{"created":"2023-06-20T14:36:10.083503+00:00","id":2479,"links":{},"metadata":{"_buckets":{"deposit":"4f826b0a-9bcc-4740-a65a-262be21bff9b"},"_deposit":{"created_by":1,"id":"2479","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"2479"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00002479","sets":["1887:1893","9:1090:1137:1142"]},"author_link":["6698","6700","6696","6701","6697","6699"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Pilot Workload Analysis for Electric Propulsion System Failure of Motor Glider"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2015-03-23","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"21","bibliographicPageStart":"1","bibliographicVolumeNumber":"JAXA-RM-14-008","bibliographic_titles":[{"bibliographic_title":"宇宙航空研究開発機構研究開発資料"},{"bibliographic_title":"JAXA Research and Development Memorandum","bibliographic_titleLang":"en"}]}]},"item_3_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"宇宙航空研究開発機構（JAXA）航空本部は、航空機用電動推進システムを独自に開発し、既存のモータグライダーのレシプロエンジンを電動推進システムに換装して2014 年度に飛行実証する計画である。飛行試験における安全性を確保するために、電動推進システムが故障した場合にいつでも滑空して帰還することを基本方針の一つとしている。本稿では電動化した後のモータグライダーが、滑空して帰還するために必要な滑走路長を決定するため、電動推進システムが飛行中に故障したことを模擬する飛行試験を実施した。本飛行試験では離陸・上昇中に電動推進システムが故障したことを想定し、その時点における高度をパラメータとして、特にジャンプ飛行で到達可能な最高高度と、上昇中に反転した後、滑空帰還可能な最低高度をパイロットワークロードの解析等から明らかにした。試験の結果、反転可能な最低高度等が判明し安全に滑空帰還するために必要となる最低滑走路長を推定することができた。","subitem_description_type":"Abstract"}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"The Japan Aerospace Exploration Agency (JAXA) has a plan of flight test evaluation for motor glider which is equipped with a new original electric propulsion system proposed by JAXA on 2014. The new electric propulsion system will be converted form the existing reciprocating engine of motor glider and be installed with motor glider. One of basic safety policy for the flight test evaluation is that the motor glider should fly within area where motor glider always is able to return runway safely when the electric propulsion system trouble such as electric motor or battery pack failure happens. In order to determine a runway length for the flight test evaluation of motor glider equipped with the electric propulsion system on 2014, a series of flight experiment of simulated electric propulsion system failure was carried out. We clarified an altitude which satisfied with both feasibility of “jump flight (takeoff/climb, power idle, straight forward landing)” and of “180 turn flight (takeoff/climb, power idle, 180 turn and landing)” from a pilot workload analysis by the flight experiment results. The altitude of the simulated electric propulsion system failure during takeoff and climb was parametrically varied in the flight experiment. The results of the experiment showed that the altitude which satisfied with both feasibility of “jump flight” and of “180 turn flight” was about 400ft from above ground level. Additionally, the results indicated that the flight test evaluation after conversion from the motor glider’s original reciprocating engine to the new electric propulsion system should be conducted by using runway area which is able to be both “jump flight” and “180 turn” with about 400ft.","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: AA1530020000","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-RM-14-008","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(JAXA)"}]},"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":"1349-1121","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":"AA11983593","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航空本部航空技術実証研究開発室(JAXA)"},{"subitem_text_value":"宇宙航空研究開発機構航空本部航空技術実証研究開発室(JAXA)"},{"subitem_text_value":"宇宙航空研究開発機構航空本部航空技術実証研究開発室(JAXA)"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Technology Demonstration Research Office, Institute of Aeronautical Technology, Japan Aerospace Exploration Agency (JAXA)"},{"subitem_text_language":"en","subitem_text_value":"Technology Demonstration Research Office, Institute of Aeronautical Technology, Japan Aerospace Exploration Agency (JAXA)"},{"subitem_text_language":"en","subitem_text_value":"Technology Demonstration Research Office, Institute of Aeronautical Technology, Japan Aerospace Exploration Agency (JAXA)"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"飯島, 朋子"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"小林, 宙"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"西沢, 啓"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Iijima, Tomoko","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kobayashi, Hiroshi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Nishizawa, 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":"2020-01-15"}],"displaytype":"detail","filename":"AA1530020000.pdf","filesize":[{"value":"4.3 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"AA1530020000.pdf","url":"https://jaxa.repo.nii.ac.jp/record/2479/files/AA1530020000.pdf"},"version_id":"6ea0db71-5f65-4207-9ebe-01fc1ed64026"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"Electric Propulsion System","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Electric Motor","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Electric Engine","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Motor Glider","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Pilot Workload","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Workload Rating","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Flight Test","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":"電動推進システム故障時のパイロットワークロード解析","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"電動推進システム故障時のパイロットワークロード解析"}]},"item_type_id":"3","owner":"1","path":["1142","1893"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-04-10"},"publish_date":"2015-04-10","publish_status":"0","recid":"2479","relation_version_is_last":true,"title":["電動推進システム故障時のパイロットワークロード解析"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T09:21:53.446670+00:00"}