{"created":"2023-06-20T15:11:29.011669+00:00","id":41150,"links":{},"metadata":{"_buckets":{"deposit":"177dfea5-df45-489e-b83e-9381b0d28da7"},"_deposit":{"created_by":1,"id":"41150","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"41150"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00041150","sets":["1887:1893","1896:1898:1913:1917"]},"author_link":["450781","450779","450777","450780","450776","450778","450783","450782"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Control system design of a cable-mounted model used for dynamic wind tunnel testing"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1992-06","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"49","bibliographicPageStart":"1","bibliographicVolumeNumber":"1161","bibliographic_titles":[{"bibliographic_title":"航空宇宙技術研究所報告"},{"bibliographic_title":"Technical Report of National Aerospace Laboratory","bibliographic_titleLang":"en"}]}]},"item_3_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"現在航技研(NAL)において行われているケーブル支持方式動的風洞試験による航空機空力特性同定の試験援助のための模型制御系設計を行った。設計手法は代表的な釣合点近傍における線形数学モデルに基づく根軌跡法とした。設計した制御系は非線形シミュレーションにより機能確認を行った後、実試験に適用された。その結果、数学モデルのモデル化誤差のために若干のゲイン調整が必要となったが最終的には良好な制御性能を示し、この制御系を用いて空力特性同定試験が実施された。","subitem_description_type":"Abstract"}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"The control system of a cable-mounted aircraft model used for dynamic wind tunnel testing was designed using the root locus method. Computer simulations were initially performed to evaluate the designed control system, which was then applied to actual wind tunnel tests. Results confirmed the system's suitability, although the control gains required slight tuning. In addition, wind tunnel tests were conducted using the control system to identify the aerodynamic model of the cable-mounted model.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0004180000","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 TR-1161","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":"0389-4010","subitem_source_identifier_type":"ISSN"}]},"item_3_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"航空宇宙技術研究所 制御部"},{"subitem_text_value":"航空宇宙技術研究所 制御部"},{"subitem_text_value":"航空宇宙技術研究所 制御部"},{"subitem_text_value":"航空宇宙技術研究所 制御部"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Control Systems Division"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Control Systems Division"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Control Systems Division"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Control Systems Division"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"柳原, 正明"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"永安, 正彦"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"佐々, 修一"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"下村, 卓"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Yanagihara, Masaaki","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Nagayasu, Masahiko","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Sasa, Syuichi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Shimomura, Takashi","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":"2020-01-27"}],"displaytype":"detail","filename":"naltr01161.pdf","filesize":[{"value":"2.8 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"naltr01161.pdf","url":"https://jaxa.repo.nii.ac.jp/record/41150/files/naltr01161.pdf"},"version_id":"bf4faac2-4149-423a-ae5c-8d754238de95"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"ケーブル支持模型","subitem_subject_scheme":"Other"},{"subitem_subject":"動的風洞試験","subitem_subject_scheme":"Other"},{"subitem_subject":"制御系","subitem_subject_scheme":"Other"},{"subitem_subject":"根軌跡法","subitem_subject_scheme":"Other"},{"subitem_subject":"自由飛行模擬風洞試験","subitem_subject_scheme":"Other"},{"subitem_subject":"スペースプレーン","subitem_subject_scheme":"Other"},{"subitem_subject":"模型支持装置","subitem_subject_scheme":"Other"},{"subitem_subject":"動的模型支持","subitem_subject_scheme":"Other"},{"subitem_subject":"空力微係数","subitem_subject_scheme":"Other"},{"subitem_subject":"安定微係数","subitem_subject_scheme":"Other"},{"subitem_subject":"運動解析","subitem_subject_scheme":"Other"},{"subitem_subject":"空力パラメータ同定","subitem_subject_scheme":"Other"},{"subitem_subject":"姿勢制御","subitem_subject_scheme":"Other"},{"subitem_subject":"模型支持系","subitem_subject_scheme":"Other"},{"subitem_subject":"cable mounted model","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"dynamic wind tunnel test","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"control system","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"root locus method","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"attitude control","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"model support system","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"free flight simulation wind tunnel test","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"aerodynamic parameter identification","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"space plane","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"model support system","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"aerodynamic derivative","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"stability derivative","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"motion analysis","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"dynamic model support","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":"ケーブル支持動的風洞試験のための模型制御系設計","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"ケーブル支持動的風洞試験のための模型制御系設計"}]},"item_type_id":"3","owner":"1","path":["1893","1917"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"41150","relation_version_is_last":true,"title":["ケーブル支持動的風洞試験のための模型制御系設計"],"weko_creator_id":"1","weko_shared_id":1},"updated":"2023-06-20T19:13:06.911685+00:00"}