{"created":"2023-06-20T15:02:06.998793+00:00","id":31174,"links":{},"metadata":{"_buckets":{"deposit":"fbf24122-492c-497f-afe2-4947615dff6b"},"_deposit":{"created_by":1,"id":"31174","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"31174"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00031174","sets":["1887:1890","1896:1898:1899:1991"]},"author_link":["403656","403654","403655","403653"],"item_9_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1983-03","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"102","bibliographicPageStart":"87","bibliographicVolumeNumber":"1","bibliographic_titles":[{},{"bibliographic_title":"The Institute of Space and Astronautical Science report. S.P. : Proceedings of the Symposium on Mechanics for Space Flight","bibliographic_titleLang":"en"}]}]},"item_9_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Two kinds of optimization problems on low thrust transfer trajectories are discussed. One is a transfer from earth parking orbit to Sun-Earth interior libration point L_1.So-called J-minimum trajectories are obtained for this case. It is shown that, in spite of some injection error, spececraft can reach L_1 by optimizing low thrust programs. The other problem treated in this paper pertains to a transfer between collinear Lagrange points, L_1 and L_2,of Sun-Earth system. In this case, two types of low thrust, that is, power-constant and thrust-constant trajectories are studied. In the former case, J-minimum trajectories are obtained, and, in the latter, fuel optimum trajectories with a single coasting arc were sought including optimal steering programs as a function of total mission time. Computational results show that spacecraft can travel between two points within a mission time that stands comparison with high thrust impulsive transfer.","subitem_description_type":"Other"}]},"item_9_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: SA0033407000","subitem_description_type":"Other"}]},"item_9_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"宇宙科学研究所"}]},"item_9_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"Institute of Space and Astronautical Science"}]},"item_9_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"0288-433X","subitem_source_identifier_type":"ISSN"}]},"item_9_source_id_24":{"attribute_name":"書誌レコードID","attribute_value_mlt":[{"subitem_source_identifier":"AA10455137","subitem_source_identifier_type":"NCID"}]},"item_9_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Totsuka Works, Hitachi, Ltd."}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"MATSUO, Hiroki","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"MATOGAWA, Yasunori","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"NOZUE, Tatsuhiro","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"SHIMODA, Toshio","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":"2020-01-23"}],"displaytype":"detail","filename":"SA0033407.pdf","filesize":[{"value":"676.0 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"SA0033407.pdf","url":"https://jaxa.repo.nii.ac.jp/record/31174/files/SA0033407.pdf"},"version_id":"0ee6ccff-1992-4072-b8c9-8da0f6211cb8"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"optimum transfer-low thrust transfer-Lagrange point","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":"departmental bulletin paper","resourceuri":"http://purl.org/coar/resource_type/c_6501"}]},"item_title":"Optimization of Low Thrust Trajectories for Collinear Largrange Point Mission","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"Optimization of Low Thrust Trajectories for Collinear Largrange Point Mission","subitem_title_language":"en"}]},"item_type_id":"9","owner":"1","path":["1890","1991"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"31174","relation_version_is_last":true,"title":["Optimization of Low Thrust Trajectories for Collinear Largrange Point Mission"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T01:08:29.611672+00:00"}