{"created":"2023-06-20T14:40:24.363690+00:00","id":7285,"links":{},"metadata":{"_buckets":{"deposit":"8b7a3bb5-537c-4f73-8f53-7c58f57c27e1"},"_deposit":{"created_by":1,"id":"7285","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"7285"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00007285","sets":["1543:1544:1553","1887:1891"]},"author_link":["38491","38496","38494","38495","38492","38493"],"item_5_alternative_title_1":{"attribute_name":"その他のタイトル","attribute_value_mlt":[{"subitem_alternative_title":"複数マーカを用いた小惑星探査機の着陸戦略"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2011-03","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"237","bibliographicPageStart":"232","bibliographicVolumeNumber":"20","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":"The 20th Workshop on JAXA Astrodynamics and Flight Mechanics","bibliographic_titleLang":"en"}]}]},"item_5_description_14":{"attribute_name":"会議概要（会議名, 開催地, 会期, 主催者等）","attribute_value_mlt":[{"subitem_description":"第20回アストロダイナミクスシンポジウム (2010年7月26-27日. 宇宙航空研究開発機構宇宙科学研究所), 相模原市, 神奈川県　","subitem_description_type":"Other"}]},"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":"The 20th Workshop on JAXA Astrodynamics and Flight Mechanics 2010 (July 26-27, 2010. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS)), Sagamihara, Kanagawa Japan","subitem_description_type":"Other"}]},"item_5_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"摘要: 小惑星探査機の小惑星表面への着陸精度を向上させるための一手法を提案する．小惑星表面に複数のマーカを順次落としていく2種類のシナリオを提案する．簡単なモンテカルロシミュレーションにより，マーカが1個の場合よりも着陸精度が向上することが示された．","subitem_description_type":"Abstract"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"We propose a novel strategy for precise landing of a space probe on an asteroid surface. In this paper, we propose two scenarios to drop multiple markers one by one, with a view to more precise landing. Preliminary Monte Carlo simulation of guidance using multiple markers with assumption of some control errors are presented. It was indicated that more than one markers allow us to increase the landing accuracy compared to the conventional method using a single marker.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0065115038","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所 (JAXA)(ISAS)"}]},"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_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":"宇宙航空研究開発機構月・惑星探査プログラムグループ (JAXA)(JSPEC)"},{"subitem_text_value":"宇宙航空研究開発機構月・惑星探査プログラムグループ (JAXA)(JSPEC) : 宇宙航空研究開発機構研究開発本部"},{"subitem_text_value":"宇宙航空研究開発機構月・惑星探査プログラムグループ (JAXA)(JSPEC)"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"JAXA Space Exploration Center, Japan Aerospace Exploration Agency (JAXA)(JSPEC)"},{"subitem_text_language":"en","subitem_text_value":"JAXA Space Exploration Center, Japan Aerospace Exploration Agency (JAXA)(JSPEC) : Aerospace Research and Development Directorate, Japan Aerospace Exploration Agency (JAXA)"},{"subitem_text_language":"en","subitem_text_value":"JAXA Space Exploration Center, Japan Aerospace Exploration Agency (JAXA)(JSPEC)"}]},"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":"尾川, 順子"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"照井, 冬人"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"川口, 淳一郎"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Ogawa, Naoko","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Terui, Fuyuto","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kawaguchi, Junichiro","creatorNameLang":"en"}],"nameIdentifiers":[{}]}]},"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":"Landing Strategy of Asteroid Probe Using Multiple Markers","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"Landing Strategy of Asteroid Probe Using Multiple Markers","subitem_title_language":"en"}]},"item_type_id":"5","owner":"1","path":["1553","1891"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"7285","relation_version_is_last":true,"title":["Landing Strategy of Asteroid Probe Using Multiple Markers"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T07:41:52.169422+00:00"}