{"created":"2023-06-20T15:17:15.067207+00:00","id":47398,"links":{},"metadata":{"_buckets":{"deposit":"944a7fd4-c3de-4084-809c-0ed00f27dac8"},"_deposit":{"created_by":1,"id":"47398","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"47398"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00047398","sets":["1398:1408:2123","1887:1893","9:10:2065:2120"]},"author_link":["532828","532827","532824","532829","532830","532825","532826","532823"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"The development of an attitude control system for a balloon experiment"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2021-02-26","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"67","bibliographicPageStart":"57","bibliographicVolumeNumber":"JAXA-RR-20-009","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":"望遠鏡を搭載しておこなう気球実験のための姿勢制御システムの開発をおこなった。このシステムは、電波望遠鏡を用いて成層圏にてvery-long-baseline interferometry (VLBI) 観測をおこなう「気球VLBI」ミッションのために開発された。他の経緯台式の望遠鏡ミッションにも使用することができると考えられる。方位角制御は、ピボットとリアクションホイールの組み合わせで実現する。仰角制御には、振り子運動の影響を軽減させるNASA のWASP のコンセプトを実験的に取り入れている。2017年、放球待機中の気球VLBI ゴンドラを大樹宇宙実験場 (Taiki Aerospace. Research Field: TARF) の組立室にてクレーン懸架し、制御実験をおこなった。その結果、方位角・仰角それぞれの１σ安定度は0.015 deg、0.016 degであった。振り子運動環境下においても、振り子運動の振幅にほとんど依存せず、仰角安定度は0.02 degに収まった。","subitem_description_type":"Abstract"}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"An attitude control system for a balloon experiment using a telescope has been developed. This system was developed for the balloon-borne very-long-baseline interferometry (VLBI) experiment, and can be used for other balloon-borne missions of the altazimuth system. The azimuth control is achieved by using a pivot and a reaction wheel. For the elevation control, we experimentally adopt the Wallops Arc Second Pointer (WASP) concept, in which the effect of pendulum motion is reduced by placing a telescope on a shaft rotating at a constant speed. We carried out hanging tests at the assembly room in the Taiki Aerospace Research Field (TARF) on 2017. The azimuth and elevation residuals were stabilized to 0.015 deg and 0.016 deg (1σ), respectively. Under the pendulum condition, the elevation stability was within 0.02 deg, which was nearly independent on the amplitude of pendulum vibration.","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: AA2030024004","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-20-009","subitem_description_type":"Other"}]},"item_3_identifier_registration":{"attribute_name":"ID登録","attribute_value_mlt":[{"subitem_identifier_reg_text":"10.20637/00047385","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_22":{"attribute_name":"ISSNONLINE","attribute_value_mlt":[{"subitem_source_identifier":"2433-2216","subitem_source_identifier_type":"ISSN"}]},"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宇宙科学研究所(JAXA)(ISAS)"},{"subitem_text_value":"国立天文台(NAOJ)"},{"subitem_text_value":"国立天文台(NAOJ)"},{"subitem_text_value":"宇宙航空研究開発機構宇宙科学研究所(JAXA)(ISAS)"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS)"},{"subitem_text_language":"en","subitem_text_value":"National Astronomical Observatory of Japan (NAOJ)"},{"subitem_text_language":"en","subitem_text_value":"National Astronomical Observatory of Japan (NAOJ)"},{"subitem_text_language":"en","subitem_text_value":"Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS)"}]},"item_3_version_type_30":{"attribute_name":"著者版フラグ","attribute_value_mlt":[{"subitem_version_resource":"http://purl.org/coar/version/c_970fb48d4fbd8a85","subitem_version_type":"VoR"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"土居, 明広"}],"nameIdentifiers":[{"nameIdentifier":"532823","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"河野, 裕介"}],"nameIdentifiers":[{"nameIdentifier":"532824","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"山下, 一芳"}],"nameIdentifiers":[{"nameIdentifier":"532825","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"佐藤, 泰貴"}],"nameIdentifiers":[{"nameIdentifier":"532826","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"DOI, Akihiro","creatorNameLang":"en"}],"nameIdentifiers":[{"nameIdentifier":"532827","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"KONO, Yusuke","creatorNameLang":"en"}],"nameIdentifiers":[{"nameIdentifier":"532828","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"YAMASHITA, Kazuyoshi","creatorNameLang":"en"}],"nameIdentifiers":[{"nameIdentifier":"532829","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"SATO, Yasutaka","creatorNameLang":"en"}],"nameIdentifiers":[{"nameIdentifier":"532830","nameIdentifierScheme":"WEKO"}]}]},"item_files":{"attribute_name":"ファイル情報","attribute_type":"file","attribute_value_mlt":[{"accessrole":"open_date","date":[{"dateType":"Available","dateValue":"2021-02-26"}],"displaytype":"detail","filename":"AA2030024004.pdf","filesize":[{"value":"4.7 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"AA2030024004.pdf","url":"https://jaxa.repo.nii.ac.jp/record/47398/files/AA2030024004.pdf"},"version_id":"8c1f6e3b-af9b-4b9f-a008-fd71faca2f84"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"balloon","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"attitude control","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"pointing system","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"stratosphere","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"telescope","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"antenna","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":"気球実験のための姿勢制御システムの開発","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"気球実験のための姿勢制御システムの開発"}]},"item_type_id":"3","owner":"1","path":["1893","2120","2123"],"pubdate":{"attribute_name":"公開日","attribute_value":"2021-02-26"},"publish_date":"2021-02-26","publish_status":"0","recid":"47398","relation_version_is_last":true,"title":["気球実験のための姿勢制御システムの開発"],"weko_creator_id":"1","weko_shared_id":1},"updated":"2023-06-20T19:39:33.424923+00:00"}