{"created":"2023-06-20T14:36:19.086349+00:00","id":2634,"links":{},"metadata":{"_buckets":{"deposit":"80bcc348-be3e-45cf-ab98-881a67358c98"},"_deposit":{"created_by":1,"id":"2634","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"2634"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00002634","sets":["1887:1893","9:1090:1280:1290"]},"author_link":["7958","7966","7967","7968","7974","7963","7959","7969","7970","7962","7965","7972","7957","7964","7971","7973","7961","7960"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Design and ground testing of the guidance and control system for a scaled-non-powered supersonic experimental airplane using to 1st flight trial"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2007-03-30","bibliographicIssueDateType":"Issued"},"bibliographicVolumeNumber":"JAXA-RM-06-007","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":"次世代超音速機に用いるための計算空気力学による革新的空力設計技術を開発するために、無推力小型超音速実験機の研究開発が1997年9月以来、宇宙航空研究開発機構(JAXA)において行われてきた。本実験機は固体ロケットブースターにより打上げられる。本報告では、第1回飛行実験に使用された、実験機を打上げるための固体ロケットブースターの誘導制御系設計と地上試験が記述される。ロケット誘導制御系はオートパイロット計算機と慣性航法センサから構成される。そして本誘導制御系の構成機器の特徴や性能、システム解析結果および機能・性能を検証するための地上試験結果が明らかにされる。また第1回飛行実験に使用された小型超音速実験機の誘導制御系設計と地上試験が記述される。実験機誘導制御系は全電気系FBW(Fly-By-Wire)概念に基づいて、FCC(Flight Control Computer:飛行制御計算機)、IMU(Inertial Measurement Unit:慣性航法装置)、ADS(Air Data System:エアーデータシステム)および垂直加速度センサー(Nzセンサー)から構成される。そして実験機誘導制御系構成機器の特徴や性能、システム解析結果および機能・性能を検証するための地上試験結果が明らかにされる。","subitem_description_type":"Abstract"}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"A research and development project will be carried out using Computational Fluid Dynamics (CFD) to develop advanced aerodynamic design technologies for the next generation supersonic transports. A supersonic flight experiment has been underway at JAXA (Japan Aerospace Exploration Agency) since September 1997 using a scaled non-powered supersonic experimental airplane launched by a solid rocket booster. This report describes the design and ground testing of the guidance and control system for a solid rocket booster using to launch the experimental airplane. The guidance and control system consists of an Autopilot Computer (AP) and Inertial Navigation Equipment (INE). Features and performance of the system components, results of system analysis and ground testing to approve the functionality and overall performance of the rocket booster's guidance and control system are presented. Similarly this report describes the design and ground testing of the guidance and control system for the experimental airplane using to first flight trial. The guidance and control system consists of a Flight Control Computer (FCC), Inertial Measurement Unit (IMU), Air Data System (ADS) and G sensor (Accelerometer) based on an all-electric fly-by-wire concept. Features and performance of the system components, results of system analysis and ground testing to approve the functionality and overall performance of the guidance and control system for the experimental airplane are presented.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0063319000","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-06-007","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":"1349-1121","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 航空プログラムグループ"},{"subitem_text_value":"宇宙航空研究開発機構 航空プログラムグループ"},{"subitem_text_value":"航空宇宙技術研究所"},{"subitem_text_value":"宇宙航空研究開発機構 航空プログラムグループ"},{"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 航空プログラムグループ"},{"subitem_text_value":"宇宙航空研究開発機構 航空プログラムグループ"},{"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"}]},"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 Aviation Program Group"},{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency Aviation Program Group"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory"},{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency Aviation Program Group"},{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency Institute of Aerospace Technology"},{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency Aviation Program Group"},{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency Aviation Program Group"},{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency Institute of Aerospace Technology"},{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"滝沢, 実"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"村上, 義隆"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"内田, 忠夫"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"石塚, 只夫"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"柳, 良二"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"大貫, 武"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"堀之内, 茂"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"平子, 敬一"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"坂田, 公夫"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Takizawa, Minoru","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Murakami, Yoshitaka","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Uchida, Tadao","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Ishizuka, Tadao","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Yanagi, Ryoji","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Onuki, Takeshi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Horinouchi, Shigeru","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Hirako, Keiichi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Sakata, Kimio","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":"63319000.pdf","filesize":[{"value":"60.6 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"63319000.pdf","url":"https://jaxa.repo.nii.ac.jp/record/2634/files/63319000.pdf"},"version_id":"ec018dfa-ccd9-4f88-b103-a230dd38c83a"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"超音速輸送機","subitem_subject_scheme":"Other"},{"subitem_subject":"計算流体力学","subitem_subject_scheme":"Other"},{"subitem_subject":"航空機設計","subitem_subject_scheme":"Other"},{"subitem_subject":"超音速飛行","subitem_subject_scheme":"Other"},{"subitem_subject":"誘導制御システム","subitem_subject_scheme":"Other"},{"subitem_subject":"固体ロケットブースター","subitem_subject_scheme":"Other"},{"subitem_subject":"地上試験","subitem_subject_scheme":"Other"},{"subitem_subject":"慣性航法","subitem_subject_scheme":"Other"},{"subitem_subject":"supersonic transport","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"computational fluid dynamics","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"aircraft design","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"supersonic flight","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"guidance and control system","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"solid rocket booster","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"ground test","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"inertial navigation","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":"小型超音速ロケット実験機の誘導制御系設計と地上試験:第1回飛行実験に向けて","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"小型超音速ロケット実験機の誘導制御系設計と地上試験:第1回飛行実験に向けて"}]},"item_type_id":"3","owner":"1","path":["1290","1893"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"2634","relation_version_is_last":true,"title":["小型超音速ロケット実験機の誘導制御系設計と地上試験:第1回飛行実験に向けて"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T09:18:44.983932+00:00"}