{"created":"2023-06-20T14:40:29.296358+00:00","id":7377,"links":{},"metadata":{"_buckets":{"deposit":"13d845d4-9d9c-43ac-a137-6cc9633165a6"},"_deposit":{"created_by":1,"id":"7377","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"7377"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00007377","sets":["1543:1544:1555","1887:1891"]},"author_link":["39069","39064","39065","39063","39066","39068","39062","39067"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Trajectory Analysis for Small Solarsail Demonstration Spacecraft"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2009-03","bibliographicIssueDateType":"Issued"},"bibliographicVolumeNumber":"2008","bibliographic_titles":[{"bibliographic_title":"アストロダイナミクスシンポジウム講演後刷り集"},{"bibliographic_title":"Proceedings of 18th workshop on JAXA Astrodynamics and flight mechanics","bibliographic_titleLang":"en"}]}]},"item_5_description_15":{"attribute_name":"会議概要（会議名, 開催地, 会期, 主催者等）（英）","attribute_value_mlt":[{"subitem_description":"Symposium on Flight Mechanics and Astrodynamics 2008 (July 28-29, 2008. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)), Sagamihara, Kanagawa Japan","subitem_description_type":"Other"}]},"item_5_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"2010 年打ち上げを前提とした小型ソーラーセイル実証機（Ikaros）の軌道解析を行った．この実証機は深宇宙を航行し，ソーラーセイルによって探査機の軌道を制御することを目的としている．ソーラーセイルは太陽光子圧で推進するため，反射率，宇宙機の姿勢によってその加速度が大きく変化する．そのようなソーラーセイルによる微小加速度を検知するためには，反射率の誤差や姿勢の変動を考慮した軌道決定が必要となる．本研究では，ソーラーセイル実証機の軌道決定のために，反射率，姿勢をパラメータとして，ソーラーセイル加速度による探査機の軌道への影響を明らかにした．","subitem_description_type":"Abstract"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"The trajectory analysis of a small solar sail demonstration spacecraft (Ikaros) is investigated including the uncertainties of the sail's reflectivity and attitude. This spacecraft is assumed to be launched in 2010, and its goal is to control the solar sail trajectory in the interplanetary space. Since solar sail spacecraft is accelerated by solar photons, the sail's reflectivity and its attitude have a significant effect on the trajectory. Therefore, orbit determination for detecting the small force of solar sail is required considering the uncertainty of reflectivity and orientation of the sail. The effect of reflectivity and attitude uncertainty are investigated by comparing the trajectory changing those parameters.","subitem_description_type":"Other"}]},"item_5_description_18":{"attribute_name":"内容記述","attribute_value_mlt":[{"subitem_description":"形態: カラー図版あり","subitem_description_type":"Other"}]},"item_5_description_19":{"attribute_name":"内容記述（英）","attribute_value_mlt":[{"subitem_description":"Physical characteristics: Original contains color illustrations","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0064733003","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)"}]},"item_5_source_id_24":{"attribute_name":"書誌レコードID","attribute_value_mlt":[{"subitem_source_identifier":"AA11567475","subitem_source_identifier_type":"NCID"}]},"item_5_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"総合研究大学院大学"},{"subitem_text_value":"宇宙航空研究開発機構月惑星探査推進グループ"},{"subitem_text_value":"宇宙航空研究開発機構宇宙科学研究本部"},{"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":"Graduate University for Advanced Studies"},{"subitem_text_language":"en","subitem_text_value":"JAXA Space Exploration Center, Japan Aerospace Exploration Agency (JAXA)(JSPEC)"},{"subitem_text_language":"en","subitem_text_value":"Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS)"},{"subitem_text_language":"en","subitem_text_value":"Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS)"}]},"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":"山口, 智宏"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"森本, 睦子"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"竹内, 央"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"吉川, 真"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Yamaguchi, Tomohiro","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Morimoto, Mutsuko Y.","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Takeuchi, Hiroshi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Yoshikawa, Makoto","creatorNameLang":"en"}],"nameIdentifiers":[{}]}]},"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":"conference paper","resourceuri":"http://purl.org/coar/resource_type/c_5794"}]},"item_title":"小型ソーラーセイル実証機の軌道解析","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"小型ソーラーセイル実証機の軌道解析"}]},"item_type_id":"5","owner":"1","path":["1555","1891"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"7377","relation_version_is_last":true,"title":["小型ソーラーセイル実証機の軌道解析"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T07:40:27.527628+00:00"}