{"created":"2023-06-20T15:10:02.446324+00:00","id":39638,"links":{},"metadata":{"_buckets":{"deposit":"117bb4de-93d1-4ac2-b37e-be01f5985b56"},"_deposit":{"created_by":1,"id":"39638","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"39638"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00039638","sets":["1887:1893","1896:1898:1913:1917"]},"author_link":["443706","443701","443705","443702","443703","443707","443699","443700","443704","443708"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Effects of visibility on helicopter pilot performance, part 2"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1995-06","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"10","bibliographicPageStart":"1","bibliographicVolumeNumber":"1272","bibliographic_titles":[{"bibliographic_title":"航空宇宙技術研究所報告"},{"bibliographic_title":"Technical Report of National Aerospace Laboratory","bibliographic_titleLang":"en"}]}]},"item_3_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"1992年11月に実施した第1次実験に引き続き、視程がヘリコプターパイロット系の安定性に及ぼす影響を調べることを目的としてシミュレータ実験を行った。1000時間から3000時間の飛行経験を持つパイロット10名が参加した。実験ではシミュレータの模擬視界の視程を変化させ、各視程で操縦安定限界となる縦揺れおよび横揺れの線形微係数の値を求めた。また、原型の数学モデルの下で、視程を変化させ操縦時のパイロットの視点移動を記録した。実験結果から、視程の変化の操縦安定性への影響をヘリコプタの安定性によって定量的に評価することができた。これらの結果より、視程不良時の有視界飛行において運航効率および運航安全性を向上させるための安定性増大装置や情報提示方式についての技術資料を得た。","subitem_description_type":"Abstract"}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"A piloted flight simulation aiming at quantifying visibility effect on helicopter piloting was carried out. The flight simulation was conducted in the way of varying the visibility of the visual scene and the stability of the aircraft, respectively, so as to determine a critical value of the stability with which the pilot can barely control the aircraft. Eye fixation points data of the pilots were obtained in each visibility condition. The flight simulation results enabled direct evaluation of visibility effects upon pilot control performance in terms of helicopter stability. Some considerations of effectiveness of stability augmentation systems and display systems in low visibility condition are also described in this paper.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0000009000","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-1272","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 制御部"},{"subitem_text_value":"航空宇宙技術研究所 制御部"},{"subitem_text_value":"航空宇宙技術研究所 制御部"},{"subitem_text_value":"航空宇宙技術研究所 制御部"},{"subitem_text_value":"航空宇宙技術研究所 制御部"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Control Systems Division"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Control Systems Division"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Control Systems Division"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Control Systems Division"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Control Systems Division"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"舩引, 浩平"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"田中, 啓司"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"川原, 弘靖"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"若色, 薫"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"渡辺, 顯"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Funabiki, Kohei","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Tanaka, Keiji","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kawahara, Hiroyasu","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Wakairo, Kaoru","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Watanabe, Akira","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":"2020-01-27"}],"displaytype":"detail","filename":"naltr01272.pdf","filesize":[{"value":"941.9 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"naltr01272.pdf","url":"https://jaxa.repo.nii.ac.jp/record/39638/files/naltr01272.pdf"},"version_id":"0c34c532-424f-4f0a-97b0-4ae6a47ac800"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"ヘリコプタ操縦","subitem_subject_scheme":"Other"},{"subitem_subject":"視覚情報","subitem_subject_scheme":"Other"},{"subitem_subject":"取得方式","subitem_subject_scheme":"Other"},{"subitem_subject":"飛行シミュレーション実験","subitem_subject_scheme":"Other"},{"subitem_subject":"パイロット行為","subitem_subject_scheme":"Other"},{"subitem_subject":"視程","subitem_subject_scheme":"Other"},{"subitem_subject":"人間機械系","subitem_subject_scheme":"Other"},{"subitem_subject":"操縦安定限界","subitem_subject_scheme":"Other"},{"subitem_subject":"縦揺れ減衰","subitem_subject_scheme":"Other"},{"subitem_subject":"横揺れ減衰","subitem_subject_scheme":"Other"},{"subitem_subject":"視点移動","subitem_subject_scheme":"Other"},{"subitem_subject":"飛行安全","subitem_subject_scheme":"Other"},{"subitem_subject":"有視界飛行","subitem_subject_scheme":"Other"},{"subitem_subject":"運行効率","subitem_subject_scheme":"Other"},{"subitem_subject":"視程影響モデル","subitem_subject_scheme":"Other"},{"subitem_subject":"helicopter piloting","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"visual information","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"flight simulation experiment","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"acquisition system","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"pilot performance","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"visual range","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"man machine system","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"critical value of piloting stability","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"pitching damping","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"rolling damping","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"eye fixation point displacement","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"flight safety","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"visual flight","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"operation efficiency","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"visual range effect model","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":"ヘリコプタ操縦時の視覚情報取得方式に関する飛行シミュレーション実験　第2報","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"ヘリコプタ操縦時の視覚情報取得方式に関する飛行シミュレーション実験　第2報"}]},"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":"39638","relation_version_is_last":true,"title":["ヘリコプタ操縦時の視覚情報取得方式に関する飛行シミュレーション実験　第2報"],"weko_creator_id":"1","weko_shared_id":1},"updated":"2023-06-20T19:20:05.799363+00:00"}