{"created":"2023-06-20T15:14:30.957205+00:00","id":44507,"links":{},"metadata":{"_buckets":{"deposit":"e6596e9e-7158-46fa-88d0-02c211e8716e"},"_deposit":{"created_by":1,"id":"44507","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"44507"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00044507","sets":["1887:1893","1896:1898:1913:1917"]},"author_link":["469770","469771","469768","469769"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Flight Control System Design for Launch Vehicles with Liquid Propellant"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1972-01","bibliographicIssueDateType":"Issued"},"bibliographicPageStart":"40","bibliographicVolumeNumber":"264","bibliographic_titles":[{"bibliographic_title":"航空宇宙技術研究所報告"},{"bibliographic_title":"Technical Report of National Aerospace Laboratory TR-264","bibliographic_titleLang":"en"}]}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"A system study has been performed to construct a model launch vehicle for a geostationary satellite by Space Technology Research Group of NAL.As a part of the study, this research was executed to provide the synthetic procedure and techniques of designing the flight control system for the boost stage of this class of vehicles, and also to present the characteristics of the prototype of the model vehicle, SS-3. This report covers(1) the derivation of relating equations, (2) the system characterization with the aids of trajectory simulations, (3) the computing methods for flexible vehicle stabilization, and (4) the discussion about calculating methods of loads on the vehicle by the effects of the wind. The computer programs for drawing Nyquist plot, Bode plot and root locus of a high order system with multiple feedback loops were worked out and used for the third problem. They will have general applications in the stability analysis of multivariable control systems.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: NALTR0264000","subitem_description_type":"Other"}]},"item_3_description_33":{"attribute_name":"レポート番号","attribute_value_mlt":[{"subitem_description":"レポート番号: NAL TR-264","subitem_description_type":"Other"}]},"item_3_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"航空宇宙技術研究所"}]},"item_3_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"National Aerospace Laboratory(NAL)"}]},"item_3_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"0389-4010","subitem_source_identifier_type":"ISSN"}]},"item_3_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"航空宇宙技術研究所宇宙研究グループ"},{"subitem_text_value":"航空宇宙技術研究所宇宙研究グループ"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Space Technology Research Group, National Aerospace Laboratory(NAL)"},{"subitem_text_language":"en","subitem_text_value":"Space Technology Research Group, National Aerospace Laboratory(NAL)"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"森, 英彦"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"輿石, 肇"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"MORI, Hidehiko","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"KOSHIISHI, Hajime","creatorNameLang":"en"}],"nameIdentifiers":[{}]}]},"item_files":{"attribute_name":"ファイル情報","attribute_type":"file","attribute_value_mlt":[{"accessrole":"open_date","date":[{"dateType":"Available","dateValue":"2020-01-29"}],"displaytype":"detail","filename":"naltr00264.pdf","filesize":[{"value":"2.7 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"naltr00264.pdf","url":"https://jaxa.repo.nii.ac.jp/record/44507/files/naltr00264.pdf"},"version_id":"815a41eb-de4a-448b-8a89-24e9f8b8baa7"}]},"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":"technical report","resourceuri":"http://purl.org/coar/resource_type/c_18gh"}]},"item_title":"液体燃料ロケットを用いた衛星打上げ用飛しょう体の初段に関する制御系構成","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"液体燃料ロケットを用いた衛星打上げ用飛しょう体の初段に関する制御系構成"}]},"item_type_id":"3","owner":"1","path":["1893","1917"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"44507","relation_version_is_last":true,"title":["液体燃料ロケットを用いた衛星打上げ用飛しょう体の初段に関する制御系構成"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T21:55:50.433508+00:00"}