{"created":"2023-06-20T15:02:18.450474+00:00","id":31400,"links":{},"metadata":{"_buckets":{"deposit":"f6ab3e15-28c8-4a3c-9a8d-471349be7d32"},"_deposit":{"created_by":1,"id":"31400","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"31400"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00031400","sets":["1887:1890","1896:1898:1899:1903"]},"author_link":["404197"],"item_9_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1988-10","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"15","bibliographicPageStart":"1","bibliographicVolumeNumber":"634","bibliographic_titles":[{},{"bibliographic_title":"The Institute of Space and Astronautical Science report","bibliographic_titleLang":"en"}]}]},"item_9_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Flight Safety System requires high reliability on its operation because of the crucial duties, duties to decide to destruct a flying vehicle or not, etc. in a state of emergency. A new Flight Safety System which is totally independent from our old one, that depends on radar information, is based upon the principle of inertial navigation in calculating a real time trajectory and impact points on earth by online PCM-Telemetry data. We have applied this back up system for practical missions such as Halley mission and Ginga mission, and have had successful results. An efficient, redundant system was born only by connecting ordinary personal computer to the line, for rapid calculation can be expected in constructing transfer matrix in single pole representation of attitude.","subitem_description_type":"Other"}]},"item_9_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: SA0035081000","subitem_description_type":"Other"}]},"item_9_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"宇宙科学研究所"}]},"item_9_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"Institute of Space and Astronautical Science"}]},"item_9_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"0285-6808","subitem_source_identifier_type":"ISSN"}]},"item_9_source_id_24":{"attribute_name":"書誌レコードID","attribute_value_mlt":[{"subitem_source_identifier":"AA10632072","subitem_source_identifier_type":"NCID"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"TSUKAMOTO, Shigeki","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":"2020-01-23"}],"displaytype":"detail","filename":"SA0035081.pdf","filesize":[{"value":"813.2 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"SA0035081.pdf","url":"https://jaxa.repo.nii.ac.jp/record/31400/files/SA0035081.pdf"},"version_id":"49ec8521-50e5-421a-94b9-7be516f21ee4"}]},"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":"departmental bulletin paper","resourceuri":"http://purl.org/coar/resource_type/c_6501"}]},"item_title":"Development of a New, Redundant Flight Safety System Using Inertial Sensors","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"Development of a New, Redundant Flight Safety System Using Inertial Sensors","subitem_title_language":"en"}]},"item_type_id":"9","owner":"1","path":["1890","1903"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"31400","relation_version_is_last":true,"title":["Development of a New, Redundant Flight Safety System Using Inertial Sensors"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T01:00:52.281417+00:00"}