{"created":"2023-06-20T15:11:38.075345+00:00","id":41322,"links":{},"metadata":{"_buckets":{"deposit":"cfefd7e2-b5a4-4bea-9662-41c91f04e967"},"_deposit":{"created_by":1,"id":"41322","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"41322"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00041322","sets":["1887:1893","1896:1898:1913:1915"]},"author_link":["489469","489468"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Stochastic approach for flight control system synthesis and analysis with Monte Carlo simulation"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2000-12","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"116","bibliographicPageStart":"115","bibliographicVolumeNumber":"46","bibliographic_titles":[{"bibliographic_title":"航空宇宙技術研究所特別資料"},{"bibliographic_title":"Special Publication of National Aerospace Laboratory","bibliographic_titleLang":"en"}]}]},"item_3_description_14":{"attribute_name":"会議概要（会議名, 開催地, 会期, 主催者等）","attribute_value_mlt":[{"subitem_description":"航空宇宙技術研究所 7-9 Jun. 2000 東京 日本","subitem_description_type":"Other"}]},"item_3_description_15":{"attribute_name":"会議概要（会議名, 開催地, 会期, 主催者等）（英）","attribute_value_mlt":[{"subitem_description":"National Aerospace Laboratory 7-9 Jun. 2000 Tokyo Japan","subitem_description_type":"Other"}]},"item_3_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"この論文では、飛行制御システムの設計および評価に関する統計的な方法について議論した。飛行シミュレーションモデルにはさまざまな不確定性を持ったパラメータが含まれており、開発段階における飛行制御システムの性能が不確かなものになっている。この方法では、パラメータの統計的性質を仮定し、性能の確率やミッション成功の確率について、モンテカルロ・シミュレーションを用いて評価した。飛行制御における調節可能な増大は、ミッション成功の確率を最大にすることによって調整した。","subitem_description_type":"Abstract"}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"This paper discusses a stochastic approach for flight control system synthesis and analysis. A flight simulation model contains various kinds of uncertainty parameters, which make the flight control system's performance uncertain in the development. In the approach, stochastic properties of the parameters are assumed, and then probability of the performance, or probability of mission achievement, is evaluated by using Monte Carlo simulation. Adjustable gains in the flight control law are tuned by maximizing the probability of mission achievement.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0028635021","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 SP-46","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":"0289-260X","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":"AN10097345","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 飛行研究部"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Flight Division"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"宮沢, 与和"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Miyazawa, Yoshikazu","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":"2020-02-10"}],"displaytype":"detail","filename":"nalsp0046021.pdf","filesize":[{"value":"173.7 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"nalsp0046021.pdf","url":"https://jaxa.repo.nii.ac.jp/record/41322/files/nalsp0046021.pdf"},"version_id":"987b2437-bdbd-41ca-a9e9-5eac63aa70df"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"飛行制御システム","subitem_subject_scheme":"Other"},{"subitem_subject":"統計的方法","subitem_subject_scheme":"Other"},{"subitem_subject":"モンテカルロ法","subitem_subject_scheme":"Other"},{"subitem_subject":"飛行力学","subitem_subject_scheme":"Other"},{"subitem_subject":"小型自動着陸","subitem_subject_scheme":"Other"},{"subitem_subject":"着陸性能","subitem_subject_scheme":"Other"},{"subitem_subject":"飛行制御ゲイン","subitem_subject_scheme":"Other"},{"subitem_subject":"分散処理システム","subitem_subject_scheme":"Other"},{"subitem_subject":"飛行シミュレーションモデル","subitem_subject_scheme":"Other"},{"subitem_subject":"不確定パラメータ","subitem_subject_scheme":"Other"},{"subitem_subject":"ミッション成功","subitem_subject_scheme":"Other"},{"subitem_subject":"flight control system","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"stochastic approach","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Monte Carlo simulation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"aerodynamics","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"automatic landing flight","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"landing performance","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"flight control gain","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"distributed processing","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"flight simulation model","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"uncertainty parameter","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"mission achievement","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":"モンテカルロ・シミュレーションによる飛行制御系の統計的な評価と設計","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"モンテカルロ・シミュレーションによる飛行制御系の統計的な評価と設計"}]},"item_type_id":"3","owner":"1","path":["1893","1915"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"41322","relation_version_is_last":true,"title":["モンテカルロ・シミュレーションによる飛行制御系の統計的な評価と設計"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T21:03:15.566089+00:00"}