{"created":"2023-06-20T15:14:43.314737+00:00","id":44708,"links":{},"metadata":{"_buckets":{"deposit":"1b7af642-2470-4ae6-aa53-1e19d41cdf1a"},"_deposit":{"created_by":1,"id":"44708","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"44708"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00044708","sets":["1887:1893","1896:1898:1913:1917"]},"author_link":["470833","470834","470835","470836"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Nutation Control of an Asymmetric Spinning Satellite Using an Axial Jet"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1976-05","bibliographicIssueDateType":"Issued"},"bibliographicPageStart":"11","bibliographicVolumeNumber":"457","bibliographic_titles":[{"bibliographic_title":"航空宇宙技術研究所報告"},{"bibliographic_title":"Technical Report of National Aerospace Laboratory TR-457","bibliographic_titleLang":"en"}]}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"This paper describes an active nutation control method for an asymmetric spinning satellite using an axial gas jet and an angular rate sensor. In this method, a constant jet thrust is continuously applied during an entire spin period, thereby preventing the angular momentum of the satellite from changing, while the initial nutation is arbitrarily controlled by selective jet firing timing. The nutational behavior of both stable and unstable asymmetric satellites is analized through transforming the nutational motion into an eccentric anomaly expression.Theoretically, this transformation makes possible elimination of the asymmetry of the satellite and determination of optimum jet firing timing. Finally, hardware simulation results using an air-bearing table were employed to verify the method. A gas rate sensor was utilized as the angular rate sensor in this experiment.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: NALTR0457000","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: NAL TR-457","subitem_description_type":"Other"}]},"item_3_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"航空宇宙技術研究所"}]},"item_3_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"National Aerospace Laboratory(NAL)"}]},"item_3_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"0389-4010","subitem_source_identifier_type":"ISSN"}]},"item_3_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"航空宇宙技術研究所宇宙研究グループ"},{"subitem_text_value":"航空宇宙技術研究所宇宙研究グループ"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Space Technology Research Group, National Aerospace Laboratory(NAL)"},{"subitem_text_language":"en","subitem_text_value":"Space Technology Research Group, National Aerospace Laboratory(NAL)"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"村上, 力"}],"nameIdentifiers":[{"nameIdentifier":"470833","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"中島, 厚"}],"nameIdentifiers":[{"nameIdentifier":"470834","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"MURAKAMI, Chikara","creatorNameLang":"en"}],"nameIdentifiers":[{"nameIdentifier":"470835","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"Atsushi, Nakajima","creatorNameLang":"en"}],"nameIdentifiers":[{"nameIdentifier":"470836","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":"2020-01-29"}],"displaytype":"detail","filename":"naltr00457.pdf","filesize":[{"value":"1.5 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"naltr00457.pdf","url":"https://jaxa.repo.nii.ac.jp/record/44708/files/naltr00457.pdf"},"version_id":"bbf28893-e165-45ba-90e5-963934fe08b6"}]},"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":"非対称スピン衛星のジェットによるニューテーション制御","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"非対称スピン衛星のジェットによるニューテーション制御"}]},"item_type_id":"3","owner":"1","path":["1893","1917"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"44708","relation_version_is_last":true,"title":["非対称スピン衛星のジェットによるニューテーション制御"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T21:52:15.330068+00:00"}