{"created":"2023-06-20T14:40:47.798692+00:00","id":7738,"links":{},"metadata":{"_buckets":{"deposit":"e84d114d-2e01-4de2-980c-9448b04fce44"},"_deposit":{"created_by":1,"id":"7738","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"7738"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00007738","sets":["1543:1544:1560","1887:1891"]},"author_link":["41589","41590"],"item_5_alternative_title_1":{"attribute_name":"その他のタイトル","attribute_value_mlt":[{"subitem_alternative_title":"半径方向に加速される宇宙機の軌道ダイナミクス"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2004-02","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"238","bibliographicPageStart":"233","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":"半径方向に連続した加速度が存在する場合の軌道ダイナミクスについて考察をする。加速度が半径方向の関数である場合の加速中の軌道パラメタの変化や最大到達距離および脱出のための条件を導いている。","subitem_description_type":"Abstract"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Orbital motion under an outward continuous radial acceleration as a function of the distance from the central body is analytically investigated. Two representative cases are analyzed in detail. One is the constant radial acceleration case, and the other assumes the radial acceleration inversely proportional to the square of the radial distance. The attainable maximum radial distance of the outbound trajectory is focused on. This paper summarizes the former half of AAS 03-521 Paper entitled 'A Guidance Strategy for the Radially Accelerated Trajectory.'","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0046652037","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":"宇宙科学研究所"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"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":"山川, 宏"}],"nameIdentifiers":[{"nameIdentifier":"41589","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"Yamakawa, Hiroshi","creatorNameLang":"en"}],"nameIdentifiers":[{"nameIdentifier":"41590","nameIdentifierScheme":"WEKO"}]}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"軌道運動","subitem_subject_scheme":"Other"},{"subitem_subject":"半径方向加速","subitem_subject_scheme":"Other"},{"subitem_subject":"解析解","subitem_subject_scheme":"Other"},{"subitem_subject":"脱出条件","subitem_subject_scheme":"Other"},{"subitem_subject":"宇宙機軌道","subitem_subject_scheme":"Other"},{"subitem_subject":"重力場","subitem_subject_scheme":"Other"},{"subitem_subject":"誘導","subitem_subject_scheme":"Other"},{"subitem_subject":"数値積分","subitem_subject_scheme":"Other"},{"subitem_subject":"orbital motion","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"radial acceleration","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"analytical solution","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"escape condition","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"spacecraft trajectory","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"gravitational field","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"guidance","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"numerical integration","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":"Dynamics of the radially accelerated trajectory","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"Dynamics of the radially accelerated trajectory","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":"7738","relation_version_is_last":true,"title":["Dynamics of the radially accelerated trajectory"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T07:34:49.189699+00:00"}