{"created":"2023-06-20T14:35:47.182714+00:00","id":2065,"links":{},"metadata":{"_buckets":{"deposit":"47502dfb-0e50-4db3-8b6d-1e3dd0048fdc"},"_deposit":{"created_by":1,"id":"2065","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"2065"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00002065","sets":["1887:1893","9:10:106:114"]},"author_link":["2755","2753","2754","2752","2756","2751"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Guidance and Control System for Lifting Body Flight Experiment (LIFLEX): Flight Control System Design"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2010-11-30","bibliographicIssueDateType":"Issued"},"bibliographicVolumeNumber":"JAXA-RR-10-006","bibliographic_titles":[{"bibliographic_title":"宇宙航空研究開発機構研究開発報告"},{"bibliographic_title":"JAXA Research and Development Report","bibliographic_titleLang":"en"}]}]},"item_3_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"将来の宇宙往還機システムとして有望視されるものの一つとして，リフティングボディ往還機の概念がある．JAXAでは，リフティングボディ往還機を実現する上で重要な技術課題の一つである自動着陸技術の開発を主目的として，リフティングボディ飛行実験 LIFLEX(Lifting-body FLight EXperiment)を計画していた．筆者らはLIFLEXの実験システムに適用する飛行制御系を担当した．設計手法としてMDM/MDP(多数遅れモデル/多数設計点)法を採用し,基準軌道をもとに得られた複数の線型化モデルに対してこれを適用することで，縦及び横/方向の飛行制御則を設計した．設計した制御系の性能評価には6自由度非線型シミュレーションプログラムを用いた．本稿では,これらの飛行制御系とその設計手法について報告する","subitem_description_type":"Abstract"}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"The lifting-body type vehicle is one of the most promising candidates for future reusable launch systems. In JAXA, the LIFLEX(LIfting-body FLight EXperiment) was planned with the main purpose of developing automatic landing technology, which is one of the most important issues in realising lifting-body type reusable launch vehicles.The authors were in charge of the flight control system of the experimental vehicle for LIFLEX. The longitual and lateral control systems were designed by applying the MDM/MDP(Multiple Delay Model/Multiple Design Point) method to linearised systems of the vehicle derived from the nominal reference trajectory. The designed control systems were evaluated using the six degree-of-freedom nonlinear flight simulation program. This paper reports the outline and design procedure of these flight control systems.","subitem_description_type":"Other"}]},"item_3_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_3_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_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0064806000","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: JAXA-RR-10-006","subitem_description_type":"Other"}]},"item_3_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"宇宙航空研究開発機構"}]},"item_3_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"Japan Aerospace Exploration Agency (JAXA)"}]},"item_3_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"1349-1113","subitem_source_identifier_type":"ISSN"}]},"item_3_source_id_24":{"attribute_name":"書誌レコードID","attribute_value_mlt":[{"subitem_source_identifier":"AA1192675X","subitem_source_identifier_type":"NCID"}]},"item_3_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"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研究開発本部"},{"subitem_text_value":"宇宙航空研究開発機構研究開発本部"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Aerospace Research and Development Directorate, Japan Aerospace Exploration Agency (JAXA)"},{"subitem_text_language":"en","subitem_text_value":"Aerospace Research and Development Directorate, Japan Aerospace Exploration Agency (JAXA)"},{"subitem_text_language":"en","subitem_text_value":"Aerospace Research and Development Directorate, Japan Aerospace Exploration Agency (JAXA)"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"濱田, 吉郎"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"牧, 緑"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"二宮, 哲次郎"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Hamada, Yoshiro","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Maki, Midori","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Ninomiya, Tetsujiro","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":"2020-01-15"}],"displaytype":"detail","filename":"64806000.pdf","filesize":[{"value":"2.1 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"64806000.pdf","url":"https://jaxa.repo.nii.ac.jp/record/2065/files/64806000.pdf"},"version_id":"4c0d401f-13f7-423f-b0f9-3a2fdefb9492"}]},"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":"リフティングボディ飛行実験(LIFLEX)誘導制御系: 飛行制御系設計","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"リフティングボディ飛行実験(LIFLEX)誘導制御系: 飛行制御系設計"}]},"item_type_id":"3","owner":"1","path":["114","1893"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"2065","relation_version_is_last":true,"title":["リフティングボディ飛行実験(LIFLEX)誘導制御系: 飛行制御系設計"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T09:29:14.053153+00:00"}