{"created":"2023-06-20T14:40:47.364257+00:00","id":7728,"links":{},"metadata":{"_buckets":{"deposit":"b9cbb1ca-4434-4472-975f-a125b695020d"},"_deposit":{"created_by":1,"id":"7728","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"7728"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00007728","sets":["1543:1544:1560","1887:1891"]},"author_link":["41531","41532","41527","41530","41529","41528"],"item_5_alternative_title_1":{"attribute_name":"その他のタイトル","attribute_value_mlt":[{"subitem_alternative_title":"2ホイール衛星の姿勢マヌーバ経路を指定した姿勢制御法の提案"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2004-02","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"173","bibliographicPageStart":"168","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":"2つのホイールで衛星の姿勢を制御する場合、衛星は非ホロノミックな拘束を受けるため、姿勢変化の軌道をうまく取ることで、姿勢の3次元を目標値に収束させることができる。これまでに、衛星の姿勢を単位球面上に射影して姿勢を表す手法の提案を行ってきた。本論文では、姿勢変化の軌道の設計と、その軌道に沿ったフィードバック制御手法の提案を行う。","subitem_description_type":"Abstract"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Attitude of a satellite is controllable using two reaction wheels. In many cases, there exist prohibited directions that satellites must not point in due to the constraints of optical sensors. In these cases, the maneuver path planning and the feedback control are essential for the attitude maneuver using two reaction wheels. In this paper, attitude of a satellite is projected on a unit spherical surface and maneuver path is planned on the spherical surface. A feedback controller is designed using an area between a planned path and an actual path. Stability and controllability are shown by simulation results.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0046652027","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":"東京大学"},{"subitem_text_value":"宇宙科学研究所"},{"subitem_text_value":"宇宙科学研究所"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"University of Tokyo"},{"subitem_text_language":"en","subitem_text_value":"Institute of Space and Astronautical Science"},{"subitem_text_language":"en","subitem_text_value":"Institute of Space and Astronautical Science"}]},"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":"下田, 真吾"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"久保田, 孝"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"中谷, 一郎"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Shimoda, Shingo","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kubota, Takashi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Nakatani, Ichiro","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":"リアクションホイール","subitem_subject_scheme":"Other"},{"subitem_subject":"人工衛星","subitem_subject_scheme":"Other"},{"subitem_subject":"光学センサー","subitem_subject_scheme":"Other"},{"subitem_subject":"フィードバック制御","subitem_subject_scheme":"Other"},{"subitem_subject":"シミュレーション","subitem_subject_scheme":"Other"},{"subitem_subject":"球表面","subitem_subject_scheme":"Other"},{"subitem_subject":"拘束方程式","subitem_subject_scheme":"Other"},{"subitem_subject":"attitude control","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"reaction wheel","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"artificial satellite","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"optical sensor","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"feedback control","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"simulation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"spherical surface","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"constraint equation","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":"Attitude control of two-wheel-satellite considering maneuver path","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"Attitude control of two-wheel-satellite considering maneuver path","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":"7728","relation_version_is_last":true,"title":["Attitude control of two-wheel-satellite considering maneuver path"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T07:34:59.009069+00:00"}