{"created":"2023-06-20T14:38:56.716083+00:00","id":5590,"links":{},"metadata":{"_buckets":{"deposit":"36888536-d148-4b12-8e37-ff1a55e0c4f8"},"_deposit":{"created_by":1,"id":"5590","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"5590"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00005590","sets":["1887:1891","9:789:972:982"]},"author_link":["27349","27350"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Application of formation flying control with low thrust satellites"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2008-02-29","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"55","bibliographicPageStart":"49","bibliographicVolumeNumber":"JAXA-SP-07-020","bibliographic_titles":[{"bibliographic_title":"宇宙航空研究開発機構特別資料: 低推力・連続加速を用いた宇宙ミッションに関する研究会論文集"},{"bibliographic_title":"JAXA Special Publication: Collection of Papers Presented at the Meeting on the Study of Space Missions Propelled by Low-Thrust and Sustained Acceleration","bibliographic_titleLang":"en"}]}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Future scientific missions such as virtual telescope and interferometer require precise formation flying where relative positions of spacecraft are controlled very precisely. A feature of the low thrust that the minimum impulse is small is very attractive for such applications. This paper takes an along-track formation control in low earth orbit as an example and numerically investigates how the size of minimum impulse affects control accuracy under the two representative natural disturbances (J2 term and air drag).","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0063739008","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-07-020","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":"三菱電機 先端技術総合研究所"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Mitsubishi Electric Corporation Advanced Technology R & D Center"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"吉河, 章二"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Yoshikawa, Shoji","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":"63739008.pdf","filesize":[{"value":"1.3 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"63739008.pdf","url":"https://jaxa.repo.nii.ac.jp/record/5590/files/63739008.pdf"},"version_id":"23fe0b18-5d83-4b5e-bc54-55089fc10eef"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"低推力推進","subitem_subject_scheme":"Other"},{"subitem_subject":"編隊飛行","subitem_subject_scheme":"Other"},{"subitem_subject":"衛星配置","subitem_subject_scheme":"Other"},{"subitem_subject":"最小インパルス","subitem_subject_scheme":"Other"},{"subitem_subject":"低高度地球周回軌道","subitem_subject_scheme":"Other"},{"subitem_subject":"超長基線干渉法","subitem_subject_scheme":"Other"},{"subitem_subject":"衛星姿勢制御","subitem_subject_scheme":"Other"},{"subitem_subject":"数値解析","subitem_subject_scheme":"Other"},{"subitem_subject":"座標系","subitem_subject_scheme":"Other"},{"subitem_subject":"low thrust propulsion","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"formation flying","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"satellite constellation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"minimum impulse","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"low Earth orbit","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"very long base interferometry","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"satellite attitude control","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"numerical analysis","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"coordinate system","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":"低推力を用いた編隊飛行制御の応用","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"低推力を用いた編隊飛行制御の応用"}]},"item_type_id":"5","owner":"1","path":["982","1891"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"5590","relation_version_is_last":true,"title":["低推力を用いた編隊飛行制御の応用"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T08:11:34.794942+00:00"}