{"created":"2023-06-20T15:10:18.986375+00:00","id":39900,"links":{},"metadata":{"_buckets":{"deposit":"427abc1b-072d-433e-960b-acb0114e273f"},"_deposit":{"created_by":1,"id":"39900","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"39900"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00039900","sets":["1887:1893","1896:1898:1913:1917"]},"author_link":["445557","445558","445556","445561","445559","445560","445562","445563"],"item_3_alternative_title_1":{"attribute_name":"その他のタイトル","attribute_value_mlt":[{"subitem_alternative_title":"MIAS飛行試験におけるMLSの角度精度"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1996-11","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"19","bibliographicPageStart":"1","bibliographicVolumeNumber":"1314T","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":"オランダのデルフト工科大学で開発を進めているMulti-mode Integrated Approach System(MIAS)は、マイクロ波着陸誘導システム(MLS)およびディファレンシャル全世界測位衛星システム(DGPS)を利用した着陸援助システムである。MIASでは、2種類の独立したシステムを利用するため、有効性およびそれぞれのシステムの保全性を増加させることができる。MIAS飛行試験は、システムの能力を評価するために、1994年にアムステルダムのスキポール空港で行われたので、その結果を報告する。特にMLSデータは、搬送波位相方式のDGPSにより得られた基準データと比較した。直線進入の場合、MLSの仰角精度は、バイアス分を除くと、今回の飛行試験装置の場合、約0.015(1σ)度で、バイアスの平均値は約0.025度であった。方位角精度は、バイアス分を除くと、約0.015(1σ)度で、バイアスの平均値は約-0.075度であった。また、離陸および急旋回のときは、精度が劣化した。","subitem_description_type":"Abstract"}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"The Multi-mode Integrated Approach System (MIAS) is under development at Delft University of Technology (DUT), the Netherlands. The system is an advanced approach system based on the Microwave Landing System (MLS) and Differential Global Positioning System (DGPS). Since the MIAS uses two independent systems, the availability of the system and the maintainability of each subsystem can be increased. Flight tests were performed at Amsterdam's Schiphol airport in 1994 to evaluate the performance of the system. This report describes the flight test results of the MIAS in 1994. Especially the MLS data was compared with true reference obtained from carrier phase DGPS. In the case of a straight approach, the accuracy of the MLS elevation angle in this flight test equipment was approximately 0.015 deg (1 sigma) except for a bias. The mean of the bias was approximately 0.025 deg. The accuracy of the MLS azimuth angle was approximately 0.015 deg (1 sigma) except for a bias. The mean of the bias was approximately -0.075 deg. In the case of take off and steep turn, the accuracy of the MLS angle decreased.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0000878000","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-1314T","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 飛行実験部"},{"subitem_text_value":"Delft University of Technology"},{"subitem_text_value":"Delft University of Technology"},{"subitem_text_value":"Delft University of Technology"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Flight Research Division"},{"subitem_text_language":"en","subitem_text_value":"Delft University of Technology"},{"subitem_text_language":"en","subitem_text_value":"Delft University of Technology"},{"subitem_text_language":"en","subitem_text_value":"Delft University of Technology"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"井之口, 浜木"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Zaayer, M."}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Sridhar, J. K."}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Mulder, J. A."}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Inokuchi, Hamaki","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Zaayer, M.","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Sridhar, J. K.","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Mulder, J. A.","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":"naltr1314t.pdf","filesize":[{"value":"1.3 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"naltr1314t.pdf","url":"https://jaxa.repo.nii.ac.jp/record/39900/files/naltr1314t.pdf"},"version_id":"83f64cc5-4b89-4cb4-82d8-d467ea78867b"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"MIAS","subitem_subject_scheme":"Other"},{"subitem_subject":"マルチモードインテグレーテッドアプローチシステム","subitem_subject_scheme":"Other"},{"subitem_subject":"MLS","subitem_subject_scheme":"Other"},{"subitem_subject":"マイクロ波着陸誘導システム","subitem_subject_scheme":"Other"},{"subitem_subject":"DGPS","subitem_subject_scheme":"Other"},{"subitem_subject":"ディファレンシャルGPS","subitem_subject_scheme":"Other"},{"subitem_subject":"仰角精度","subitem_subject_scheme":"Other"},{"subitem_subject":"方位角精度","subitem_subject_scheme":"Other"},{"subitem_subject":"ターミナルエリア航法","subitem_subject_scheme":"Other"},{"subitem_subject":"ILS","subitem_subject_scheme":"Other"},{"subitem_subject":"計器着陸システム","subitem_subject_scheme":"Other"},{"subitem_subject":"飛行試験","subitem_subject_scheme":"Other"},{"subitem_subject":"MIAS","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"multimode integrated approach system","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"MLS","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"microwave landing system","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"DGPS","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"differential global positioning system","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"elevation angle accuracy","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"azimuth angle accuracy","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"terminal area navigation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"ILS","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"instrument landing system","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"flight testing","subitem_subject_language":"en","subitem_subject_scheme":"Other"}]},"item_language":{"attribute_name":"言語","attribute_value_mlt":[{"subitem_language":"eng"}]},"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":"MLS angle accuracy of the MIAS flight test","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"MLS angle accuracy of the MIAS flight test","subitem_title_language":"en"}]},"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":"39900","relation_version_is_last":true,"title":["MLS angle accuracy of the MIAS flight test"],"weko_creator_id":"1","weko_shared_id":1},"updated":"2023-06-20T19:18:22.826512+00:00"}