{"created":"2023-06-20T15:13:51.702840+00:00","id":43831,"links":{},"metadata":{"_buckets":{"deposit":"a08c89bd-2d59-46b8-a6f1-b6799c1afa37"},"_deposit":{"created_by":1,"id":"43831","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"43831"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00043831","sets":["1887:1893","1896:1898:1913:1916"]},"author_link":["465842","465844","465847","465843","465846","465845"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Test Rig for Automatic Landing System Study"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1973-10","bibliographicIssueDateType":"Issued"},"bibliographicPageStart":"18","bibliographicVolumeNumber":"248","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_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Studies on hardwares of automatic landing system, as a part of automatic landing system study programs, have been conducted at National Aerospace Laboratory. A test rig for the study on the hardwares has been designed and constructed. The test rig is a ground test equipment for evaluating the. automatic flight control system including actual hardwares and human factors of a pilot. The testing hardwares, such as servo actuators, servo amplifiers, auto-land computers and control pannels so on, are equipped on the test rig and tested in a simulated flight condition with an analog computer. The test rig has actual control systems of experimental aircraft, which is Beechcraft Queen Air Model 65, such as elevator control system, aileron control system, rudder cont- rol system, trim controls, and engine throttle control system. And each of the control systems consists of control rigs, pulleies, control load which is simulated an aerodynamic load and control wheel or pedal. In this paper, the design, construction and performance of the test rig are reported here.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: NALTM0248000","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-248","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計測部"},{"subitem_text_value":"航空宇宙技術研究所計測部"},{"subitem_text_value":"航空宇宙技術研究所計測部"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"堀川, 勇壮"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"小川, 鑛一"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"永安, 正彦"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"HORIKAWA, Yuso","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"OGAWA, Koichi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"NAGAYASU, Masahiko","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":"2020-01-28"}],"displaytype":"detail","filename":"naltm00248.pdf","filesize":[{"value":"1.7 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"naltm00248.pdf","url":"https://jaxa.repo.nii.ac.jp/record/43831/files/naltm00248.pdf"},"version_id":"449dbd6a-f2d4-4907-bfed-13268b911c50"}]},"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":"自動着陸研究用テスト・リグについて","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"自動着陸研究用テスト・リグについて"}]},"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":"43831","relation_version_is_last":true,"title":["自動着陸研究用テスト・リグについて"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T22:07:10.062659+00:00"}