{"created":"2023-06-20T15:03:58.800394+00:00","id":33179,"links":{},"metadata":{"_buckets":{"deposit":"430429ce-450b-44b8-ab66-3fc36fc7f7a1"},"_deposit":{"created_by":1,"id":"33179","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"33179"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00033179","sets":["1887:1890","1896:1898:1899:1912"]},"author_link":["415106","415116","415111","415112","415113","415119","415107","415118","415120","415121","415115","415105","415109","415104","415117","415110","415108","415114"],"item_9_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Flight Control Experiment of Gliding Parachute using Balloon"}]},"item_9_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1997-03","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"44","bibliographicPageStart":"27","bibliographicVolumeNumber":"34","bibliographic_titles":[{"bibliographic_title":"宇宙科学研究所報告. 特集: 大気球研究報告"}]}]},"item_9_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"グライディング・パラシュートを回収システムに適用することを目指して, 気球を利用しての高度8kmからのグライディング・パラシュートの開傘・飛翔制御試験を1994年6月5日に実施した。レベルフライト高度(34km)からパイロットシュートにより降下させ, 気圧スイッチにより高度約8kmにおいてグライディング・パラシュートを開傘させた。開傘後, GPS受信器および地磁気姿勢センサからのデータに基づくオンボード・コンピュータによる自律飛翔方向制御を試みた。しかし, 開傘直後にパラシュートのコントロール索を制御する機構に一部不具合が生じ, 制御試験については期待されたデータを得ることができなかった。それでも, ほとんど風のなくなった高度3km以下の領域では飛翔軌道は円を描き, 旋回性能に関するデータを得ることができた。また, 本飛翔試験全体を通じて, 自身の水平方向速度を越える強風下でのグライディング・パラシュートの開傘・飛翔の挙動の把握など, 今後のより効率的な回収システム開発のための貴重なデータを得ることができた。","subitem_description_type":"Abstract"}]},"item_9_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"The recovery operation of sounding rocket of ISAS takes much time and cost due to its long down range, amounted to approximately 300km off shore. The recovery system using gliding parachute is expected to be a hopeful candidate because of its maneuverability and high-glide performance. ISAS has been so far developing it through wind tunnel tests with sub-scaled model and drop test from helicopter at low altitude with full-scaled model. In June 1994,the opportunity was took for the autonomous flight test of recovery system with gliding parachute, released from balloon. The gliding parachute deployed at the altitude of about 8km, activated by a baro switch. The autonomous flight control was attempted during descent by the on-boarded computer with GPS data and geomagnetic attitude data. However, post flight analysis showes that the conrol mechnisum malfunctioned at the right moment of the deployment, and that the expected conrol was not carried out at all throughout its flight. In spite of this malfunction, below the altitude of 3km where the wind was weak, the flight tajectory was nearly a circle, and the data such as turning characteristics were obtained. Through this flight test, valuable data were obtained for the further development of recovery system using gliding parachute.","subitem_description_type":"Other"}]},"item_9_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: SA0167083000","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":"0285-9920","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":"AN00354485","subitem_source_identifier_type":"NCID"}]},"item_9_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"宇宙科学研究所"},{"subitem_text_value":"宇宙科学研究所"},{"subitem_text_value":"宇宙科学研究所"},{"subitem_text_value":"宇宙科学研究所"},{"subitem_text_value":"宇宙科学研究所"},{"subitem_text_value":"宇宙科学研究所"},{"subitem_text_value":"宇宙科学研究所"},{"subitem_text_value":"宇宙科学研究所"},{"subitem_text_value":"宇宙科学研究所"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"中島, 俊"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"雛田, 元紀"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"森田, 泰弘"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"平木, 講儒"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"矢島, 信之"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"山上, 隆正"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"太田, 茂雄"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"本田, 秀之"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"気球グループ"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"NAKAJIMA, Takashi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"HINADA, Motoki","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"MORITA, Yasuhiro","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"HIRAKI, Koju","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"YAJIMA, Nobuyuki","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"YAMAGAMI, Takamasa","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"OHTA, Shigeo","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"HONDA, Hideyuki","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Balloon, Group","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":"2020-01-24"}],"displaytype":"detail","filename":"SA0167083.pdf","filesize":[{"value":"2.1 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"SA0167083.pdf","url":"https://jaxa.repo.nii.ac.jp/record/33179/files/SA0167083.pdf"},"version_id":"395ba958-11a9-4a64-995f-384a1c219d04"}]},"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":"departmental bulletin paper","resourceuri":"http://purl.org/coar/resource_type/c_6501"}]},"item_title":"気球によるグライディングパラシュート飛翔制御試験","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"気球によるグライディングパラシュート飛翔制御試験"}]},"item_type_id":"9","owner":"1","path":["1890","1912"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"33179","relation_version_is_last":true,"title":["気球によるグライディングパラシュート飛翔制御試験"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T00:13:35.544322+00:00"}