{"created":"2023-06-20T14:49:34.434252+00:00","id":17449,"links":{},"metadata":{"_buckets":{"deposit":"5ebf618b-f405-404e-b0b9-4dc002a81715"},"_deposit":{"created_by":1,"id":"17449","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"17449"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00017449","sets":["1543:1693:1711","1887:1891"]},"author_link":["158335","158332","158333","158334"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Ascent trajectory optimization of a space plane considering rigid body dynamics"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2002-04","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"86","bibliographicPageStart":"83","bibliographic_titles":[{"bibliographic_title":"宇宙輸送シンポジウム　平成13年度"},{"bibliographic_title":"Proceedings of Space Transportation Symposium FY2001","bibliographic_titleLang":"en"}]}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"In the past studies on the ascent trajectory optimization of a space plane, mass point approximation is usually used to simplify the problem. However, the validity of those obtained trajectory must be verified under the more precise dynamics model. Especially; if the rigid body dynamics is considered, the attitude control system and vehicle's flight trajectory usually have a strong coupling. Therefore, this study considers the trajectory optimization of a SSTO with the rigid body dynamics. New proposed method, in which the guidance law and the attitude control system are optimized simultaneously, is compared with the conventional method, in which the guidance law and the attitude control system are optimized sequentially, and the advantages of the new method are demonstrated.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0033392021","subitem_description_type":"Other"}]},"item_5_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"宇宙科学研究所"}]},"item_5_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"The Institute of Space and Astronautical Science (ISAS)"}]},"item_5_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"東京大学 大学院工学系研究科"},{"subitem_text_value":"東京大学 工学部"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"University of Tokyo Graduate School of Engineering"},{"subitem_text_language":"en","subitem_text_value":"University of Tokyo Faculty of Engineering"}]},"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":"横山, 信宏"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"鈴木, 真二"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Yokoyama, Nobuhiro","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Suzuki, Shinji","creatorNameLang":"en"}],"nameIdentifiers":[{}]}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"上昇飛行経路","subitem_subject_scheme":"Other"},{"subitem_subject":"飛行経路最適化","subitem_subject_scheme":"Other"},{"subitem_subject":"スペースプレーン","subitem_subject_scheme":"Other"},{"subitem_subject":"SSTO","subitem_subject_scheme":"Other"},{"subitem_subject":"剛体ダイナミクス","subitem_subject_scheme":"Other"},{"subitem_subject":"ascent trajectory","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"trajectory optimization","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"spaceplane","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"SSTO","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"rigid body dynamics","subitem_subject_language":"en","subitem_subject_scheme":"Other"}]},"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":"剛体ダイナミクスを考慮した宇宙往還機の上昇飛行経路最適化","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"剛体ダイナミクスを考慮した宇宙往還機の上昇飛行経路最適化"}]},"item_type_id":"5","owner":"1","path":["1711","1891"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"17449","relation_version_is_last":true,"title":["剛体ダイナミクスを考慮した宇宙往還機の上昇飛行経路最適化"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T04:38:01.626174+00:00"}