{"created":"2023-07-25T10:05:45.562449+00:00","id":804,"links":{},"metadata":{"_buckets":{"deposit":"a595346b-bedf-4e01-8c95-445a614a363c"},"_deposit":{"created_by":2,"id":"804","owners":[2],"pid":{"revision_id":0,"type":"depid","value":"804"},"status":"published"},"_oai":{"id":"oai:tsuyama-nit.repo.nii.ac.jp:00000804","sets":["2:5:62"]},"author_link":["5936","5935"],"item_10002_biblio_info_25":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2015-02-28","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"59","bibliographicPageStart":"55","bibliographicVolumeNumber":"56","bibliographic_titles":[{"bibliographic_title":"津山工業高等専門学校紀要"},{"bibliographic_title":"Bulletin of National Institute of Technology, Tsuyama College","bibliographic_titleLang":"en"}]}]},"item_10002_description_19":{"attribute_name":"著者版フラグ","attribute_value_mlt":[{"subitem_description":"publisher","subitem_description_type":"Other"}]},"item_10002_description_6":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"A procedure for calculating trajectory of quasi-geostationary satellites is demonstrated. Satellite orbit is calculated based on the Kepler's law. A way of obtaining trajectory of the orbit in the sky observed from arbitrary point on the Earth is explained. Influence on the trajectory by orbit eccentricity and tilting angle to equatorial plane is under consideration.","subitem_description_type":"Abstract"}]},"item_10002_full_name_4":{"attribute_name":"著者（別表記）","attribute_value_mlt":[{"nameIdentifiers":[{"nameIdentifier":"5936","nameIdentifierScheme":"WEKO"}],"names":[{"name":"Sato, Makoto"}]}]},"item_10002_publisher_9":{"attribute_name":"出版者（別表記）","attribute_value_mlt":[{"subitem_publisher":"National Institute of Technology, Tsuyama College"}]},"item_10002_source_id_10":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"0287-7066","subitem_source_identifier_type":"ISSN"}]},"item_10002_source_id_12":{"attribute_name":"書誌レコードID","attribute_value_mlt":[{"subitem_source_identifier":"AN00149351","subitem_source_identifier_type":"NCID"}]},"item_10002_subject_20":{"attribute_name":"日本十進分類法","attribute_value_mlt":[{"subitem_subject":"440","subitem_subject_scheme":"NDC"}]},"item_10002_text_2":{"attribute_name":"備考","attribute_value_mlt":[{"subitem_text_value":"論文"}]},"item_10002_text_7":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_text_value":"津山工業高等専門学校"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"佐藤, 誠"}],"nameIdentifiers":[{"nameIdentifier":"5935","nameIdentifierScheme":"WEKO"}]}]},"item_files":{"attribute_name":"ファイル情報","attribute_type":"file","attribute_value_mlt":[{"accessrole":"open_date","date":[{"dateType":"Available","dateValue":"2015-02-28"}],"displaytype":"detail","filename":"56-8.pdf","filesize":[{"value":"626.2 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"56-8.pdf","url":"https://tsuyama-nit.repo.nii.ac.jp/record/804/files/56-8.pdf"},"version_id":"5e5d8107-7792-4c81-acfe-b2f0e1cbd578"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"Kepler’s law","subitem_subject_scheme":"Other"},{"subitem_subject":"Quasi-zenith satellite","subitem_subject_scheme":"Other"},{"subitem_subject":"Geostationary satellite","subitem_subject_scheme":"Other"},{"subitem_subject":"Orbit","subitem_subject_scheme":"Other"},{"subitem_subject":"Trajectory","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":"departmental bulletin paper","resourceuri":"http://purl.org/coar/resource_type/c_6501"}]},"item_title":"準静止衛星の軌跡","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"準静止衛星の軌跡"},{"subitem_title":"Trajectory of quasi-geostationary satellites","subitem_title_language":"en"}]},"item_type_id":"10002","owner":"2","path":["62"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-02-28"},"publish_date":"2015-02-28","publish_status":"0","recid":"804","relation_version_is_last":true,"title":["準静止衛星の軌跡"],"weko_creator_id":"2","weko_shared_id":2},"updated":"2023-07-25T10:32:01.774233+00:00"}