{"created":"2023-06-20T15:11:33.510972+00:00","id":41238,"links":{},"metadata":{"_buckets":{"deposit":"6337fe07-9f44-4e73-8c7a-b827f97c8e55"},"_deposit":{"created_by":1,"id":"41238","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"41238"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00041238","sets":["1887:1893","1896:1898:1913:1917"]},"author_link":["451396","451394","451389","451395","451398","451397","451388","451399","451400","451390","451393","451401","451392","451391"],"item_3_alternative_title_1":{"attribute_name":"その他のタイトル","attribute_value_mlt":[{"subitem_alternative_title":"DGPS-INSハイブリッド航法システムの予備的飛行評価"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1995-03","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"10","bibliographicPageStart":"1","bibliographicVolumeNumber":"1262T","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":"本論文は、次世代航法システム構築のために進められているGPS差分航法(DGPS)慣性航法(INS)複合航法システムの飛行評価の概要を記している。地上設備、計測システムを含む飛行実験の構成を述べるとともに、カルマンフィルタを用いた航法誤差評価方法の設計概念を明らかにし、また、実験に用いる飛行プロファイルを定義し、GPS,DGPS,INSの各航法システムの単独あるいは複合モードにおける飛行実験の結果を各プロファイルに即して評価し、DGPS-INS複合航法システムの導入によって航法性能が向上することを実験的に立証している。最後に、将来の航空宇宙機に適用可能なDGPS-INS複合航法システムの設計概念が確立できたと結論している。","subitem_description_type":"Abstract"}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"This paper summarizes the flight evaluation of the DGPS (Differential Global Positioning System) -INS (Inertial Navigation System) hybrid navigation system conducted as a preliminary study for constructing a next-generation navigation system at the National Aerospace Laboratory (NAL). First, the configuration used in the flight experiments, including ground facilities and the measurement systems, is described. Secondly, the design concept for a method of estimating navigation errors using a Kalmann filter is presented. Thirdly, flight profiles employed in the experiments are defined, and the experimental results of GPS, DGPS, INS in both stand-alone and hybrid modes which correspond to each profile are shown. Also, improvement in navigation performance by introducing the DGPS-INS hybrid navigation system was experimentally verified. In conclusion, the design concept of the DGPS-INS hybrid navigation system available for future space vehicles has been successfully completed.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0004269000","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-1262T","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 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"},{"subitem_text_value":"航空宇宙技術研究所 飛行実験部"},{"subitem_text_value":"航空宇宙技術研究所 飛行実験部"},{"subitem_text_value":"航空宇宙技術研究所 飛行実験部"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Control Systems Division"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Control Systems Division"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Control Systems Division"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Control Systems Division"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Flight Research Division"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Flight Research Division"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Flight Research Division"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"新宮, 博公"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"村田, 正秋"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"張替, 正敏"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"辻井, 敏秋"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"小野, 孝次"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"石川, 和敏"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"宮沢, 与和"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Shingu, Hirokimi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Murata, Masaaki","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Harigae, Masatoshi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Tsujii, Toshiaki","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Ono, Takatsugu","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Ishikawa, Kazutoshi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Miyazawa, Yoshikazu","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":"naltr1262t.pdf","filesize":[{"value":"869.9 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"naltr1262t.pdf","url":"https://jaxa.repo.nii.ac.jp/record/41238/files/naltr1262t.pdf"},"version_id":"e22f5bcf-db1d-476a-a3b6-b2f2a97471f3"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"GPS","subitem_subject_scheme":"Other"},{"subitem_subject":"全地球的位置決めシステム","subitem_subject_scheme":"Other"},{"subitem_subject":"INS","subitem_subject_scheme":"Other"},{"subitem_subject":"慣性航法装置","subitem_subject_scheme":"Other"},{"subitem_subject":"ディファレンシャルGPS","subitem_subject_scheme":"Other"},{"subitem_subject":"DGPS","subitem_subject_scheme":"Other"},{"subitem_subject":"複合航法","subitem_subject_scheme":"Other"},{"subitem_subject":"終着地域航法","subitem_subject_scheme":"Other"},{"subitem_subject":"飛行評価","subitem_subject_scheme":"Other"},{"subitem_subject":"航法システム","subitem_subject_scheme":"Other"},{"subitem_subject":"航空宇宙技術研究所","subitem_subject_scheme":"Other"},{"subitem_subject":"地上施設","subitem_subject_scheme":"Other"},{"subitem_subject":"測定システム","subitem_subject_scheme":"Other"},{"subitem_subject":"飛行実験","subitem_subject_scheme":"Other"},{"subitem_subject":"飛行プロフィール","subitem_subject_scheme":"Other"},{"subitem_subject":"GPS","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"global positioning system","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"INS","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"inertial navigation system","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"differential global positioning system","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"DGPS","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"hybrid navigation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"terminal area navigation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"flight evaluation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"navigation system","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"National Aerospace Laboratory","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"ground facilities","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"measurement system","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"flight experiment","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"flight profile","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":"A preliminary flight evaluation of DGPS-INS hybrid navigation system","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"A preliminary flight evaluation of DGPS-INS hybrid navigation system","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":"41238","relation_version_is_last":true,"title":["A preliminary flight evaluation of DGPS-INS hybrid navigation system"],"weko_creator_id":"1","weko_shared_id":1},"updated":"2023-06-20T19:11:31.635180+00:00"}