{"created":"2023-06-20T14:39:12.134072+00:00","id":5897,"links":{},"metadata":{"_buckets":{"deposit":"d82c71f5-718a-4093-88a0-c1dac19dc5e8"},"_deposit":{"created_by":1,"id":"5897","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"5897"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00005897","sets":["1887:1891","9:789:998:1019"]},"author_link":["29137","29138","29135","29136"],"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2007-03-30","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"76","bibliographicPageStart":"69","bibliographicVolumeNumber":"JAXA-SP-06-015","bibliographic_titles":[{"bibliographic_title":"宇宙航空研究開発機構特別資料: 先進的軌道計測・決定技術に関する研究会論文集"},{"bibliographic_title":"JAXA Special Publication: Proceedings of Advanced Orbit Measurement and Orbit Calculation Technologies","bibliographic_titleLang":"en"}]}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Japan Aerospace Exploration Agency (JAXA) is planning the next generation magnetosphere observation mission called 'SCOPE' (cross-Scale Coupling in Plasma universE). SCOPE aims at observing the Earth's magnetotail with five satellites flying in formation to fully resolve the temporary and spatial distribution of the magnetospheric phenomena in the near future. For this observation, the clock synchronization and relative distance measurement between the spacecrafts are essential. This paper describes introduced onboard relative ranging and clock synchronization systems and a robust and efficient approach for relative navigation and parameter estimation of spacecraft flying in formation in general in the main topics. In the main focuses, the approach uses measurements from the optical data that provides a line of sight vector from the master spacecraft to the secondary satellite. State estimation for formation flying is achieved through an optimal observer design. Also, because the rotational and translational motions are coupled through the observation vectors, three approaches are suggested to separate both signals just for stability analysis. Simulation results indicate that the combined sensor/estimator approach provides accurate relative position estimate.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0063223011","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-06-015","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":"宇宙航空研究開発機構 宇宙科学研究本部"},{"subitem_text_value":"宇宙航空研究開発機構 宇宙科学研究本部"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency Institute of Space and Astronautical Science"},{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency Institute of Space and Astronautical Science"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"市川, 勉"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"津田, 雄一"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Ichikawa, Tsutomu","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Tsuda, Yuichi","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":"63223011.pdf","filesize":[{"value":"1.4 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"63223011.pdf","url":"https://jaxa.repo.nii.ac.jp/record/5897/files/63223011.pdf"},"version_id":"329a4da6-823d-41d3-93d5-cb6d9998f54b"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"SCOPE","subitem_subject_scheme":"Other"},{"subitem_subject":"編隊飛行","subitem_subject_scheme":"Other"},{"subitem_subject":"測距","subitem_subject_scheme":"Other"},{"subitem_subject":"時刻の同期","subitem_subject_scheme":"Other"},{"subitem_subject":"位置誤差","subitem_subject_scheme":"Other"},{"subitem_subject":"ステーションキーピング","subitem_subject_scheme":"Other"},{"subitem_subject":"視線","subitem_subject_scheme":"Other"},{"subitem_subject":"カルマンフィルタ","subitem_subject_scheme":"Other"},{"subitem_subject":"観測方程式","subitem_subject_scheme":"Other"},{"subitem_subject":"相対高度","subitem_subject_scheme":"Other"},{"subitem_subject":"相対航法","subitem_subject_scheme":"Other"},{"subitem_subject":"航法","subitem_subject_scheme":"Other"},{"subitem_subject":"軌道決定","subitem_subject_scheme":"Other"},{"subitem_subject":"SCOPE","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"formation flying","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"rangefinding","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"time synchronization","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"position error","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"stationkeeping","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"line of sight","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Kalman filter","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"observation equation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"relative attitude","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"relative navigation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"navigation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"orbit determination","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":"The navigation for Formation flying of spacecraft","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"The navigation for Formation flying of spacecraft","subitem_title_language":"en"}]},"item_type_id":"5","owner":"1","path":["1019","1891"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"5897","relation_version_is_last":true,"title":["The navigation for Formation flying of spacecraft"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T08:06:24.241532+00:00"}