{"created":"2023-06-20T14:40:49.522282+00:00","id":7777,"links":{},"metadata":{"_buckets":{"deposit":"2c7ae5cf-c96f-4f59-8105-e1fb6936a70d"},"_deposit":{"created_by":1,"id":"7777","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"7777"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00007777","sets":["1543:1544:1561","1887:1891"]},"author_link":["41855","41857","41856","41858"],"item_5_alternative_title_1":{"attribute_name":"その他のタイトル","attribute_value_mlt":[{"subitem_alternative_title":"H-2Aロケット航法誘導系の概要と高機能化に関する一考察"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2003-02","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"89","bibliographicPageStart":"85","bibliographic_titles":[{"bibliographic_title":"平成14年度アストロダイナミクスシンポジウム:講演後刷り集"},{"bibliographic_title":"ISAS Proceedings of 12th Workshop on Astrodynamics and Flight Mechanics 2002: A Collection of Technical Papers","bibliographic_titleLang":"en"}]}]},"item_5_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"H-2Aロケットの航法・誘導系について、その概要(構成、H-2からの変更点など)、試験機1号機についてのフライト結果を紹介するとともに、将来的な高機能化(GPSとの複合化)の1案について考察する。","subitem_description_type":"Abstract"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"In this paper, an overview of guidance and navigation system for H-2A launch vehicle is introduced with a focus on the improved aspects from H-2. Also discussed is a study about modified navigation system (added GPS to current H-2A).","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0045497015","subitem_description_type":"Other"}]},"item_5_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"宇宙科学研究所"}]},"item_5_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"The Institute of Space and Astronautical Science (ISAS)"}]},"item_5_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"0918-8053","subitem_source_identifier_type":"ISSN"}]},"item_5_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"宇宙開発事業団"},{"subitem_text_value":"宇宙開発事業団"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"National Space Development Agency of Japan"},{"subitem_text_language":"en","subitem_text_value":"National Space Development Agency of Japan"}]},"item_access_right":{"attribute_name":"アクセス権","attribute_value_mlt":[{"subitem_access_right":"metadata only access","subitem_access_right_uri":"http://purl.org/coar/access_right/c_14cb"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"麦谷, 高志"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"横田, 清美"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Mugitani, Takashi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Yokota, Kiyomi","creatorNameLang":"en"}],"nameIdentifiers":[{}]}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"総覧","subitem_subject_scheme":"Other"},{"subitem_subject":"H-2Aロケット","subitem_subject_scheme":"Other"},{"subitem_subject":"航法誘導系","subitem_subject_scheme":"Other"},{"subitem_subject":"飛行後解析","subitem_subject_scheme":"Other"},{"subitem_subject":"慣性計測装置","subitem_subject_scheme":"Other"},{"subitem_subject":"GPS受信機","subitem_subject_scheme":"Other"},{"subitem_subject":"誘導ロジック","subitem_subject_scheme":"Other"},{"subitem_subject":"軌道投入精度","subitem_subject_scheme":"Other"},{"subitem_subject":"general overview","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"H-2A rocket","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"guidance navigation system","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"postflight analysis","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"inertial measurement unit","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"GPS receiver","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"guidance logic","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"orbit insertion accuracy","subitem_subject_language":"en","subitem_subject_scheme":"Other"}]},"item_language":{"attribute_name":"言語","attribute_value_mlt":[{"subitem_language":"eng"}]},"item_resource_type":{"attribute_name":"資源タイプ","attribute_value_mlt":[{"resourcetype":"conference paper","resourceuri":"http://purl.org/coar/resource_type/c_5794"}]},"item_title":"An overview of H-2A guidance & navigation system and a study on the modification","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"An overview of H-2A guidance & navigation system and a study on the modification","subitem_title_language":"en"}]},"item_type_id":"5","owner":"1","path":["1561","1891"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"7777","relation_version_is_last":true,"title":["An overview of H-2A guidance & navigation system and a study on the modification"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T07:34:13.943515+00:00"}