltd"},{"subitem_text_language":"en","subitem_text_value":"Mitsubishi Space Software Co.,Ltd"},{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency(JAXA)"}]},"item_5_version_type_30":{"attribute_name":"著者版フラグ","attribute_value_mlt":[{"subitem_version_resource":"http://purl.org/coar/version/c_970fb48d4fbd8a85","subitem_version_type":"VoR"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"服部, 和恵"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"林, 健太郎"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"横田, 清美"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Hattori, Kazue","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Hyashi, Kentaroh","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Yokota, Kiyomi","creatorNameLang":"en"}],"nameIdentifiers":[{}]}]},"item_files":{"attribute_name":"ファイル情報","attribute_type":"file","attribute_value_mlt":[{"accessrole":"open_date","date":[{"dateType":"Available","dateValue":"2020-01-24"}],"displaytype":"detail","filename":"AC1400030.pdf","filesize":[{"value":"566.4 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"AC1400030.pdf","url":"https://jaxa.repo.nii.ac.jp/record/38614/files/AC1400030.pdf"},"version_id":"afc72b7c-a44a-4706-b341-c783b1e7c7c1"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"Launch Vehicle; Endoatomospheric Guidance; H-3","subitem_subject_language":"en","subitem_subject_scheme":"Other"}]},"item_language":{"attribute_name":"言語","attribute_value_mlt":[{"subitem_language":"jpn"}]},"item_resource_type":{"attribute_name":"資源タイプ","attribute_value_mlt":[{"resourcetype":"conference paper","resourceuri":"http://purl.org/coar/resource_type/c_5794"}]},"item_title":"次期基幹ロケットを想定した大気中誘導の検討","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"次期基幹ロケットを想定した大気中誘導の検討"}]},"item_type_id":"5","owner":"1","path":["1891"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"38614","relation_version_is_last":true,"title":["次期基幹ロケットを想定した大気中誘導の検討"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T22:38:24.603336+00:00"}