{"created":"2023-06-20T14:40:46.705824+00:00","id":7713,"links":{},"metadata":{"_buckets":{"deposit":"2f86cab7-5bdb-4508-a905-f1584e189e14"},"_deposit":{"created_by":1,"id":"7713","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"7713"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00007713","sets":["1543:1544:1560","1887:1891"]},"author_link":["41434","41435","41433","41436"],"item_5_alternative_title_1":{"attribute_name":"その他のタイトル","attribute_value_mlt":[{"subitem_alternative_title":"繰り返しインパルス入力によるタンブリング衛星の角運動量制御"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2004-02","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"83","bibliographicPageStart":"76","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":"外部から繰り返しインパルスを入力することでタンブリング衛星の角運動量を減衰させる制御において、接触モデルにゲイン不確定性がある場合に角運動量が0収束する条件について考察する。","subitem_description_type":"Abstract"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"An angular momentum control of a tumbling spacecraft is discussed. The proposed control method is to apply an impulse by a space robot arm, to measure and control the relative position and attitude between the target spacecraft, and then to apply another impulse until the rotational motion of the target spacecraft is well damped. A discrete controller is designed using the simplified equations of rotational motion through appropriate coordinate transformation. The stationary response under contact model uncertainty is investigated and stability condition is analytically derived. Numerical simulations are given to validate the proposed approach.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0046652012","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"}]},"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"}]},"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":"吉河, 章二"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"山田, 克彦"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Yoshikawa, Shoji","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Yamada, Katsuhiko","creatorNameLang":"en"}],"nameIdentifiers":[{}]}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"角運動量制御","subitem_subject_scheme":"Other"},{"subitem_subject":"タンブリング宇宙機","subitem_subject_scheme":"Other"},{"subitem_subject":"反復衝撃入力","subitem_subject_scheme":"Other"},{"subitem_subject":"宇宙ロボットアーム","subitem_subject_scheme":"Other"},{"subitem_subject":"標的宇宙機","subitem_subject_scheme":"Other"},{"subitem_subject":"数値シミュレーション","subitem_subject_scheme":"Other"},{"subitem_subject":"モデル","subitem_subject_scheme":"Other"},{"subitem_subject":"安定条件","subitem_subject_scheme":"Other"},{"subitem_subject":"angular momentum control","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"tumbling spacecraft","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"repetitive impulse input","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"space robot arm","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"target spacecraft","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"numerical simulation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"model","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"stability condition","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":"Angular momentum control of tumbling spacecraft by repetitive impulse inputs","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"Angular momentum control of tumbling spacecraft by repetitive impulse inputs","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":"7713","relation_version_is_last":true,"title":["Angular momentum control of tumbling spacecraft by repetitive impulse inputs"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T07:35:13.292957+00:00"}