{"created":"2023-06-20T15:10:18.636315+00:00","id":39895,"links":{},"metadata":{"_buckets":{"deposit":"d6a82699-c111-4b73-9fa3-1ac00f18dd2a"},"_deposit":{"created_by":1,"id":"39895","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"39895"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00039895","sets":["1887:1893","1896:1898:1913:1917"]},"author_link":["445523","445522"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Maximum-likelihood estimation of the NAL spaceplane aerodynamic model using dynamic wind tunnel tests"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1996-09","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"13","bibliographicPageStart":"1","bibliographicVolumeNumber":"1307","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":"動的風洞試験による、航空機空力特性の推定法の研究の一環として、航技研のスペースプレーンの5％モデルを用いたケーブルマウント方式による動的風洞試験が1989年より実施された。そこで得られた試験データに最尤推定法を適用し、低速空力パラメータの推定を行い、同手法の基本性能の評価を、他の手法との比較を含めて行った。","subitem_description_type":"Abstract"}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"As a part of a study of the estimation of aircraft aerodynamic characteristics using dynamic wind tunnel tests, cable mount dynamic wind tunnel tests were executed from 1989. Maximum likelihood estimation algorithm is applied to the test data, and low speed aerodynamic parameters are estimated. The basic performance of the algorithm is evaluated by comparing it to other estimation algorithm.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0000873000","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-1307","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 動的風洞試験グループ"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Dynamic Wind Tunnel Test Group"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"動的風洞試験グループ"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Dynamic Wind Tunnel Test Group","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":"naltr01307.pdf","filesize":[{"value":"1.1 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"naltr01307.pdf","url":"https://jaxa.repo.nii.ac.jp/record/39895/files/naltr01307.pdf"},"version_id":"c529152c-6a4e-4abc-9f42-0d66ea9591ab"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"スペースプレーン","subitem_subject_scheme":"Other"},{"subitem_subject":"動的風洞試験","subitem_subject_scheme":"Other"},{"subitem_subject":"空力パラメータ","subitem_subject_scheme":"Other"},{"subitem_subject":"パラメータ推定","subitem_subject_scheme":"Other"},{"subitem_subject":"最尤法","subitem_subject_scheme":"Other"},{"subitem_subject":"2ステップ法","subitem_subject_scheme":"Other"},{"subitem_subject":"ピッチング運動","subitem_subject_scheme":"Other"},{"subitem_subject":"ケーブルマウント方式","subitem_subject_scheme":"Other"},{"subitem_subject":"カルマンフィルタ","subitem_subject_scheme":"Other"},{"subitem_subject":"space plane","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"dynamic wind tunnel test","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"aerodynamic parameter","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"parameter estimation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"maximum likelihood method","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"two step method","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"pitching motion","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"cable mount method","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Kalman filter","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":"最尤推定法によるNALスペースプレーン空力パラメータの動的風洞試験での推定","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"最尤推定法によるNALスペースプレーン空力パラメータの動的風洞試験での推定"}]},"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":"39895","relation_version_is_last":true,"title":["最尤推定法によるNALスペースプレーン空力パラメータの動的風洞試験での推定"],"weko_creator_id":"1","weko_shared_id":1},"updated":"2023-06-20T19:18:27.879099+00:00"}