{"created":"2023-06-20T14:40:41.712312+00:00","id":7612,"links":{},"metadata":{"_buckets":{"deposit":"23f003b1-753c-46bb-96a6-232ecabc51db"},"_deposit":{"created_by":1,"id":"7612","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"7612"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00007612","sets":["1543:1544:1558","1887:1891"]},"author_link":["40771","40772"],"item_5_alternative_title_1":{"attribute_name":"その他のタイトル","attribute_value_mlt":[{"subitem_alternative_title":"初期角運動量を持つ衛星の2ホイールによる最小エネルギー姿勢変更"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2006-03","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"299","bibliographicPageStart":"296","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":"筆者らはこれまでに、2ホイール衛星の姿勢変更について、エネルギ最小制御則を議論してきた。これらは、姿勢変更をホイールの存在しない軸周りの姿勢変更に限定して検討を行ってきた。本論では、3軸の慣性モーメント比が2軸対称、1軸非対称の初期角運動量を持つ衛星(バイアスモーメンタム衛星を含む)の3軸姿勢制御について角運動量保存の観点から安定化可能な姿勢について議論するため、数値最適解をニューテーション周期と比較した。結果、最適解とニューテーション周期の相関は見られなかった。","subitem_description_type":"Abstract"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Authors have been discussing the energy minimum control low about the satellite maneuver with only two reaction wheel. The maneuver is limited around the axis where the wheel doesn't exist and these have been being examined. This paper discuss about the energy minimum control low of satellite having initial angular momentum. That is included the bias momentum satellite. The satellite's moment of inertia is axisymmetric. The attitude stability of satellite on three-axis pointing control is discussed from the point of angular momentum preservation rule. Moreover, a numerical solution is compared with the Nutation cycle.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0063480047","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":"宇宙航空研究開発機構 総合技術研究本部"}]},"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 Technology and Aeronautics"}]},"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":"遠藤, 達也"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Endo, Tatsuya","creatorNameLang":"en"}],"nameIdentifiers":[{}]}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"姿勢制御","subitem_subject_scheme":"Other"},{"subitem_subject":"姿勢安定性","subitem_subject_scheme":"Other"},{"subitem_subject":"ホイール衛星","subitem_subject_scheme":"Other"},{"subitem_subject":"リアクションホイール","subitem_subject_scheme":"Other"},{"subitem_subject":"バイアスモーメンタム衛星","subitem_subject_scheme":"Other"},{"subitem_subject":"衛星制御","subitem_subject_scheme":"Other"},{"subitem_subject":"最適制御","subitem_subject_scheme":"Other"},{"subitem_subject":"角運動量","subitem_subject_scheme":"Other"},{"subitem_subject":"ニューテーション","subitem_subject_scheme":"Other"},{"subitem_subject":"角速度","subitem_subject_scheme":"Other"},{"subitem_subject":"制御則","subitem_subject_scheme":"Other"},{"subitem_subject":"最小エネルギー軌道","subitem_subject_scheme":"Other"},{"subitem_subject":"数値解析","subitem_subject_scheme":"Other"},{"subitem_subject":"attitude control","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"attitude stability","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"wheel satellite","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"reaction wheel","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"bias momentum satellite","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"satellite control","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"optimal control","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"angular momentum","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"nutation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"angular velocity","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"control law","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"minimum energy trajectory","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":"Optimization of three axis control of two wheel satellite with initial angular momentum","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"Optimization of three axis control of two wheel satellite with initial angular momentum","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":"7612","relation_version_is_last":true,"title":["Optimization of three axis control of two wheel satellite with initial angular momentum"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T07:36:47.786725+00:00"}