{"created":"2023-06-20T15:11:37.820322+00:00","id":41317,"links":{},"metadata":{"_buckets":{"deposit":"9b2a3854-ccf4-49c9-a5cf-17b5a79a81a3"},"_deposit":{"created_by":1,"id":"41317","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"41317"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00041317","sets":["1887:1893","1896:1898:1913:1915"]},"author_link":["489456","489457"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Simulation technology in Fuji Heavy Industries: Today and in the future"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2000-12","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"88","bibliographicPageStart":"85","bibliographicVolumeNumber":"46","bibliographic_titles":[{"bibliographic_title":"航空宇宙技術研究所特別資料"},{"bibliographic_title":"Special Publication of National Aerospace Laboratory","bibliographic_titleLang":"en"}]}]},"item_3_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":"航空宇宙技術研究所 7-9 Jun. 2000 東京 日本","subitem_description_type":"Other"}]},"item_3_description_15":{"attribute_name":"会議概要（会議名, 開催地, 会期, 主催者等）（英）","attribute_value_mlt":[{"subitem_description":"National Aerospace Laboratory 7-9 Jun. 2000 Tokyo Japan","subitem_description_type":"Other"}]},"item_3_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"産業用ロボットを用いて風洞内における特定の航空機に適用する制御則を容易に評価するためのシミュレーション技術を開発した。このシステムは風洞運転をとおして航空機の機体形状と制御則の適切な組み合わせを求めることを可能にし、かつ最適化に対する設計の仕事を軽減した。このようなシステムは産業用ロボットおよびパーソナルコンピュータを使用して容易に構築することでき、パーソナルコンピュータ上で制御則を設計できた。ここではこの基本実証システムを構築して、基礎的な動作を実証した。これらの詳細について以下に示す。","subitem_description_type":"Abstract"}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"A simulation technique was developed to evaluate easily the control law applied for some particular airplane in the wind tunnel by utilizing industrial use Robots. This system enables obtaining a suitable combination of airplane configuration and control law by the wind tunnel operation, and lightens the design work for optimization. Such a system will be easily constructed by use of an industrial use robot and a personal computer, and the control law will be designed on the personal computer. This time, a prototype system was constructed and a basic operation was confirmed. Though, details will be shown below.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0028635016","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: NAL SP-46","subitem_description_type":"Other"}]},"item_3_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"航空宇宙技術研究所"}]},"item_3_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"National Aerospace Laboratory (NAL)"}]},"item_3_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"0289-260X","subitem_source_identifier_type":"ISSN"}]},"item_3_source_id_24":{"attribute_name":"書誌レコードID","attribute_value_mlt":[{"subitem_source_identifier":"AN10097345","subitem_source_identifier_type":"NCID"}]},"item_3_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"富士重工業 航空宇宙技術本部"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Fuji Heavy Industries Ltd Aerospace Division"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"越岡, 康弘"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Koshioka, Yasuhiro","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":"2020-02-10"}],"displaytype":"detail","filename":"nalsp0046016.pdf","filesize":[{"value":"477.9 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"nalsp0046016.pdf","url":"https://jaxa.repo.nii.ac.jp/record/41317/files/nalsp0046016.pdf"},"version_id":"1c2c6fd8-366a-45c7-96b3-2ca3c876cb16"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"シミュレーション技術","subitem_subject_scheme":"Other"},{"subitem_subject":"航空機機体形状","subitem_subject_scheme":"Other"},{"subitem_subject":"風洞運転","subitem_subject_scheme":"Other"},{"subitem_subject":"CFD","subitem_subject_scheme":"Other"},{"subitem_subject":"パーソナルコンピュータ","subitem_subject_scheme":"Other"},{"subitem_subject":"産業用ロボット","subitem_subject_scheme":"Other"},{"subitem_subject":"機体形状設計","subitem_subject_scheme":"Other"},{"subitem_subject":"静的空気力試験","subitem_subject_scheme":"Other"},{"subitem_subject":"動的空気力計測","subitem_subject_scheme":"Other"},{"subitem_subject":"CTS","subitem_subject_scheme":"Other"},{"subitem_subject":"制御則評価","subitem_subject_scheme":"Other"},{"subitem_subject":"操縦性能","subitem_subject_scheme":"Other"},{"subitem_subject":"計算流体力学","subitem_subject_scheme":"Other"},{"subitem_subject":"係留軌道システム","subitem_subject_scheme":"Other"},{"subitem_subject":"simulation technique","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"airplane configuration","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"wind tunnel operation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"CFD","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"personal computer","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"industrial use Robot","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"airframe design work","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"aerostatic test","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"aerodynamic measurement","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"CTS","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"control law evaluation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"maneuver capability","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"computational fluid dynamics","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"captive trajectory system","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":"富士重工業(株)におけるシミュレーション技術の現状と今後の方向について","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"富士重工業(株)におけるシミュレーション技術の現状と今後の方向について"}]},"item_type_id":"3","owner":"1","path":["1893","1915"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"41317","relation_version_is_last":true,"title":["富士重工業(株)におけるシミュレーション技術の現状と今後の方向について"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T21:03:21.410090+00:00"}