{"created":"2023-06-20T14:40:47.983267+00:00","id":7742,"links":{},"metadata":{"_buckets":{"deposit":"0e86f6ff-7fc7-4bfb-845f-fecffe7a9e4d"},"_deposit":{"created_by":1,"id":"7742","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"7742"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00007742","sets":["1543:1544:1560","1887:1891"]},"author_link":["41610","41609"],"item_5_alternative_title_1":{"attribute_name":"その他のタイトル","attribute_value_mlt":[{"subitem_alternative_title":"惑星探査機の軌道決定に対するノンコヒーレントドップラーデータの一適用"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2004-02","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"259","bibliographicPageStart":"254","bibliographic_titles":[{"bibliographic_title":"平成15年度アストロダイナミクスシンポジウム:講演後刷り集"},{"bibliographic_title":"ISAS Proceedings of 13th Workshop on Astrodynamics and Flight Mechanics 2003: A Collection of Technical Papers","bibliographic_titleLang":"en"}]}]},"item_5_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"惑星探査機の軌道決定(電波航法)においては、精度に限界があるが地上局で取得する2-wayのレンジ・ドップラーを観測量として用いており安定した結果が得られている。そこでドップラー観測に注目してみると、地上局の時計、計測装置の高精度化、搭載発振器の高安定化などめざましく研究開発が行われており1-wayの観測量の利用方が見直されており、本論ではその適用について検討を行ったことを述べる。","subitem_description_type":"Abstract"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Recent improvements in computational capability and station technology have renewed interest in examining the possibility of using one-way Doppler data alone to navigate interplanetary spacecraft. The one-way data can be formulated as the standard differenced-count Doppler or as phase measurements, and the data can be received at a single station or differenced if obtained simultaneously at two stations. A covariance analysis, which analyzes the accuracy obtainable by combinations of one-way Doppler data, is performed and compared with similar results using standard two-way Doppler and range.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0046652041","subitem_description_type":"Other"}]},"item_5_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"宇宙航空研究開発機構宇宙科学研究本部"}]},"item_5_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA/ISAS)"}]},"item_5_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"0918-8053","subitem_source_identifier_type":"ISSN"}]},"item_5_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"宇宙航空研究開発機構 宇宙科学研究本部"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency Institute of Space and Astronautical Science"}]},"item_access_right":{"attribute_name":"アクセス権","attribute_value_mlt":[{"subitem_access_right":"metadata only access","subitem_access_right_uri":"http://purl.org/coar/access_right/c_14cb"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"市川, 勉"}],"nameIdentifiers":[{"nameIdentifier":"41609","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"Ichikawa, Tsutomu","creatorNameLang":"en"}],"nameIdentifiers":[{"nameIdentifier":"41610","nameIdentifierScheme":"WEKO"}]}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"ノンコヒーレント・ドップラーデータ","subitem_subject_scheme":"Other"},{"subitem_subject":"共変数解析","subitem_subject_scheme":"Other"},{"subitem_subject":"位相測定","subitem_subject_scheme":"Other"},{"subitem_subject":"軌道決定","subitem_subject_scheme":"Other"},{"subitem_subject":"惑星間宇宙機","subitem_subject_scheme":"Other"},{"subitem_subject":"モデル","subitem_subject_scheme":"Other"},{"subitem_subject":"深宇宙","subitem_subject_scheme":"Other"},{"subitem_subject":"感度","subitem_subject_scheme":"Other"},{"subitem_subject":"non-coherent Doppler data","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"covariance analysis","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"phase measurement","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"orbit determination","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"interplanetary spacecraft","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"model","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"deep space","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"sensitivity","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":"An application of non-coherent doppler data for the orbit determination to a spacecraft","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"An application of non-coherent doppler data for the orbit determination to a spacecraft","subitem_title_language":"en"}]},"item_type_id":"5","owner":"1","path":["1560","1891"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"7742","relation_version_is_last":true,"title":["An application of non-coherent doppler data for the orbit determination to a spacecraft"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T07:34:45.680696+00:00"}