{"created":"2023-06-20T15:10:22.089200+00:00","id":39950,"links":{},"metadata":{"_buckets":{"deposit":"4e0a63ac-9ba8-45f9-bfcd-cf158e1a78d9"},"_deposit":{"created_by":1,"id":"39950","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"39950"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00039950","sets":["1887:1893","1896:1898:1913:1916"]},"author_link":["445719","445718"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Operational simulation of redundant output actuator for multiple hydraulic flight control systems"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1997-05","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"26","bibliographicPageStart":"1","bibliographicVolumeNumber":"711","bibliographic_titles":[{"bibliographic_title":"航空宇宙技術研究所資料"},{"bibliographic_title":"Technical Memorandum of National Aerospace Laboratory","bibliographic_titleLang":"en"}]}]},"item_3_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"航空機の操縦系統の多重化は、その信頼性を向上させるために必要な対策である。ここでは、その多重化のうちで、多系統の出力を1系統に加算出力する方式について取り扱う。この加算出力するアクチュエータが冗長出力型油圧アクチュエータである。このアクチュエータの作動により、多重系出力を1系統出力に変換して、舵面を駆動することになる。一般に、この種のアクチュエータの加算出力部の作動は、複雑なフィードバックループを含むブロック線図の形で与えられるが、本報告では、このようなブロック線図の表し方に代えて、出力軸の捩り振動の問題として定式化する。これにより、設計時において、その作動特性を数値計算によって取得し、さらに高性能な制御系を構成することが容易になる。","subitem_description_type":"Abstract"}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Multiple channels of flight control systems improve reliability. This report shows the analysis of such systems in which outputs are mechanically tied together to a common output axis so that the multiple output should be summed. Though the operation of this actuator has been given in the form of a block diagram so far, mathematical formulas are provided to solve the problem of twisted oscillation of an axis. This method allows the detailed of operational characteristics to be estimated.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0001066000","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 TM-711","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":"0452-2982","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":"AN00314334","subitem_source_identifier_type":"NCID"}]},"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 新型航空機研究グループ"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Advanced Aircraft Research Group"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"小川, 敏雄"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Ogawa, Toshio","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":"naltm0000711.pdf","filesize":[{"value":"1.5 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"naltm0000711.pdf","url":"https://jaxa.repo.nii.ac.jp/record/39950/files/naltm0000711.pdf"},"version_id":"71724ba4-94e7-4a49-a33c-f442bbdd18ee"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"冗長出力型アクチュエータ","subitem_subject_scheme":"Other"},{"subitem_subject":"多重油圧操縦システム","subitem_subject_scheme":"Other"},{"subitem_subject":"3重系油圧操縦システム","subitem_subject_scheme":"Other"},{"subitem_subject":"多重油圧アクチュエータ","subitem_subject_scheme":"Other"},{"subitem_subject":"多重油圧アクチュエータ作動シミュレーション","subitem_subject_scheme":"Other"},{"subitem_subject":"多重制御系","subitem_subject_scheme":"Other"},{"subitem_subject":"舵面駆動部","subitem_subject_scheme":"Other"},{"subitem_subject":"出力軸捩り振動","subitem_subject_scheme":"Other"},{"subitem_subject":"アクチュエータ加算出力","subitem_subject_scheme":"Other"},{"subitem_subject":"モデル追従制御","subitem_subject_scheme":"Other"},{"subitem_subject":"redundant output actuator","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"multiple hydraulic flight control system","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"triple hydraulic flight control system","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"multiple hydraulic actuator","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"multiple hydraulic actuator operational simulation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"multiple control system","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"control surface actuator","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"output axis twisted oscillation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"actuator summing output","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"model follow up control","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":"多重油圧操縦系統における冗長出力型アクチュエータの作動シミュレーション","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"多重油圧操縦系統における冗長出力型アクチュエータの作動シミュレーション"}]},"item_type_id":"3","owner":"1","path":["1893","1916"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"39950","relation_version_is_last":true,"title":["多重油圧操縦系統における冗長出力型アクチュエータの作動シミュレーション"],"weko_creator_id":"1","weko_shared_id":1},"updated":"2023-06-20T19:18:08.364096+00:00"}