{"created":"2023-06-20T14:39:12.221225+00:00","id":5899,"links":{},"metadata":{"_buckets":{"deposit":"45fc3605-6be5-42c2-993b-6a67acda1f94"},"_deposit":{"created_by":1,"id":"5899","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"5899"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00005899","sets":["1887:1891","9:789:998:1019"]},"author_link":["29146","29152","29148","29150","29151","29149","29147","29145"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Lunar gravity measurements system by orbital determination using three lunar orbiter of SELENE"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2007-03-30","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"90","bibliographicPageStart":"85","bibliographicVolumeNumber":"JAXA-SP-06-015","bibliographic_titles":[{"bibliographic_title":"宇宙航空研究開発機構特別資料: 先進的軌道計測・決定技術に関する研究会論文集"},{"bibliographic_title":"JAXA Special Publication: Proceedings of Advanced Orbit Measurement and Orbit Calculation Technologies","bibliographic_titleLang":"en"}]}]},"item_5_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"SELENEによる測月観測のためのリレー衛星中継器(RSAT; Relay Satellite Transponders)は、リレー衛星(Rstar)に搭載されるRSAT-1と主衛星に搭載されるRSAT-2から構成され、主衛星の月の裏側の軌道をRstar経由の4wayドプラ計測により観測する。RSATによる月裏側の重力場分布の観測と、相対VLBI用電波源(VRAD)による重力場低次項の精測により、月重力場モデルの改善を図る。","subitem_description_type":"Abstract"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Global mapping of the lunar gravity field will be conducted by using two small sub-satellites of SELENE (SELenological and Engineering Explorer): the Relay Satellite (Rstar) and the VLBI (Very Large Baseline Interferometry) Radio Satellite (Vstar). Four-way Doppler measurements toward the SELENE Main Orbiter above the lunar far side will be carried out by the Relay Satellite Transponders (RSAT) on Rstar and the Main Orbiter. Phase-delay differential VLBI observations will be performed for multi-frequency carrier waves emitted from the Differential VLBI Radio Sources (VRAD) on Rstar and Vstar. We have executed proto-flight tests and confirmed that instruments and the ground system of RSAT and VRAD have enough performances to improve the accuracy of the lunar gravity field.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0063223013","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: JAXA-SP-06-015","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"}]},"item_5_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"Japan Aerospace Exploration Agency (JAXA)"}]},"item_5_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"1349-113X","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":"AA11984031","subitem_source_identifier_type":"NCID"}]},"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"},{"subitem_text_value":"九州大学 理学部"},{"subitem_text_value":"国立天文台 水沢観測所"},{"subitem_text_value":"国立天文台"}]},"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"},{"subitem_text_language":"en","subitem_text_value":"Kyushu University School of Sciences"},{"subitem_text_language":"en","subitem_text_value":"National Astronomical Observatory Mizusawa Astrogeodynamics Observatory"},{"subitem_text_language":"en","subitem_text_value":"National Astronomical Observatory"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"岩田, 隆浩"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"並木, 則行"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"花田, 英夫"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"RSAT/VRADグループ"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Iwata, Takahiro","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Namiki, Noriyuki","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Hanada, Hideo","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"RSAT/VRAD Group","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":"2020-01-16"}],"displaytype":"detail","filename":"63223013.pdf","filesize":[{"value":"2.2 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"63223013.pdf","url":"https://jaxa.repo.nii.ac.jp/record/5899/files/63223013.pdf"},"version_id":"19d1af8d-121f-4d6a-a558-0b8041c4a15e"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"月重力","subitem_subject_scheme":"Other"},{"subitem_subject":"軌道決定","subitem_subject_scheme":"Other"},{"subitem_subject":"小型衛星技術","subitem_subject_scheme":"Other"},{"subitem_subject":"超長距離干渉計","subitem_subject_scheme":"Other"},{"subitem_subject":"SELENE","subitem_subject_scheme":"Other"},{"subitem_subject":"リレー衛星中継器","subitem_subject_scheme":"Other"},{"subitem_subject":"RSAT","subitem_subject_scheme":"Other"},{"subitem_subject":"VLBI用電波源","subitem_subject_scheme":"Other"},{"subitem_subject":"VRAD","subitem_subject_scheme":"Other"},{"subitem_subject":"重力場","subitem_subject_scheme":"Other"},{"subitem_subject":"衛星摂動","subitem_subject_scheme":"Other"},{"subitem_subject":"衛星ドップラー測位","subitem_subject_scheme":"Other"},{"subitem_subject":"月の裏側","subitem_subject_scheme":"Other"},{"subitem_subject":"lunar gravitation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"orbit determination","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"small satellite technology","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"very long base interferometry","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"SELENE","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Relay Satellite Transponder","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"RSAT","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"VLBI Radio Source","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"VRAD","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"gravitational field","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"satellite perturbation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"satellite Doppler positioning","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"lunar far side","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":"conference paper","resourceuri":"http://purl.org/coar/resource_type/c_5794"}]},"item_title":"SELENEの3機の月周回衛星を用いた軌道決定による月重力場観測システム","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"SELENEの3機の月周回衛星を用いた軌道決定による月重力場観測システム"}]},"item_type_id":"5","owner":"1","path":["1019","1891"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"5899","relation_version_is_last":true,"title":["SELENEの3機の月周回衛星を用いた軌道決定による月重力場観測システム"],"weko_creator_id":"1","weko_shared_id":1},"updated":"2023-06-20T19:45:42.319225+00:00"}