{"created":"2023-06-20T15:10:05.788980+00:00","id":39687,"links":{},"metadata":{"_buckets":{"deposit":"46da91e2-93eb-467c-b1e6-6e37ca01bd54"},"_deposit":{"created_by":1,"id":"39687","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"39687"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00039687","sets":["1887:1893","1896:1898:1913:1917"]},"author_link":["443911","443918","443909","443917","443908","443914","443916","443913","443912","443910","443919","443915"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Orbit determination of the orbital reentry experiment (OREX) vehicle by GPS"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1995-11","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"30","bibliographicPageStart":"1","bibliographicVolumeNumber":"1280","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":"わが国における最初の宇宙用GPS(地球測位システム)受信機による人工衛星の軌道決定実験が、1994年2月に打ち上げられたOREX(軌道再突入実験機)を利用して実施された。本報告では、GPSによる人工衛星の軌道決定の可能性を実データをもとに検証することを目的として、このとき得られたOREXのGPS受信データを事後解析し、受信データの妥当性やGPSによる軌道決定精度の評価を行った。さらに、HOPE(H-2ロケット打上型有翼回収機)のように滑走路へ自動着陸する飛翔体の誘導制御に不可欠の、ディファレンシャルGPS(DGPS)や精密軌道暦によるGPS航法、GPS/IMU(慣性計測装置)複合航法といったGPSの最新の利用技術を応用した結果も示した。","subitem_description_type":"Abstract"}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"A Japanese first spaceborne GPS (Global Positionings System) receiver, within the OREX (Orbital Reentry Experiment) vehicle, was launched by the H-2 launch vehicle on February 4, 1994. The observed GPS data are analyzed in this report to evaluate the accuracy of orbit determination by GPS. Following four techniques for orbit determination were examined: GPS stand-alone navigation, differential GPS navigation, GPS navigation with the precise ephemeris, and GPS/IMU (Inertial Measurement Unit) hybrid navigation. These results were evaluated by comparison with independent radar data and the efficiency of GPS orbit determination is confirmed.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0000107000","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-1280","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":"宇宙開発事業団"},{"subitem_text_value":"宇宙開発事業団"}]},"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 System Division"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Control System Division"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Control System Division"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Control System Division"},{"subitem_text_language":"en","subitem_text_value":"National Space Development Agency of Japan"},{"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":"張替, 正敏"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"村田, 正秋"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"辻井, 利昭"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"新宮, 博公"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"冨田, 博史"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"松本, 秀一"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Harigae, Masatoshi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Murata, Masaaki","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Tsujii, Toshiaki","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Shingu, Hirokimi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Tomita, Hiroshi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Matsumoto, Shuichi","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":"naltr01280.pdf","filesize":[{"value":"2.8 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"naltr01280.pdf","url":"https://jaxa.repo.nii.ac.jp/record/39687/files/naltr01280.pdf"},"version_id":"0e5116e6-73bd-41ca-9d0e-56e25eaa40e5"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"GPS","subitem_subject_scheme":"Other"},{"subitem_subject":"地球測位システム","subitem_subject_scheme":"Other"},{"subitem_subject":"自動着陸","subitem_subject_scheme":"Other"},{"subitem_subject":"軌道決定","subitem_subject_scheme":"Other"},{"subitem_subject":"ディファレンシャルGPS","subitem_subject_scheme":"Other"},{"subitem_subject":"軌道再突入実験機","subitem_subject_scheme":"Other"},{"subitem_subject":"OREX","subitem_subject_scheme":"Other"},{"subitem_subject":"Kalmanフィルタ","subitem_subject_scheme":"Other"},{"subitem_subject":"GPS受信機","subitem_subject_scheme":"Other"},{"subitem_subject":"誘導制御","subitem_subject_scheme":"Other"},{"subitem_subject":"スペースプレーン","subitem_subject_scheme":"Other"},{"subitem_subject":"GPS航法","subitem_subject_scheme":"Other"},{"subitem_subject":"誤差解析","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":"automatic landing","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"orbit determination","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"differential GPS","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"orbital reentry experiment vehicle","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"OREX","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Kalman filter","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"GPS receiver","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"guidance and control","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"space plane","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"GPS navigation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"error analysis","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":"GPSによる軌道再突入実験機(OREX)の軌道決定","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"GPSによる軌道再突入実験機(OREX)の軌道決定"}]},"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":"39687","relation_version_is_last":true,"title":["GPSによる軌道再突入実験機(OREX)の軌道決定"],"weko_creator_id":"1","weko_shared_id":1},"updated":"2023-06-20T19:19:40.291625+00:00"}