{"created":"2023-06-20T15:10:05.226566+00:00","id":39679,"links":{},"metadata":{"_buckets":{"deposit":"f87ae152-73d2-4a18-8870-7ff8de56074b"},"_deposit":{"created_by":1,"id":"39679","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"39679"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00039679","sets":["1887:1893","1896:1898:1913:1917"]},"author_link":["443861","443858","443860","443859"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Dynamical model and numerical simulations for engineering test satellite 6"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1993-06","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"18","bibliographicPageStart":"1","bibliographicVolumeNumber":"1239","bibliographic_titles":[{"bibliographic_title":"航空宇宙技術研究所報告"},{"bibliographic_title":"Technical Report of National Aerospace Laboratory","bibliographic_titleLang":"en"}]}]},"item_3_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"1994年度夏期にH-2ロケット2号機で静止軌道上に打ち上げ予定の技術試験衛星6型(ETS-6)は2トン級静止3軸姿勢制御型の実用衛星を実現するための技術基盤を確立することを第1の目的として開発が進められている大型柔軟構造衛星である。当所ではこの衛星のバス系搭載実験のひとつである軌道上柔構造制御実験に宇宙開発事業団との共同研究として実験に参加している。本報告ではこの実験のために導出した動力学モデルの構築と運動方程式とそしてそれらに基づいて作成した数値シミュレーションプログラムについて詳細に記述する。これは打ち上げ前の搭載ソフトウエアの機能・性能評価に使われるためである。また数値例として3種類の制御アルゴリズムについてシミュレーションを行った結果を示す。","subitem_description_type":"Abstract"}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"This report derives the dynamical model of Engineering Test Satellite-6 (ETS-6), which is a large-scale high-performance test satellite launched by H-2 rocket in the summer launch window of 1994. The mission of ETS-6 is to establish the bus technology necessary for realizing a two-ton-class geosynchronous three-axis stabilized application satellite. The National Aerospace Laboratory is participating in the on-orbit flight experiments of ETS-6 for the system identification and attitude control. Numerical simulation software have been developed and used to check the on-board control algorithm before launch. This paper describes their details.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0000099000","subitem_description_type":"Other"}]},"item_3_description_33":{"attribute_name":"レポート番号","attribute_value_mlt":[{"subitem_description":"レポート番号: NAL TR-1239","subitem_description_type":"Other"}]},"item_3_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"航空宇宙技術研究所"}]},"item_3_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"National Aerospace Laboratory (NAL)"}]},"item_3_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"0389-4010","subitem_source_identifier_type":"ISSN"}]},"item_3_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"航空宇宙技術研究所 宇宙研究グループ"},{"subitem_text_value":"航空宇宙技術研究所 宇宙研究グループ"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Space Technology Research Group"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Space Technology Research Group"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"山口, 功"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"木田, 隆"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Yamaguchi, Isao","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kida, Takashi","creatorNameLang":"en"}],"nameIdentifiers":[{}]}]},"item_files":{"attribute_name":"ファイル情報","attribute_type":"file","attribute_value_mlt":[{"accessrole":"open_date","date":[{"dateType":"Available","dateValue":"2020-01-27"}],"displaytype":"detail","filename":"naltr01239.pdf","filesize":[{"value":"1.3 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"naltr01239.pdf","url":"https://jaxa.repo.nii.ac.jp/record/39679/files/naltr01239.pdf"},"version_id":"c056a092-879f-43f1-a28a-7f6be7d3ffef"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"技術試験衛星6","subitem_subject_scheme":"Other"},{"subitem_subject":"ETS-6","subitem_subject_scheme":"Other"},{"subitem_subject":"動力学モデル","subitem_subject_scheme":"Other"},{"subitem_subject":"姿勢制御","subitem_subject_scheme":"Other"},{"subitem_subject":"リアクション制御システム","subitem_subject_scheme":"Other"},{"subitem_subject":"パドル加速度計","subitem_subject_scheme":"Other"},{"subitem_subject":"数値シミュレーション","subitem_subject_scheme":"Other"},{"subitem_subject":"静止軌道","subitem_subject_scheme":"Other"},{"subitem_subject":"大型柔構造","subitem_subject_scheme":"Other"},{"subitem_subject":"太陽電池パドル","subitem_subject_scheme":"Other"},{"subitem_subject":"反射器","subitem_subject_scheme":"Other"},{"subitem_subject":"衛星通信","subitem_subject_scheme":"Other"},{"subitem_subject":"ガスジェットスラスタ","subitem_subject_scheme":"Other"},{"subitem_subject":"振動モード解析","subitem_subject_scheme":"Other"},{"subitem_subject":"engineering test satellite 6","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"ETS 6","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"dynamics model","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"attitude control","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"reaction control system","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"paddle accelerometer","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"numerical simulation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"geostationary orbit","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"large flexible structure","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"solar cell paddle","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"reflector","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"communication satellite","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"gasjet thruster","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"modal vibration analysis","subitem_subject_language":"en","subitem_subject_scheme":"Other"}]},"item_language":{"attribute_name":"言語","attribute_value_mlt":[{"subitem_language":"jpn"}]},"item_resource_type":{"attribute_name":"資源タイプ","attribute_value_mlt":[{"resourcetype":"technical report","resourceuri":"http://purl.org/coar/resource_type/c_18gh"}]},"item_title":"技術試験衛星6型の動力学モデルと数値シミュレーション","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"技術試験衛星6型の動力学モデルと数値シミュレーション"}]},"item_type_id":"3","owner":"1","path":["1893","1917"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"39679","relation_version_is_last":true,"title":["技術試験衛星6型の動力学モデルと数値シミュレーション"],"weko_creator_id":"1","weko_shared_id":1},"updated":"2023-06-20T19:19:48.483742+00:00"}