{"created":"2023-06-20T14:35:35.336248+00:00","id":1828,"links":{},"metadata":{"_buckets":{"deposit":"35d6dd42-d34e-44e9-86e6-398bebc1b586"},"_deposit":{"created_by":1,"id":"1828","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"1828"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00001828","sets":["1887:1893","9:10:25:33"]},"author_link":["476133","476135","476137","476138","476136","476132","476131","476134"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Report on the Flight Simulation Model of Flight Demonstration of Low Sonic Boom Design Concept Phase II (D-SEND#2)"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2018-01-22","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"165","bibliographicPageStart":"1","bibliographicVolumeNumber":"JAXA-RR-17-006","bibliographic_titles":[{"bibliographic_title":"宇宙航空研究開発機構研究開発報告"},{"bibliographic_title":"JAXA Research and Development Report","bibliographic_titleLang":"en"}]}]},"item_3_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"本稿では低ソニックブーム設計概念実証フェーズ2（D-SEND#2）の誘導制御則の設計ならびに評価に用いるための 6 自由度非線形飛行シミュレーション環境の構築に必要となる各種数学モデルをまとめる. また目標としたブーム計測システムにおけるブーム計測条件の評価に用いるためのブーム伝播解析とモンテカルロシミュレーション（MCS）による誘導制御則のロバスト性解析で使用する各種誤差モデルと評価基準についても詳述する.","subitem_description_type":"Abstract"}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"This report provides a comprehensive set of information on the mathematical models necessary to develop a six-degree-of-freedom nonlinear flight simulation code for the design and evaluation of the guidance and control law for D-SEND#2. This paper also elaborates the sonic boom propagation model to evaluate sonic boom measurement condition at the target boom measurement system and provides a list of modeling error data and evaluation criteria for robustness analysis of the guidance and control law using Monte Carlo simulation (MCS).","subitem_description_type":"Other"}]},"item_3_description_18":{"attribute_name":"内容記述","attribute_value_mlt":[{"subitem_description":"形態: カラー図版あり","subitem_description_type":"Other"}]},"item_3_description_19":{"attribute_name":"内容記述（英）","attribute_value_mlt":[{"subitem_description":"Physical characteristics: Original contains color illustrations","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA1730014000","subitem_description_type":"Other"}]},"item_3_description_33":{"attribute_name":"レポート番号","attribute_value_mlt":[{"subitem_description":"レポート番号: JAXA-RR-17-006","subitem_description_type":"Other"}]},"item_3_identifier_registration":{"attribute_name":"ID登録","attribute_value_mlt":[{"subitem_identifier_reg_text":"10.20637/JAXA-RR-17-006/0001","subitem_identifier_reg_type":"JaLC"}]},"item_3_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"宇宙航空研究開発機構(JAXA)"}]},"item_3_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"Japan Aerospace Exploration Agency (JAXA)"}]},"item_3_source_id_22":{"attribute_name":"ISSNONLINE","attribute_value_mlt":[{"subitem_source_identifier":"2433-2216","subitem_source_identifier_type":"ISSN"}]},"item_3_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"宇宙航空研究開発機構航空技術部門飛行技術研究ユニット(JAXA)"},{"subitem_text_value":"宇宙航空研究開発機構研究開発部門第一研究ユニット(JAXA)"},{"subitem_text_value":"宇宙航空研究開発機構航空技術部門飛行技術研究ユニット(JAXA)"},{"subitem_text_value":"宇宙航空研究開発機構航空技術部門飛行技術研究ユニット(JAXA)"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Flight Research Unit, Aeronautical Technology Directorate, Japan Aerospace Exploration Agency (JAXA)"},{"subitem_text_language":"en","subitem_text_value":"Research Unit I, Research and Development Directorate, Japan Aerospace Exploration Agency (JAXA)"},{"subitem_text_language":"en","subitem_text_value":"Flight Research Unit, Aeronautical Technology Directorate, Japan Aerospace Exploration Agency (JAXA)"},{"subitem_text_language":"en","subitem_text_value":"Flight Research Unit, Aeronautical Technology Directorate, Japan Aerospace Exploration Agency (JAXA)"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"川口, 純一郎"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"鈴木, 広一"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"二宮, 哲次郎"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"冨田, 博史"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kawaguchi, Junichiro","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Suzuki, Hirokazu","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Ninomiya, Tetsujiro","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Tomita, Hiroshi","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":"2020-01-31"}],"displaytype":"detail","filename":"AA1730014000.pdf","filesize":[{"value":"8.3 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"AA1730014000.pdf","url":"https://jaxa.repo.nii.ac.jp/record/1828/files/AA1730014000.pdf"},"version_id":"089ea772-daca-4780-b3b3-4dfe6d4fb3d4"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"Supersonic Flight","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Flight Simulation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Guidance and Control","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":"technical report","resourceuri":"http://purl.org/coar/resource_type/c_18gh"}]},"item_title":"低ソニックブーム設計概念実証フェーズ2（D-SEND#2）飛行シミュレーションモデル","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"低ソニックブーム設計概念実証フェーズ2（D-SEND#2）飛行シミュレーションモデル"}]},"item_type_id":"3","owner":"1","path":["33","1893"],"pubdate":{"attribute_name":"公開日","attribute_value":"2018-01-23"},"publish_date":"2018-01-23","publish_status":"0","recid":"1828","relation_version_is_last":true,"title":["低ソニックブーム設計概念実証フェーズ2（D-SEND#2）飛行シミュレーションモデル"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T21:38:26.987923+00:00"}