{"created":"2023-06-20T14:35:36.046492+00:00","id":1845,"links":{},"metadata":{"_buckets":{"deposit":"69c776dc-36f6-42f0-8f4e-86d1e340386f"},"_deposit":{"created_by":1,"id":"1845","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"1845"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00001845","sets":["1398:1408:1411","1887:1893","9:10:39:46"]},"author_link":["476339","476340","476343","476341","476338","476342"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Development and evaluation flight test results of a controlled-descent type payload system optimized for the recovery from a very small balloon"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2017-03-14","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"100","bibliographicPageStart":"81","bibliographicVolumeNumber":"JAXA-RR-16-008","bibliographic_titles":[{"bibliographic_title":"宇宙航空研究開発機構研究開発報告: 大気球研究報告"},{"bibliographic_title":"JAXA Research and Development Report","bibliographic_titleLang":"en"}]}]},"item_3_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"従来型パラシュートを用いて回収を行う超小型気球回収システムの問題点解決のため、滑空可能なパラフォイルを用い制御降下式ペイロードによる回収システムを設計し、近い将来の実飛行運用を目指した搭載システムの基礎開発を行った。実際の小型気球からの放球・制御着陸運用を模擬して高所作業車からの6回の投下実験を行い、旋回制御能力を評価し短期間の滑空比を測定した。一連の評価試験によって、構築ペイロードモデルに一定の設計妥当性が認められ、約5秒間の短期間平均の滑空比として3以上の実験値を計測した。","subitem_description_type":"Abstract"}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"In order to solve some difficulties on the balloon recovery system with a conventional parachute, a recovery system with a parafoil for the controlled-descent was designed and basic on-board system was developed for the real flight operation in near future. Simulating flights from small balloons, six flight tests from an aerial vehicle were carried out to evaluate its capability of the trajectory control and to measure its short term gliding ratio. Through the series of the tests, the system was validated and the averaged short term gliding ratio for about 5 s was measured to be larger than 3.","subitem_description_type":"Other"}]},"item_3_description_18":{"attribute_name":"内容記述","attribute_value_mlt":[{"subitem_description":"形態: カラー図版あり","subitem_description_type":"Other"}]},"item_3_description_19":{"attribute_name":"内容記述（英）","attribute_value_mlt":[{"subitem_description":"Physical characteristics: Original contains color illustrations","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA1630045005","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-16-008","subitem_description_type":"Other"}]},"item_3_identifier_registration":{"attribute_name":"ID登録","attribute_value_mlt":[{"subitem_identifier_reg_text":"10.20637/JAXA-RR-16-008/0005","subitem_identifier_reg_type":"JaLC"}]},"item_3_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"宇宙航空研究開発機構(JAXA)"}]},"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":"高知工科大学"},{"subitem_text_value":"高知工科大学"},{"subitem_text_value":"高知工科大学"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Kochi University of Technology"},{"subitem_text_language":"en","subitem_text_value":"Kochi University of Technology"},{"subitem_text_language":"en","subitem_text_value":"Kochi University of Technology"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"平塚, 丘将"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"河野, 紘基"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"山本, 真行"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Hiratsuka, Takamasa","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kono, Hiroki","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Yamamoto, Masayuki","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":"2020-01-31"}],"displaytype":"detail","filename":"AA1630045005.pdf","filesize":[{"value":"17.5 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"AA1630045005.pdf","url":"https://jaxa.repo.nii.ac.jp/record/1845/files/AA1630045005.pdf"},"version_id":"cab9edd6-53e3-4896-8149-4a3800ba9ee5"}]},"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":"超小型気球の回収に最適化された制御降下式ペイロードシステムの開発と飛行試験結果の評価","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"超小型気球の回収に最適化された制御降下式ペイロードシステムの開発と飛行試験結果の評価"}]},"item_type_id":"3","owner":"1","path":["46","1411","1893"],"pubdate":{"attribute_name":"公開日","attribute_value":"2017-03-23"},"publish_date":"2017-03-23","publish_status":"0","recid":"1845","relation_version_is_last":true,"title":["超小型気球の回収に最適化された制御降下式ペイロードシステムの開発と飛行試験結果の評価"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T21:38:10.826538+00:00"}