{"created":"2023-06-20T14:40:48.201046+00:00","id":7747,"links":{},"metadata":{"_buckets":{"deposit":"026c63af-fe63-4563-8855-16c004406846"},"_deposit":{"created_by":1,"id":"7747","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"7747"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00007747","sets":["1543:1544:1560","1887:1891"]},"author_link":["41653","41657","41656","41655","41654","41658"],"item_5_alternative_title_1":{"attribute_name":"その他のタイトル","attribute_value_mlt":[{"subitem_alternative_title":"宇宙機間の相対位置の制御について"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2004-02","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"289","bibliographicPageStart":"282","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":"本稿では2機の宇宙機の編隊飛行制御について検討する。推薬消費が最小となるような相対的な軌道変更軌道をHill方程式に基づいて導出し、そのときの推薬量を求める。また軌道変更軌道を実現するような離散的な2自由度制御則を求める。この制御則はデッドビートの特性を有しており、ゲイン低下に対してロバストである。これらの軌道設計および制御を数値的に検証する。","subitem_description_type":"Abstract"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"The formation flight control of two spacecraft is considered in this paper. The trajectory of the relative position change in one spacecraft with respect to the other is designed on the basis of the Hill's equation from the viewpoint of minimum fuel consumption. The total fuel consumed along the trajectory is obtained analytically. Discrete two-degree-of-freedom control law is also proposed in order to realize the designed trajectory. The controller achieves the deadbeat property of the closed loop system and guarantees the robustness to the controller gain decrease. Numerical studies are conducted in order to verify the trajectory generation and the discrete control.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0046652046","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":"三菱電機"},{"subitem_text_value":"三菱電機"},{"subitem_text_value":"三菱電機"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Mitsubishi Electric Corporation"},{"subitem_text_language":"en","subitem_text_value":"Mitsubishi Electric Corporation"},{"subitem_text_language":"en","subitem_text_value":"Mitsubishi Electric Corporation"}]},"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":"山田, 克彦"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"吉河, 章二"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"西山, 岳宏"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Yamada, Katsuhiko","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Yoshikawa, Shoji","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Nishiyama, Takehiro","creatorNameLang":"en"}],"nameIdentifiers":[{}]}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"宇宙機軌道","subitem_subject_scheme":"Other"},{"subitem_subject":"編隊飛行","subitem_subject_scheme":"Other"},{"subitem_subject":"フィードバック制御","subitem_subject_scheme":"Other"},{"subitem_subject":"位置制御","subitem_subject_scheme":"Other"},{"subitem_subject":"速度制御","subitem_subject_scheme":"Other"},{"subitem_subject":"燃料消費","subitem_subject_scheme":"Other"},{"subitem_subject":"DOF","subitem_subject_scheme":"Other"},{"subitem_subject":"数値解析","subitem_subject_scheme":"Other"},{"subitem_subject":"spacecraft trajectory","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"formation flying","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"feedback control","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"position control","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"velocity control","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"fuel consumption","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"DOF","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"numerical analysis","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":"On relative position control between two spacecraft","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"On relative position control between two spacecraft","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":"7747","relation_version_is_last":true,"title":["On relative position control between two spacecraft"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T07:34:41.323938+00:00"}