{"created":"2023-06-20T15:05:14.957541+00:00","id":34529,"links":{},"metadata":{"_buckets":{"deposit":"da20a6f6-eb4f-4929-9a37-87924949f6ed"},"_deposit":{"created_by":1,"id":"34529","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"34529"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00034529","sets":["1887:1890","1896:1898:1899:1992"]},"author_link":["419768"],"item_9_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1977-11","bibliographicIssueDateType":"Issued"},"bibliographicIssueNumber":"6","bibliographicPageEnd":"207","bibliographicPageStart":"167","bibliographicVolumeNumber":"42","bibliographic_titles":[{},{"bibliographic_title":"ISAS report/Institute of Space and Aeronautical Science,University of Tokyo","bibliographic_titleLang":"en"}]}]},"item_9_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"The problem of multiple rendezvous with low-thrust propulsion systems is discussed. The motivation of this problem is given by the necessity of the space sweep mission in future which will aim to revover or deorbit several mission completed orbiting bodies in succession. Optimization parameter is the fuel consumption required to complete a multiple rendezvous in a given mission time. Optimum targeting sequence and time allocation to each rendezvous are determined by a simple method developed on the basis of a linear theory. Solutions are obtainable not only for the case of variable thrust mode but for the case of constant thrust mode of low-thrust propulsion systems. Some numerical examples for the verification of the developed methods are presented and the feasibility of low-thrust propelled space sweeper is discussed.","subitem_description_type":"Other"}]},"item_9_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: SA2401275000","subitem_description_type":"Other"}]},"item_9_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"東京大学宇宙航空研究所"}]},"item_9_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"Institute of Space and Aeronautical Science,University of Tokyo"}]},"item_9_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"0372-1418","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":"AA00675986","subitem_source_identifier_type":"NCID"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"UESUGI, Kuninori","creatorNameLang":"en"}],"nameIdentifiers":[{"nameIdentifier":"419768","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":"2020-01-24"}],"displaytype":"detail","filename":"SA2401275.pdf","filesize":[{"value":"2.3 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"SA2401275.pdf","url":"https://jaxa.repo.nii.ac.jp/record/34529/files/SA2401275.pdf"},"version_id":"121a8efb-0068-4c02-8b94-208beb770b01"}]},"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":"Optimum Low-Thrust Multiple Rendezvous","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"Optimum Low-Thrust Multiple Rendezvous","subitem_title_language":"en"}]},"item_type_id":"9","owner":"1","path":["1890","1992"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"34529","relation_version_is_last":true,"title":["Optimum Low-Thrust Multiple Rendezvous"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T23:40:13.768192+00:00"}