{"created":"2023-06-20T15:02:35.801011+00:00","id":31689,"links":{},"metadata":{"_buckets":{"deposit":"52e33b6f-7b95-4704-8240-8079f66f767a"},"_deposit":{"created_by":1,"id":"31689","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"31689"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00031689","sets":["1887:1890","1896:1898:1899:1910"]},"author_link":["405744","405747","405749","405745","405746","405748"],"item_9_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Attitude Stabilization System of a Sounding Rocket"}]},"item_9_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1976-12","bibliographicIssueDateType":"Issued"},"bibliographicIssueNumber":"4_B","bibliographicPageEnd":"1014","bibliographicPageStart":"1005","bibliographicVolumeNumber":"12","bibliographic_titles":[{"bibliographic_title":"東京大学宇宙航空研究所報告"}]}]},"item_9_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"K-10-11号機の三軸姿勢制御に使用した姿勢安定制御装置について述べる.本装置は太陽センサデータ処理回路からピッチ,ヨー誤差電圧(2.5V/度)を,また地磁気姿勢計からロール誤差電圧(0.5 V/度)を受けて,内部のレートジャイロ3個の出力と共に;ロケットの三軸姿勢安定と制御を行なう.また出力として,6個のH_2O_2サイドジェットをバーングバング方式でそれぞれ動作させることができる.本装置は種種の姿勢誤差検出回路に対しで,共通にまた手軽に適用できるように設計してある.飛しようの実験結果,本装置の安定度が非常によいことがわかった.","subitem_description_type":"Abstract"}]},"item_9_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"The attitude stabilization system applied to the 3-axis attitude control system of K-10-11 rocket is described. Receiving the pitch and yaw error voltage (2.5 V/degree) from a sun sensor electronics and the roll error voltage (0.5 V/degree) from a geomagnetic aspectmeter, 3-axis rocket attitude stabilization and control is performed by this system that has 3 rate gyros. Also, this has outputs which respectively control 6 H_2O_2 side jets in bang-bang fashion. This system was designed as a commonly used element in a 3-axis attitude control system adapting to various attitude error detection device, with little effort. Viewing from flight test results this system had superior function and stability.","subitem_description_type":"Other"}]},"item_9_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: SA0124694000","subitem_description_type":"Other"}]},"item_9_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"東京大学宇宙航空研究所"}]},"item_9_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"0563-8100","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":"AN00161914","subitem_source_identifier_type":"NCID"}]},"item_9_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"東京大学宇宙航空研究所"},{"subitem_text_value":"三菱プレシジョン株式会社"},{"subitem_text_value":"三菱プレシジョン株式会社"}]},"item_9_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Institute of Space and Aeronautical Science University of Tokyo"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"東口, 実"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"辻本, 博司"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"平岡, 誠"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"HIGASHIGUCHI, Minoru","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"TSUJIMOTO, Hiroshi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"HIRAOKA, Makoto","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":"SA0124694.pdf","filesize":[{"value":"449.5 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"SA0124694.pdf","url":"https://jaxa.repo.nii.ac.jp/record/31689/files/SA0124694.pdf"},"version_id":"e1b4bb3c-b8a3-4ca7-9c0d-f741facb376e"}]},"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":"観測ロケット用姿勢安定制御装置について","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"観測ロケット用姿勢安定制御装置について"}]},"item_type_id":"9","owner":"1","path":["1890","1910"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"31689","relation_version_is_last":true,"title":["観測ロケット用姿勢安定制御装置について"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T00:53:20.511508+00:00"}