{"created":"2023-06-20T14:35:55.287483+00:00","id":2215,"links":{},"metadata":{"_buckets":{"deposit":"6ce3e8de-57ff-40b6-8ac2-7ec2f06e9ccd"},"_deposit":{"created_by":1,"id":"2215","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"2215"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00002215","sets":["1887:1893","9:10:200:237"]},"author_link":["4353","4355","4350","4349","4354","4348","4352","4351"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"A study on a new gain scheduling controller synthesis for attitude control of a large flexible satellite"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2007-03-30","bibliographicIssueDateType":"Issued"},"bibliographicVolumeNumber":"JAXA-RR-06-016","bibliographic_titles":[{"bibliographic_title":"宇宙航空研究開発機構研究開発報告"},{"bibliographic_title":"JAXA Research and Development Report","bibliographic_titleLang":"en"}]}]},"item_3_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"筆者らは、将来の大型柔軟構造衛星に必要となる姿勢および振動制御則を確立し、その有効性を軌道上で確認することを目的とする、新しい軌道上制御実験を計画中である。本稿では、計画中の実験に採用予定の制御則の1つである、ゲインスケジューリング制御則の新しい設計手法について論じ、大型柔軟構造衛星の姿勢制御系へ適用するための設計手順について述べる。提案する設計手法では、太陽電池パドルの回転角に応じてダイナミクスが変動する「LPV(Linear Parameter Varying)システム」として制御対象を扱うことができ、パドル角の変化と高次振動モードに対してロバストな制御則を構築することができる。導出される制御則は、従来のゲインスケジューリング制御則と比較して、必要とするメモリ量とスケジュールのための演算負荷が小さいため、搭載計算機能力に制約のある衛星での使用に適している。シミュレーションによって、PD(Proportional-Derivative)制御によるベースライン制御則との比較を行ない、その有効性を明らかにする。","subitem_description_type":"Abstract"}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"A new on-orbit control experiment is being planned aimed at establishing attitude and vibration control methods for future large flexible satellites and demonstrating the effectiveness of the proposed control methods on orbit. In this paper, a new design method for a gain scheduling controller which will be employed in the experiment is described, and a design procedure for an attitude control system for a large flexible satellite is explained. Using this method, a robust control system that is resilient to changes in the paddle rotation angle and higher order vibration modes is designed as this method can treat the satellite system as a Linear Parameter Varying (LPV) system whose dynamics vary according to the paddle rotation angle. The derived gains can be easily scheduled since the scheduling law consists of small number of grid points and requires just linear interpolation calculation. Using this method, stability and performance are guaranteed at each parameter value (paddle angle in this case). Some simulation results are provided to show the effectiveness of our controller.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0063455000","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: JAXA-RR-06-016","subitem_description_type":"Other"}]},"item_3_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"宇宙航空研究開発機構"}]},"item_3_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"Japan Aerospace Exploration Agency (JAXA)"}]},"item_3_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"1349-1113","subitem_source_identifier_type":"ISSN"}]},"item_3_source_id_24":{"attribute_name":"書誌レコードID","attribute_value_mlt":[{"subitem_source_identifier":"AA1192675X","subitem_source_identifier_type":"NCID"}]},"item_3_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"},{"subitem_text_value":"宇宙航空研究開発機構 総合技術研究本部"},{"subitem_text_value":"電気通信大学"},{"subitem_text_value":"電気通信大学"}]},"item_3_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 Aerospace Technology"},{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency Institute of Aerospace Technology"},{"subitem_text_language":"en","subitem_text_value":"University of Electro-Communications"},{"subitem_text_language":"en","subitem_text_value":"University of Electro-Communications"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"濱田, 吉郎"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"大谷, 崇"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"木田, 隆"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"長塩, 知之"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Hamada, Yoshiro","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Otani, Takashi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kida, Takashi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Nagashio, Tomoyuki","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":"2020-01-15"}],"displaytype":"detail","filename":"63455000.pdf","filesize":[{"value":"3.1 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"63455000.pdf","url":"https://jaxa.repo.nii.ac.jp/record/2215/files/63455000.pdf"},"version_id":"7e9fcbf7-b3c7-4d08-89df-2af597832da1"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"ゲインスケジューリング","subitem_subject_scheme":"Other"},{"subitem_subject":"衛星姿勢制御","subitem_subject_scheme":"Other"},{"subitem_subject":"大型柔軟構造衛星","subitem_subject_scheme":"Other"},{"subitem_subject":"大型宇宙構造物","subitem_subject_scheme":"Other"},{"subitem_subject":"構造振動","subitem_subject_scheme":"Other"},{"subitem_subject":"振動減衰","subitem_subject_scheme":"Other"},{"subitem_subject":"姿勢安定性","subitem_subject_scheme":"Other"},{"subitem_subject":"宇宙機安定性","subitem_subject_scheme":"Other"},{"subitem_subject":"オンボード計算機","subitem_subject_scheme":"Other"},{"subitem_subject":"gain scheduling","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"satellite attitude control","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"large flexible satellite","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"large space structure","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"structural vibration","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"vibration damping","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"attitude stability","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"spacecraft stability","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"onboard computer","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":"大型柔軟構造衛星の姿勢制御系へのゲインスケジューリング制御則の適用検討","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"大型柔軟構造衛星の姿勢制御系へのゲインスケジューリング制御則の適用検討"}]},"item_type_id":"3","owner":"1","path":["237","1893"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"2215","relation_version_is_last":true,"title":["大型柔軟構造衛星の姿勢制御系へのゲインスケジューリング制御則の適用検討"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T09:26:30.733807+00:00"}