{"created":"2023-06-20T15:14:14.602833+00:00","id":44224,"links":{},"metadata":{"_buckets":{"deposit":"78c4a65b-ddc7-4f85-9e6f-ed581c260f78"},"_deposit":{"created_by":1,"id":"44224","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"44224"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00044224","sets":["1887:1893","1896:1898:1913:1916"]},"author_link":["468446","468442","468445","468444","468443","468448","468441","468447"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Estimation of Cable-Mounted Model Inertia Characteristics for Dynamic Wind-Tunnel Test"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1991-10","bibliographicIssueDateType":"Issued"},"bibliographicPageStart":"41","bibliographicVolumeNumber":"641","bibliographic_titles":[{"bibliographic_title":"航空宇宙技術研究所資料"},{"bibliographic_title":"Technical Memorandum of National Aerospace Laboratory","bibliographic_titleLang":"en"}]}]},"item_3_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"ケーブル支持方式動的風洞試験用5％スペースプレーン模型の慣性特性推定実験を行った。推定対象は上下重心位置と3軸回りの慣性モーメントIx, Iy, Iz及び慣性乗積Ixzとし,計測方法は2本吊り自由振動法を用いた。また,それらの持つ誤差についても最大推定値の計算を行った。その結果,Iy, Iz及び重心位置に関しては良好な誤差範囲内で推定が行われたが,Ix及びIxzについては比較的大きな誤差を持つ可能性が生じた。これらの結果については測定に使用する吊り下げ治具として小型軽量のものを用いれば改善されることが確認された。","subitem_description_type":"Abstract"}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"The inertia characteristics of a National Aerospace Laboratory (NAL) Spaceplane cable-mounted model (1:20) used for dynamic wind tunnel tests were experimentally estimated. The estimated parameters consisted of the vertical position of the model′s center of gravity, the inertia moments Ix, Iy and Iz, and the product of inertia Ixz. The method was based on a bifilar pendulun system and estimation errors were evaluated. As a result, the moment of inertia Iy and Iz were estimated within an about ±1％ error, although Ix and the product of inertia Ixz had larger errors. An analysis of the estimation error confirmed that the errors for Ix and Ixz can be improved b using a smaller suspension rig.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: NALTM0641000","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 TM-641","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":"0452-2982","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":"AN00314334","subitem_source_identifier_type":"NCID"}]},"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":"Contorol Systems Division"},{"subitem_text_language":"en","subitem_text_value":"Contorol Systems Division"},{"subitem_text_language":"en","subitem_text_value":"Contorol Systems Division"},{"subitem_text_language":"en","subitem_text_value":"Contorol 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, Shuichi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Takashi, Shimomura","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":"2020-01-29"}],"displaytype":"detail","filename":"naltm00641.pdf","filesize":[{"value":"2.1 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"naltm00641.pdf","url":"https://jaxa.repo.nii.ac.jp/record/44224/files/naltm00641.pdf"},"version_id":"ebf01c97-99f4-4b70-bb18-2f8548811500"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"moment of inertia;  cable-mounted model;  bifilar pendulum","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模型の慣性特性推定","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模型の慣性特性推定"}]},"item_type_id":"3","owner":"1","path":["1893","1916"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"44224","relation_version_is_last":true,"title":["ケーブル支持動的風洞試験模型の慣性特性推定"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T22:00:39.672451+00:00"}