{"created":"2023-06-20T14:38:59.894973+00:00","id":5660,"links":{},"metadata":{"_buckets":{"deposit":"9cd2b203-7eb1-480f-b2e8-eb6a26cd0677"},"_deposit":{"created_by":1,"id":"5660","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"5660"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00005660","sets":["1887:1891","9:789:972:991"]},"author_link":["27765"],"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2008-02-29","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"51","bibliographicPageStart":"44","bibliographicVolumeNumber":"JAXA-SP-07-008E","bibliographic_titles":[{"bibliographic_title":"宇宙航空研究開発機構特別資料"},{"bibliographic_title":"JAXA Special Publication: Proceedings of Lectures and Workshop International: Recent Advances in Multidisciplinary Technology and Modeling","bibliographic_titleLang":"en"}]}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Multidisciplinary Design Optimization is frequently looked at as the use of new computational tools, coupling together models of various disciplines in a single numerical environment, integrating a mathematical optimization algorithm with tuned design characteristics so as to optimize the objective criteria. Although this 'tool' aspect is an important one, the deployment of Multidisciplinary Design also represents challenges in terms of organization, competence, and engineering processes. The objective of this paper is to illustrate such aspects of MDO (Multidisciplinary Design Optimization), focusing on one particular example: the optimization of the interactions between the electronic flight control system and the structural loads and dynamic behavior of the A380 aircraft. These processes will be presented along with the well-known V&V (Validation and Verification) cycle of the system development where each part of this 'V' has different objectives and induces differences in engineering activities and the relationships between disciplines. It will be shown that this MDO process not only relies on integrated multidisciplinary models and mathematical optimization dependent on the phase and part of the FCS (Flight Control System) design, but also on engineers from the different disciplines sharing their knowledge, models, and exchanging technical information.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0063824005","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: JAXA-SP-07-008E","subitem_description_type":"Other"}]},"item_5_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"宇宙航空研究開発機構"}]},"item_5_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"Japan Aerospace Exploration Agency (JAXA)"}]},"item_5_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"1349-113X","subitem_source_identifier_type":"ISSN"}]},"item_5_source_id_24":{"attribute_name":"書誌レコードID","attribute_value_mlt":[{"subitem_source_identifier":"AA11984031","subitem_source_identifier_type":"NCID"}]},"item_5_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"Airbus Industries Loads and Aeroelastics"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Airbus Industries Loads and Aeroelastics"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"Humbert, Marc","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":"2020-01-16"}],"displaytype":"detail","filename":"63824005.pdf","filesize":[{"value":"552.6 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"63824005.pdf","url":"https://jaxa.repo.nii.ac.jp/record/5660/files/63824005.pdf"},"version_id":"a9e66e84-ab7b-4453-8e64-9ba1022d95ea"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"航空機設計","subitem_subject_scheme":"Other"},{"subitem_subject":"複合領域設計最適化","subitem_subject_scheme":"Other"},{"subitem_subject":"エアバス","subitem_subject_scheme":"Other"},{"subitem_subject":"飛行制御","subitem_subject_scheme":"Other"},{"subitem_subject":"旅客機","subitem_subject_scheme":"Other"},{"subitem_subject":"空力弾性","subitem_subject_scheme":"Other"},{"subitem_subject":"最適化アルゴリズム","subitem_subject_scheme":"Other"},{"subitem_subject":"認証","subitem_subject_scheme":"Other"},{"subitem_subject":"構造振動","subitem_subject_scheme":"Other"},{"subitem_subject":"飛行シミュレーション","subitem_subject_scheme":"Other"},{"subitem_subject":"フライトシミュレータ","subitem_subject_scheme":"Other"},{"subitem_subject":"aircraft design","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"multidisciplinary design optimization","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Airbus","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"flight control","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"passenger aircraft","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"aeroelasticity","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"optimization algorithm","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"validation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"structural vibration","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"flight simulation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"flight simulator","subitem_subject_language":"en","subitem_subject_scheme":"Other"}]},"item_language":{"attribute_name":"言語","attribute_value_mlt":[{"subitem_language":"eng"}]},"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":"An example of a multidisciplinary process applied to an Airbus design: Optimization of the A380 weight and ride comfort by an active flight control system","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"An example of a multidisciplinary process applied to an Airbus design: Optimization of the A380 weight and ride comfort by an active flight control system","subitem_title_language":"en"}]},"item_type_id":"5","owner":"1","path":["991","1891"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"5660","relation_version_is_last":true,"title":["An example of a multidisciplinary process applied to an Airbus design: Optimization of the A380 weight and ride comfort by an active flight control system"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T08:09:53.164523+00:00"}