{"created":"2023-06-20T14:40:37.465796+00:00","id":7542,"links":{},"metadata":{"_buckets":{"deposit":"931ed69b-5c8a-4e98-9217-4b9e55d637a2"},"_deposit":{"created_by":1,"id":"7542","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"7542"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00007542","sets":["1543:1544:1557","1887:1891"]},"author_link":["40329","40330"],"item_5_alternative_title_1":{"attribute_name":"その他のタイトル","attribute_value_mlt":[{"subitem_alternative_title":"MV7号機サブペイロード衛星の姿勢制御系について"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2007-03","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"241","bibliographicPageStart":"237","bibliographic_titles":[{"bibliographic_title":"第16回アストロダイナミクスシンポジウム講演後刷り集　2006"},{"bibliographic_title":"Proceedings of 16th Workshop on JAXA Astrodynamics and Flight Mechanics","bibliographic_titleLang":"en"}]}]},"item_5_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"JAXAではスピン展開型のソーラーセイルの研究が行われている。2006年の秋には、スピン展開型ソーラーセイルに必要とされるいくつかの技術の実証の為の小型衛星がMV7号機のサブペイロードとして打ち上げられた。衛星は重量6kg程度であるが、スラスタを持っており、スピンアップ、ニューテーション制御、膜の展開制御の機能を持っていた。本研究ではサブペイロード衛星の姿勢制御系について概観し、展開のシーケンス、制御ロジックおよびシミュレーションの結果を示す。","subitem_description_type":"Abstract"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"A Solar Sail demonstration SATellite (SSSAT) was launched by the 7th MV rocket as the sub-payload in the fall, 2006. The mission of this satellite was to demonstrate the feasibility of the spinning solar sail. The weight of this sub-payload satellite was about 6 kg and its size was also strictly restricted by the small sub-payload space of the rocket. However, the satellite had the spin up, active nutation control and deployment support functions. This paper reviews the configuration of the controller and the outline of the experiment, and evaluates the control performance. And we explain the sequence and the control law of spin-up control, deployment of membrane and spin axis reorientation and the simulation results are shown.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0063481041","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 宇宙科学研究本部"}]},"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 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":"佐伯, 孝尚"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Saiki, Takanao","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":"衛星制御","subitem_subject_scheme":"Other"},{"subitem_subject":"衛星搭載装置","subitem_subject_scheme":"Other"},{"subitem_subject":"衛星回転","subitem_subject_scheme":"Other"},{"subitem_subject":"角速度","subitem_subject_scheme":"Other"},{"subitem_subject":"太陽センサ","subitem_subject_scheme":"Other"},{"subitem_subject":"ニューテーション制御","subitem_subject_scheme":"Other"},{"subitem_subject":"ソーラーセイル","subitem_subject_scheme":"Other"},{"subitem_subject":"展開","subitem_subject_scheme":"Other"},{"subitem_subject":"スピン安定化","subitem_subject_scheme":"Other"},{"subitem_subject":"気液平衡スタスタ","subitem_subject_scheme":"Other"},{"subitem_subject":"太陽角センサ","subitem_subject_scheme":"Other"},{"subitem_subject":"スピンアップ制御","subitem_subject_scheme":"Other"},{"subitem_subject":"SSSAT","subitem_subject_scheme":"Other"},{"subitem_subject":"ソーラ電力セイル実験小型衛星","subitem_subject_scheme":"Other"},{"subitem_subject":"attitude control","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"satellite control","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"satellite-borne instrument","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"satellite rotation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"angular velocity","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"solar sensor","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"nutation control","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"solar sail","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"deployment","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"spin stabilization","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"gas-liquid equilibrium thruster","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"sun angle sensor","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"spin up control","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"SSSAT","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Solarsail Subpayload Satellite","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 system of spinning solar sail sub-payload satellite","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"Attitude control system of spinning solar sail sub-payload satellite","subitem_title_language":"en"}]},"item_type_id":"5","owner":"1","path":["1557","1891"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"7542","relation_version_is_last":true,"title":["Attitude control system of spinning solar sail sub-payload satellite"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T07:37:53.907989+00:00"}