{"created":"2023-06-20T15:10:25.437679+00:00","id":40004,"links":{},"metadata":{"_buckets":{"deposit":"5db2a7ee-ec36-4e78-b177-69a106a3e087"},"_deposit":{"created_by":1,"id":"40004","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"40004"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00040004","sets":["1887:1893","1896:1898:1913:1917"]},"author_link":["445956","445957"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Model following control scheme incorporating integral compensator for multiple hydraulic flight control systems"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1997-10","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"16","bibliographicPageStart":"1","bibliographicVolumeNumber":"1336","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":"航空機の操縦系統において、信頼性を向上させるために、多重油圧操縦システムを構成する場合、各系統の出力を同期させることが、円滑な作動のために必要である。しかし、各系統はそれぞれのシステムパラメータの変動や外乱などにより、出力が変動するので、各系統間に出力差が生じやすい。これに対して、積分補償を加えたサーボモデルの動きに、各系統が追従するモデル追従制御を構成すれば、各系統の出力は1つのサーボモデルに近付くことになり、結局その出力差は微小になり、良好な出力特性が得られることが期待される。この報告では、多重油圧操縦システムにおいて、積分補償型モデル追従制御を構成し、これらの出力特性を3重系油圧操縦装置の作動により検証する。","subitem_description_type":"Abstract"}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Mechanical summing of the output of redundant flight control systems into a single axis shows that the output forces do not always act synchronously, because there are the differences of output in respective systems caused by system parameter variations and disturbances. As a result, operation of the systems is never smooth and the servomechanism is subjected to excessive loads. To prevent these problems, a model following control incorporating an integral compensator is applied to the redundant systems. In this control system, steady state errors do not arise if the system parameters vary from their nominal values and constant disturbances. Experimental results were demonstrated by operating three-channel electrohydraulic servosystems.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0001146000","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-1336","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 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":"naltr0001336.pdf","filesize":[{"value":"812.0 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"naltr0001336.pdf","url":"https://jaxa.repo.nii.ac.jp/record/40004/files/naltr0001336.pdf"},"version_id":"132adf92-a264-4452-b257-4e0acd469437"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"多重油圧制御システム","subitem_subject_scheme":"Other"},{"subitem_subject":"油圧操縦系統","subitem_subject_scheme":"Other"},{"subitem_subject":"冗長システム","subitem_subject_scheme":"Other"},{"subitem_subject":"モデル追従制御","subitem_subject_scheme":"Other"},{"subitem_subject":"積分補償器","subitem_subject_scheme":"Other"},{"subitem_subject":"最適サーボシステム","subitem_subject_scheme":"Other"},{"subitem_subject":"サーボ弁","subitem_subject_scheme":"Other"},{"subitem_subject":"舵面アクチュエータ","subitem_subject_scheme":"Other"},{"subitem_subject":"システムパラメータ","subitem_subject_scheme":"Other"},{"subitem_subject":"油圧シリンダ","subitem_subject_scheme":"Other"},{"subitem_subject":"数式モデル","subitem_subject_scheme":"Other"},{"subitem_subject":"状態方程式","subitem_subject_scheme":"Other"},{"subitem_subject":"過渡応答","subitem_subject_scheme":"Other"},{"subitem_subject":"最適サーボシステム","subitem_subject_scheme":"Other"},{"subitem_subject":"multiple hydraulic control system","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"hydraulic flight control system","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"redundant system","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"model following control","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"integral compensator","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"optimal servosystem","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"servo valve","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"control surface actuator","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"system parameter","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"oil hydraulic cylinder","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"mathematical model","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"state equation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"transient response","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"optimal servosystem","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":"多重油圧操縦系統の積分補償型モデル追従制御","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"多重油圧操縦系統の積分補償型モデル追従制御"}]},"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":"40004","relation_version_is_last":true,"title":["多重油圧操縦系統の積分補償型モデル追従制御"],"weko_creator_id":"1","weko_shared_id":1},"updated":"2023-06-20T19:17:25.148307+00:00"}