{"created":"2023-06-20T14:40:48.725432+00:00","id":7759,"links":{},"metadata":{"_buckets":{"deposit":"e234073a-6366-4767-af7a-b13986fbbd51"},"_deposit":{"created_by":1,"id":"7759","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"7759"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00007759","sets":["1543:1544:1560","1887:1891"]},"author_link":["41723","41726","41722","41721","41728","41725","41727","41724"],"item_5_alternative_title_1":{"attribute_name":"その他のタイトル","attribute_value_mlt":[{"subitem_alternative_title":"柔軟宇宙構造物のスルーマヌーバに対するInput shapingの適用"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2004-02","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"363","bibliographicPageStart":"356","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":"柔軟宇宙構造物のrest-to-restスルーマヌーバにおいて、曲げモーメント拘束つきInput Shapingを適用し、実験的に検証を行う。曲げモーメント拘束つきInput Shapingは、移動過程における曲げモーメントの大きさをある一定値以下に抑えながら、rest-to-restスルーマヌーバを行うための制御手法であり、その制御入力は、残留振動、移動距離、曲げモーメントの拘束条件を満たしながら、移動時間を最小にするようにして求められる。用いた柔軟宇宙構造物モデルは、柔軟梁が付属した剛体の台車から成っている。実験により、曲げモーメント拘束つきInput Shapingの有効性が示される。","subitem_description_type":"Abstract"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"The Deflection-Limiting Input Shaping for the rest-to-rest maneuver of flexible space structures is demonstrated experimentally. The deflection-limiting input shaping is the method for slewing flexible space structures with both suppression of deflection during the slew and elimination of residual oscillations. The method minimizes the maneuver time subject to constraints on residual vibration magnitude, rest-to-rest distance, and the transient deflection amplitude. A model employed in the experiment is a rigid body equipped with a flexible appendage. Results of the experiment show satisfactory performance.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0046652058","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":"東京都立科学技術大学"},{"subitem_text_value":"東京都立科学技術大学"},{"subitem_text_value":"東京都立科学技術大学"},{"subitem_text_value":"Georgia Institute of Technology"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Tokyo Metropolitan Institute of Technology"},{"subitem_text_language":"en","subitem_text_value":"Tokyo Metropolitan Institute of Technology"},{"subitem_text_language":"en","subitem_text_value":"Tokyo Metropolitan Institute of Technology"},{"subitem_text_language":"en","subitem_text_value":"Georgia Institute of Technology"}]},"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":"藤井, 裕矩"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"田中, 成和"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"小島, 広久"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Robertson, Michael J."}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Fujii, Hironori A.","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Tanaka, Shigekazu","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kojima, Hirohisa","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Robertson, Michael J.","creatorNameLang":"en"}],"nameIdentifiers":[{}]}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"柔軟宇宙構造体","subitem_subject_scheme":"Other"},{"subitem_subject":"スルーイング操縦","subitem_subject_scheme":"Other"},{"subitem_subject":"歪曲","subitem_subject_scheme":"Other"},{"subitem_subject":"振動","subitem_subject_scheme":"Other"},{"subitem_subject":"モデル","subitem_subject_scheme":"Other"},{"subitem_subject":"境界条件","subitem_subject_scheme":"Other"},{"subitem_subject":"入力形状制御","subitem_subject_scheme":"Other"},{"subitem_subject":"数値シミュレーション","subitem_subject_scheme":"Other"},{"subitem_subject":"flexible space structure","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"slewing maneuver","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"deflection","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"oscillation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"model","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"boundary condition","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"input shaping control","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"numerical simulation","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":"Application of input shaping control to slew maneuver problem of a flexible space structure","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"Application of input shaping control to slew maneuver problem of a flexible space structure","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":"7759","relation_version_is_last":true,"title":["Application of input shaping control to slew maneuver problem of a flexible space structure"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T07:34:29.935985+00:00"}