{"created":"2023-06-20T14:40:34.414564+00:00","id":7481,"links":{},"metadata":{"_buckets":{"deposit":"e27ba7f0-5f02-42dd-be09-be2108e408a5"},"_deposit":{"created_by":1,"id":"7481","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"7481"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00007481","sets":["1543:1544:1556","1887:1891"]},"author_link":["39876","39880","39878","39875","39879","39877"],"item_5_alternative_title_1":{"attribute_name":"その他のタイトル","attribute_value_mlt":[{"subitem_alternative_title":"発送電一体型パネルを用いたマルチバス太陽発電衛星のダイナミクス"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2008-03","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"274","bibliographicPageStart":"267","bibliographic_titles":[{"bibliographic_title":"第17回アストロダイナミクスシンポジウム講演後刷り集　2007"},{"bibliographic_title":"Proceedings of 17th Workshop on JAXA Astrodynamics and Flight Mechanics","bibliographic_titleLang":"en"}]}]},"item_5_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"本研究では、2006年度にUSEF(Institute for Unmanned Space Experiment Free Flyer)で提案された太陽発電衛星(SPS: Solar Power Satellite)の設計点の安定性を評価している。このSPSは、発送電パネル部、バス部、それらを繋ぐテザーから成る。原案システムと派生型の静的釣合システムに対して、最小ポテンシャルエネルギの原理とシミュレータの2つの方法で、平衡点を求め、安定性を評価する。解析の結果、原案システムはパネルが撓むが安定な平衡点を持ち、静的釣合システムの1つはパネルの撓まない安定な平衡点を持つことが示される。次に、静的釣合システムを柔軟多体系でモデル化してシミュレーションを行う。柔軟多体系でモデル化した場合、パネル弾性変形が現れると剛体多体系での解析結果と異なる解析結果が得られる場合があることが示される。","subitem_description_type":"Abstract"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"This study evaluates stability of the design points of Solar Power Satellites (SPS's) proposed by USEF (Institute for Unmanned Space Experiment Free Flyer) in 2006. The SPS consists of the power generation and transmission panel part, the distributed bus part, and tethers connecting them. For the original system and three types of static balance systems, the equilibrium points are found and their stabilities are evaluated by using the principle of minimum potential energy and the numerical simulations. The original system has the stable equilibrium point whereas the panel part is bent. One of the static balance systems has the stable equilibrium point at the design point where the panel part is flat. Then the static balance system is analyzed again as a flexible multi-body system by numerical simulation. The analysis using a flexible body is slightly different from that of rigid body when the elastic deformation becomes remarkable.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0063718044","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":"金沢大学 大学院自然科学研究科"},{"subitem_text_value":"北海道大学 大学院情報科学研究科"},{"subitem_text_value":"金沢大学 大学院自然科学研究科"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Kanazawa University Graduate School of Natural Science and Technology"},{"subitem_text_language":"en","subitem_text_value":"Hokkaido University Graduate School of Information Science and Technology"},{"subitem_text_language":"en","subitem_text_value":"Kanazawa University Graduate School of Natural Science and 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":"泉田, 啓"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"石村, 康生"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"竹本, 逸史"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Senda, Kei","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Ishimura, Kosei","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Takemoto, Itsushi","creatorNameLang":"en"}],"nameIdentifiers":[{}]}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"太陽発電衛星","subitem_subject_scheme":"Other"},{"subitem_subject":"柔軟体","subitem_subject_scheme":"Other"},{"subitem_subject":"動特性","subitem_subject_scheme":"Other"},{"subitem_subject":"安定性","subitem_subject_scheme":"Other"},{"subitem_subject":"テザー線","subitem_subject_scheme":"Other"},{"subitem_subject":"ソーラーセル","subitem_subject_scheme":"Other"},{"subitem_subject":"宇宙太陽発電システム","subitem_subject_scheme":"Other"},{"subitem_subject":"SPSS","subitem_subject_scheme":"Other"},{"subitem_subject":"柔軟多体系","subitem_subject_scheme":"Other"},{"subitem_subject":"静的釣合システム","subitem_subject_scheme":"Other"},{"subitem_subject":"USEF","subitem_subject_scheme":"Other"},{"subitem_subject":"ポテンシャルエネルギー","subitem_subject_scheme":"Other"},{"subitem_subject":"弾性変形","subitem_subject_scheme":"Other"},{"subitem_subject":"シミュレーション","subitem_subject_scheme":"Other"},{"subitem_subject":"ニュートン・ラプソン法","subitem_subject_scheme":"Other"},{"subitem_subject":"solar power satellite","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"flexible body","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"dynamic characteristic","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"stability","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"tetherline","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"solar cell","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"space solar power system","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"SPSS","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"flexible multi-body system","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"static balance system","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"USEF","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"potential energy","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"elastic deformation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"simulation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Newton-Raphson method","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":"Dynamics of a solar power satellite composed of multi-bus with panels for power generation and transmission","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"Dynamics of a solar power satellite composed of multi-bus with panels for power generation and transmission","subitem_title_language":"en"}]},"item_type_id":"5","owner":"1","path":["1556","1891"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"7481","relation_version_is_last":true,"title":["Dynamics of a solar power satellite composed of multi-bus with panels for power generation and transmission"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T07:38:51.701818+00:00"}