{"created":"2023-06-20T14:36:05.629749+00:00","id":2394,"links":{},"metadata":{"_buckets":{"deposit":"b60052c2-cb8c-477b-97d8-8cb659448b5d"},"_deposit":{"created_by":1,"id":"2394","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"2394"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00002394","sets":["1887:1893","9:10:309:366"]},"author_link":["6019","6020","6021","6018","6016","6017"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Evaluation of guidance and control system of high speed flight demonstrator phase 2"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2004-10-25","bibliographicIssueDateType":"Issued"},"bibliographicVolumeNumber":"JAXA-RR-04-002","bibliographic_titles":[{"bibliographic_title":"宇宙航空研究開発機構研究開発報告"},{"bibliographic_title":"JAXA Research and Development Report","bibliographic_titleLang":"en"}]}]},"item_3_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"本稿では、高速飛行実証機フェーズ2の誘導制御系の飛行前評価を行う。高速飛行実証機は、その打ち上げ方式の特殊性から、所謂ノミナル軌道を持たないため、一般的に用いられるRoot Sum Squareによる評価は適切ではない。そこで本稿では、モンテカルロ・シミュレーション(MC)を中心とした単独誤差解析、感度解析、線形解析から構成される通常評価と、打ち上げ方式の特殊性に配慮した特殊評価により、誘導制御系の評価を総合的に行った。その結果、MCにおいて耐性目標を達成することが出来なかった。ただしその要求逸脱ケースを精査した結果、実飛行上は問題にならないものと判断した。一連の評価解析を通し、誘導制御系の評価手法に対して1つの提案が出来たものと考える。また本評価を通し、実機運用上、重要な基礎データを取得することが出来た。","subitem_description_type":"Abstract"}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"This report describes the results of the preflight evaluation of the guidance and control system of the High Speed Flight Demonstrator Phase 2 (HSFD2). Since the vehicle does not have a nominal trajectory because of its launch method, it is not appropriate to evaluate this system by the root sum square method. The present evaluation followed two approaches, using one standard and one custom designed analysis. The former comprised a Monte-Carlo simulation, single error analysis, sensitivity analysis, and linear analysis. The latter used GPS receiver error, analysis of robustness for individual conditions, and emergency separation. Although in some cases the Monte-Carlo simulation in the standard analysis showed a failure to satisfy mission requirements, detailed analysis indicates that the system would guide the vehicle through a successful flight experiment. This evaluation establishes that the system satisfies all mission requirements. Based on the results of the preflight evaluation, this paper concludes that the guidance and control system of the vehicle was properly designed.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0047678000","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-RR-04-002","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"}]},"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":"1349-1113","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":"AA1192675X","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 総合技術研究本部"},{"subitem_text_value":"宇宙航空研究開発機構 総合技術研究本部"},{"subitem_text_value":"宇宙航空研究開発機構 総合技術研究本部"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency Institute of Space Technology and Aeronautics"},{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency Institute of Space Technology and Aeronautics"},{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency Institute of Space Technology and Aeronautics"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"二宮, 哲次郎"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"鈴木, 広一"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"塚本, 太郎"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Ninomiya, Tetsujiro","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Suzuki, Hirokazu","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Tsukamoto, Taro","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":"47678000.pdf","filesize":[{"value":"5.3 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"47678000.pdf","url":"https://jaxa.repo.nii.ac.jp/record/2394/files/47678000.pdf"},"version_id":"999b4132-4a7b-4a08-a03b-b9d0fd8057b8"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"誘導制御系","subitem_subject_scheme":"Other"},{"subitem_subject":"ノミナル軌道","subitem_subject_scheme":"Other"},{"subitem_subject":"モンテカルロ・シミュレーション","subitem_subject_scheme":"Other"},{"subitem_subject":"感度分析","subitem_subject_scheme":"Other"},{"subitem_subject":"誤差分析","subitem_subject_scheme":"Other"},{"subitem_subject":"飛行前評価","subitem_subject_scheme":"Other"},{"subitem_subject":"HYFLEX","subitem_subject_scheme":"Other"},{"subitem_subject":"ALFLEX","subitem_subject_scheme":"Other"},{"subitem_subject":"guidance and control system","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"nominal trajectory","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Monte Carlo simulation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"sensitivity analysis","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"error analysis","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"preflight evaluation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"HYFLEX","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"ALFLEX","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":"高速飛行実証機フェーズ2の誘導制御系評価","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"高速飛行実証機フェーズ2の誘導制御系評価"}]},"item_type_id":"3","owner":"1","path":["366","1893"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"2394","relation_version_is_last":true,"title":["高速飛行実証機フェーズ2の誘導制御系評価"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T09:23:20.443764+00:00"}