{"created":"2023-06-20T15:07:50.842810+00:00","id":37210,"links":{},"metadata":{"_buckets":{"deposit":"30a3b427-cc65-44f0-b37d-b64c39f455a2"},"_deposit":{"created_by":1,"id":"37210","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"37210"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00037210","sets":["1887:1891","1896:1898:1913:1915"]},"author_link":["479612","479610","479615","479620","479614","479617","479618","479622","479621","479623","479624","479625","479619","479616","479611","479613"],"item_5_alternative_title_1":{"attribute_name":"その他のタイトル","attribute_value_mlt":[{"subitem_alternative_title":"ALFLEX誘導、操縦および制御システムの飛行試験結果"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1998-08","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"84","bibliographicPageStart":"73","bibliographicVolumeNumber":"39T","bibliographic_titles":[{"bibliographic_title":"航空宇宙技術研究所特別資料"},{"bibliographic_title":"Special Publication of National Aerospace Laboratory","bibliographic_titleLang":"en"}]}]},"item_5_description_14":{"attribute_name":"会議概要（会議名, 開催地, 会期, 主催者等）","attribute_value_mlt":[{"subitem_description":"航空宇宙技術研究所　宇宙開発事業団 28 Feb. 1997 Sydney","subitem_description_type":"Other"}]},"item_5_description_15":{"attribute_name":"会議概要（会議名, 開催地, 会期, 主催者等）（英）","attribute_value_mlt":[{"subitem_description":"National Aerospace Laboratory. National Space Development Agency of Japan 28 Feb. 1997 Sydney Australia","subitem_description_type":"Other"}]},"item_5_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"この論文では、自動着陸飛行実験(ALFLEX)用に開発した誘導、操縦および制御(GNC)システムの飛行試験結果について議論する。飛行試験はすべての事項において成功し、GNCシステムが自動着陸に適切であることを示した。この論文では、GNCシステムに関する飛行試験データを分析し、GNCシステム設計の結果について議論する。","subitem_description_type":"Abstract"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"This paper discusses the flight test results of the Guidance, Navigation and Control (GNC) system developed for the Automatic Landing Flight Experiment, (ALFLEX). The flight tests were successful in every respect, which shows the GNC system is adequate for automatic landing. In this paper, the flight test data concerning the GNC system is analyzed, and also the results of designing the GNC system is discussed.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0001565007","subitem_description_type":"Other"}]},"item_5_description_33":{"attribute_name":"レポート番号","attribute_value_mlt":[{"subitem_description":"レポート番号: NAL SP-39T","subitem_description_type":"Other"}]},"item_5_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"航空宇宙技術研究所"}]},"item_5_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"National Aerospace Laboratory (NAL)"}]},"item_5_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"0289-260X","subitem_source_identifier_type":"ISSN"}]},"item_5_source_id_24":{"attribute_name":"書誌レコードID","attribute_value_mlt":[{"subitem_source_identifier":"AN10097345","subitem_source_identifier_type":"NCID"}]},"item_5_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"三菱重工業 名古屋航空宇宙システム製作所"},{"subitem_text_value":"三菱重工業 名古屋航空宇宙システム製作所"},{"subitem_text_value":"三菱重工業 名古屋航空宇宙システム製作所"},{"subitem_text_value":"三菱重工業 名古屋航空宇宙システム製作所"},{"subitem_text_value":"三菱重工業 名古屋航空宇宙システム製作所"},{"subitem_text_value":"航空宇宙技術研究所"},{"subitem_text_value":"航空宇宙技術研究所"},{"subitem_text_value":"宇宙開発事業団"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Mitsubishi Heavy Industries Ltd Nagoya Aerospace Systems"},{"subitem_text_language":"en","subitem_text_value":"Mitsubishi Heavy Industries Ltd Nagoya Aerospace Systems"},{"subitem_text_language":"en","subitem_text_value":"Mitsubishi Heavy Industries Ltd Nagoya Aerospace Systems"},{"subitem_text_language":"en","subitem_text_value":"Mitsubishi Heavy Industries Ltd Nagoya Aerospace Systems"},{"subitem_text_language":"en","subitem_text_value":"Mitsubishi Heavy Industries Ltd Nagoya Aerospace Systems"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory"},{"subitem_text_language":"en","subitem_text_value":"National Space Development Agency of Japan"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"小沼, 裕之"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"岩崎, 知二"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"山口, 泰弘"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"後藤, 敬太"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"水谷, さおり"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"宮沢, 与和"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"元田, 敏和"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"泉, 達司"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Onuma, Hiroyuki","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Iwasaki, Tomoji","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Yamaguchi, Yasuhiro","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Goto, Keita","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Mizutani, Saori","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Miyazawa, Yoshikazu","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Motoda, Toshikazu","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Izumi, Tatsushi","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":"2020-02-10"}],"displaytype":"detail","filename":"nalsp0039007.pdf","filesize":[{"value":"4.1 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"nalsp0039007.pdf","url":"https://jaxa.repo.nii.ac.jp/record/37210/files/nalsp0039007.pdf"},"version_id":"1dba6fe0-006e-47fe-8478-f847a06a270b"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"ALFLEX","subitem_subject_scheme":"Other"},{"subitem_subject":"小型自動着陸実験","subitem_subject_scheme":"Other"},{"subitem_subject":"GNCシステム","subitem_subject_scheme":"Other"},{"subitem_subject":"誘導・操縦・制御システム","subitem_subject_scheme":"Other"},{"subitem_subject":"HOPE","subitem_subject_scheme":"Other"},{"subitem_subject":"H-2打上げ型有翼回収機","subitem_subject_scheme":"Other"},{"subitem_subject":"6自由度シミュレーションモデル","subitem_subject_scheme":"Other"},{"subitem_subject":"誤差モデル","subitem_subject_scheme":"Other"},{"subitem_subject":"混成航行則","subitem_subject_scheme":"Other"},{"subitem_subject":"飛行路再構成","subitem_subject_scheme":"Other"},{"subitem_subject":"差分GPS","subitem_subject_scheme":"Other"},{"subitem_subject":"マイクロ波着陸システム","subitem_subject_scheme":"Other"},{"subitem_subject":"慣性センサユニット","subitem_subject_scheme":"Other"},{"subitem_subject":"ALFLEX","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Automatic Landing Flight Experiment","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"GNC system","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"guidance navigation control system","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"HOPE","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"H 2 Orbiting Plane","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"6 degree of freedom simulation model","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"error model","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"hybrid navigation law","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"flight path reconstruction","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"differential GPS","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"microwave landing system","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"inertia measurement unit","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":"conference paper","resourceuri":"http://purl.org/coar/resource_type/c_5794"}]},"item_title":"Flight test results of ALFLEX guidance, navigation and control system","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"Flight test results of ALFLEX guidance, navigation and control system","subitem_title_language":"en"}]},"item_type_id":"5","owner":"1","path":["1891","1915"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"37210","relation_version_is_last":true,"title":["Flight test results of ALFLEX guidance, navigation and control system"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T21:23:24.902527+00:00"}