{"created":"2023-06-20T14:40:41.911920+00:00","id":7615,"links":{},"metadata":{"_buckets":{"deposit":"6988927a-187e-450f-b262-1d0a01fe18a1"},"_deposit":{"created_by":1,"id":"7615","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"7615"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00007615","sets":["1543:1544:1558","1887:1891"]},"author_link":["40787","40788","40786","40785"],"item_5_alternative_title_1":{"attribute_name":"その他のタイトル","attribute_value_mlt":[{"subitem_alternative_title":"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":"2006-03","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"327","bibliographicPageStart":"320","bibliographic_titles":[{"bibliographic_title":"第15回アストロダイナミクスシンポジウム講演後刷り集　2005"},{"bibliographic_title":"Proceedings of 15th Workshop on JAXA Astrodynamics and Flight Mechanics","bibliographic_titleLang":"en"}]}]},"item_5_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"タンブリング状態にある故障衛星に外力を加えることでその角運動量を減衰させる問題において、特に繰り返しインパルスを入力とする場合の制御上の特徴について検討する。","subitem_description_type":"Abstract"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"We discuss an angular momentum control of a tumbling spacecraft. 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: AA0063480050","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_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"三菱電機"},{"subitem_text_value":"名古屋大学"}]},"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":"Nagoya University"}]},"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":"衛星制御","subitem_subject_scheme":"Other"},{"subitem_subject":"タンブリング運動","subitem_subject_scheme":"Other"},{"subitem_subject":"角運動量","subitem_subject_scheme":"Other"},{"subitem_subject":"運動方程式","subitem_subject_scheme":"Other"},{"subitem_subject":"制御理論","subitem_subject_scheme":"Other"},{"subitem_subject":"モデルの不確実性","subitem_subject_scheme":"Other"},{"subitem_subject":"安定性条件","subitem_subject_scheme":"Other"},{"subitem_subject":"2分岐条件","subitem_subject_scheme":"Other"},{"subitem_subject":"制御則","subitem_subject_scheme":"Other"},{"subitem_subject":"ロボットアーム","subitem_subject_scheme":"Other"},{"subitem_subject":"衝撃","subitem_subject_scheme":"Other"},{"subitem_subject":"制御シミュレーション","subitem_subject_scheme":"Other"},{"subitem_subject":"安定化","subitem_subject_scheme":"Other"},{"subitem_subject":"satellite control","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"tumbling motion","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"angular momentum","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"equation of motion","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"control theory","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"model uncertainty","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"stability condition","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"bifurcation condition","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"control law","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"robot arm","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"impulse","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"control simulation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"stabilization","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","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"Angular momentum control of tumbling spacecraft","subitem_title_language":"en"}]},"item_type_id":"5","owner":"1","path":["1558","1891"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"7615","relation_version_is_last":true,"title":["Angular momentum control of tumbling spacecraft"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T07:36:45.005731+00:00"}