{"created":"2023-06-20T14:46:46.210357+00:00","id":14348,"links":{},"metadata":{"_buckets":{"deposit":"27fafe5e-1853-42f2-919b-4c7d0d774d9f"},"_deposit":{"created_by":1,"id":"14348","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"14348"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00014348","sets":["1543:1656:1662","1887:1891"]},"author_link":["131356","131357","131355","131354","131359","131358"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Study on Guidance Control Law for Precision Landing of a Reentry Vehicle with Superorbital Velocity"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2011-08","bibliographicIssueDateType":"Issued"},"bibliographic_titles":[{"bibliographic_title":"宇宙航行の力学シンポジウム: 平成22年度"},{"bibliographic_title":"Symposium on Flight Mechanics and Astrodynamics: 2010","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":"宇宙航行の力学シンポジウム 平成22年度 (2010年12月16-17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":"Symposium on Flight Mechanics and Astrodynamics,  2010 (December 16-17, 2010. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency(JAXA)(ISAS)), Sagamihara, Kanagawa Japan","subitem_description_type":"Other"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Lifting flights during reentry are considered as one of the method to reduce total heat flux and load factor. However, small deviations in initial entry conditions around the nominal trajectory will lead to very large terminal errors as for the terminal point in lifting flights compared with ballistic flights. In this study, the guidance control law is derived to reduce terminal errors under various restraint conditions. The guidance control law shows acceptable simulation results and robustness to the changes of entry conditions. Furthermore, acceptable simulations results are shown when using dead zone to reduce change rates of bank angles. Then, characteristics of the guidance control law using dead zone are discussed.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0065106029","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"}]},"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_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"横浜国立大学"},{"subitem_text_value":"宇宙航空研究開発機構宇宙科学研究所 (JAXA)(ISAS)"},{"subitem_text_value":"横浜国立大学"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Yokohama National University"},{"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":"Yokohama National University"}]},"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":"正田, 浩一"}],"nameIdentifiers":[{"nameIdentifier":"131354","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"山田, 哲哉"}],"nameIdentifiers":[{"nameIdentifier":"131355","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"上野, 誠也"}],"nameIdentifiers":[{"nameIdentifier":"131356","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"Shoda, -","creatorNameLang":"en"}],"nameIdentifiers":[{"nameIdentifier":"131357","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"Yamada, Tetsuya","creatorNameLang":"en"}],"nameIdentifiers":[{"nameIdentifier":"131358","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"Ueno, Seiya","creatorNameLang":"en"}],"nameIdentifiers":[{"nameIdentifier":"131359","nameIdentifierScheme":"WEKO"}]}]},"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":"超軌道速度を持つ再突入宇宙機の定点着地誘導に関する研究","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"超軌道速度を持つ再突入宇宙機の定点着地誘導に関する研究"}]},"item_type_id":"5","owner":"1","path":["1662","1891"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"14348","relation_version_is_last":true,"title":["超軌道速度を持つ再突入宇宙機の定点着地誘導に関する研究"],"weko_creator_id":"1","weko_shared_id":1},"updated":"2023-06-20T20:22:40.742521+00:00"}