{"created":"2023-06-20T15:02:35.867821+00:00","id":31690,"links":{},"metadata":{"_buckets":{"deposit":"472e50cd-d9a4-41ab-846e-c14f8dc4666e"},"_deposit":{"created_by":1,"id":"31690","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"31690"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00031690","sets":["1887:1890","1896:1898:1899:1910"]},"author_link":["405751","405755","405750","405754","405753","405752"],"item_9_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"3-Axis Attitude Control System of a Sounding Rocket (K-10-11)"}]},"item_9_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1976-12","bibliographicIssueDateType":"Issued"},"bibliographicIssueNumber":"4_B","bibliographicPageEnd":"1031","bibliographicPageStart":"1015","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":"観測ロケット(K-10-11号機)に塔載した三軸姿勢制御装置は昭和50年9月24日に飛しょうし,好成績をおさめた.観測目的に応じた姿勢センサを使用して姿勢制御系を構成できるように計画してある.この系は三つの部分からできている.1)姿勢センサ,零位置附近で適当な感度を持ち,±5Vで飽和する特性を持ったピッチ,ヨーおよびロール誤差電圧を出力する.2)姿勢安定エレクトロニクス:3個のレートジャイロとサイドジェット1基ずつをON-OFFする出力を発生する制御電子回路を持ち,バングバング制御方式で機体姿勢を不惑帯内に保持する.3) H_2O_2サイドジェット:機体後端に6基の推力300grのサイドジェットがあり,2基はピッチ制御に,4基はヨー/ロール制御に使用する.中央部にある.推力2.3kgの2基のサイドジェットはロケットの約2 rpsのスピンを止めて三軸姿勢制御を始めるためのデスピントルクを発生させる。本稿には飛しょう実験結果を示してあり,太陽およびX線星観測が満足に行われた.","subitem_description_type":"Abstract"}]},"item_9_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"A 3-axis attitude control system applied to a sounding rocket (K-10-11) achieves its task in the flight experiment of Sept. 24th, 1975. This system can be applied for various attitude control purposes equipped suitable attitude error sensor fitting to the observation. This system can be considered as in three parts. (1) Attitude sensors: providing pitch, yaw and roll attitude error output voltage that has saturation characteristics at 5 volts and appropriate sensitivity about zero error position. (2) Attitude stabilization electronics: including 3 rate gyros and control electronics which gives ON-OFF signal that actuate each one of side jets, and maintaining the vehicle attitude within the dead band in the bang-bang control mode. (3) H_2O_2 side jets: mounting 6 side jets, at the tail of vehicle each having thrust of 300 gr., two of these control pitch motion and four others control yaw/roll motion. Attaching at the middle of the vehicle 2 side jets those have thrust of 2.3 kg each and generate despinning torque before initiating 3-axis attitude control to reduce 2-rps spin of the rocket. In this paper, flight test results are also shown, and these are so satisfactory for sun and X-ray star observation.","subitem_description_type":"Other"}]},"item_9_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: SA0124695000","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":"東京大学宇宙航空研究所"},{"subitem_text_value":"東京大学宇宙航空研究所"}]},"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"},{"subitem_text_language":"en","subitem_text_value":"Institute of Space and Aeronautical Science University of Tokyo"},{"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, 實"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"細川, 繁"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"佐藤, 忠直"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"HIGASHIGUCHI, Minoru","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"HOSOKAWA, Shigeru","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"SATOO, Tadanao","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":"SA0124695.pdf","filesize":[{"value":"942.6 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"SA0124695.pdf","url":"https://jaxa.repo.nii.ac.jp/record/31690/files/SA0124695.pdf"},"version_id":"76980b4a-0006-4660-bdf2-df869246cecb"}]},"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(K-10-11号機)の姿勢制御","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"観測ロケット(K-10-11号機)の姿勢制御"}]},"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":"31690","relation_version_is_last":true,"title":["観測ロケット(K-10-11号機)の姿勢制御"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T00:53:18.504574+00:00"}