{"created":"2023-06-20T14:35:49.774147+00:00","id":2107,"links":{},"metadata":{"_buckets":{"deposit":"6b2b9d84-74a8-41ed-b6a4-15dc32cb4c06"},"_deposit":{"created_by":1,"id":"2107","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"2107"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00002107","sets":["1887:1893","9:10:132:136"]},"author_link":["3305","3308","3304","3300","3307","3309","3303","3301","3306","3302"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Objective evaluation method for motion cueing fidelity"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2009-03-31","bibliographicIssueDateType":"Issued"},"bibliographicVolumeNumber":"JAXA-RR-08-009","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":"本研究ではPilot-in-the-loopにおける位相余有に着目し，モーション・システムの設定が向上するにつれてパイロットの予測動作が進み位相余有の値が増加することを検証した．これによりモーション・システムが最適となる設定の位相余有と実機の位相余有を比較すれば，シミュレータがどの程度実機に近い操縦性を有しているかを客観的に評価することができる．また，位相余有を測定した各々のモーション・システムの設定での操縦を通して得られたパイロット・コメントと位相余有の増減の傾向を比較して，モーション・システムの設定と操縦性の関係を示すことに位相余有を使う方法の妥当性を検証した．","subitem_description_type":"Abstract"}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"The relationship between the motion fidelity and pilot handling quality was investigated through a series of pilot-in-the-loop simulations. The phase margin of the aircraft-pilot system during a high gain tracking task was measured while varying the gain and filtering parameters of the motion cueing algorithm. As a result, measuring the phase margin the handling quality of the flight simulator can be compared with the actual aircraft. In addition, pilot comment at the same motion system setup as the phase margin measurement was verified with the tendency of the phase margin fluctuation and it supported the adequacy of the method to use the phase margin for evaluating motion cueing fidelity.","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_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0064330000","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-08-009","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飛行技術研究センター飛行シミュレーションセクション"},{"subitem_text_value":"宇宙航空研究開発機構研究開発本部飛行技術研究センター飛行シミュレーションセクション"},{"subitem_text_value":"宇宙航空研究開発機構研究開発本部飛行技術研究センター飛行シミュレーションセクション"},{"subitem_text_value":"宇宙航空研究開発機構研究開発本部飛行技術研究センター飛行性セクション"},{"subitem_text_value":"宇宙航空研究開発機構研究開発本部飛行技術研究センター飛行シミュレーションセクション"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Flight Simulation Section, Flight Research Center, Aerospace Research and Development Directorate, Japan Aerospace Exploration Agency (JAXA)"},{"subitem_text_language":"en","subitem_text_value":"Flight Simulation Section, Flight Research Center, Aerospace Research and Development Directorate, Japan Aerospace Exploration Agency (JAXA)"},{"subitem_text_language":"en","subitem_text_value":"Flight Simulation Section, Flight Research Center, Aerospace Research and Development Directorate, Japan Aerospace Exploration Agency (JAXA)"},{"subitem_text_language":"en","subitem_text_value":"Flight Qualities Section, Flight Research Center, Aerospace Research and Development Directorate, Japan Aerospace Exploration Agency (JAXA)"},{"subitem_text_language":"en","subitem_text_value":"Flight Simulation Section, Flight Research Center, Aerospace Research and Development Directorate, Japan Aerospace Exploration Agency (JAXA)"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"萩原, 敏正"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"舩引, 浩平"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"若色, 薫"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"村岡, 浩治"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"野嶋, 琢也"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Hagiwara, Toshimasa","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Funabiki, Kohei","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Wakairo, Kaoru","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Muraoka, Koji","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Nojima, Takuya","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":"64330000.pdf","filesize":[{"value":"1.7 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"64330000.pdf","url":"https://jaxa.repo.nii.ac.jp/record/2107/files/64330000.pdf"},"version_id":"e63d71d4-2d7a-47b1-b2c8-14f7043d66e1"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"Flight Simulator, Motion System, Setup, Evaluation, Handling Quality, Phase Margin","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":"technical report","resourceuri":"http://purl.org/coar/resource_type/c_18gh"}]},"item_title":"フライト・シミュレータにおけるモーション・キューの客観的評価手法についての研究","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"フライト・シミュレータにおけるモーション・キューの客観的評価手法についての研究"}]},"item_type_id":"3","owner":"1","path":["136","1893"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"2107","relation_version_is_last":true,"title":["フライト・シミュレータにおけるモーション・キューの客観的評価手法についての研究"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T09:28:31.507747+00:00"}