{"created":"2023-06-20T15:02:35.935161+00:00","id":31691,"links":{},"metadata":{"_buckets":{"deposit":"86ade6d0-1758-4b91-90ec-c473daf430d4"},"_deposit":{"created_by":1,"id":"31691","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"31691"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00031691","sets":["1887:1890","1896:1898:1899:1910"]},"author_link":["405759","405761","405757","405756","405760","405758"],"item_9_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Data Processing Circuit of Solar Sensor Borne on K-10-11 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":"1040","bibliographicPageStart":"1033","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太陽角誤差電圧出力データ処理回路について述べる。4個の太陽電池を二組使用して精粗の姿勢誤差出力を得ている。太陽電池4個の出力の和差をとることによりピッチ,ヨー誤差出力を得ている。また精粗誤差出力を組合わせて零附近で2.5V/度の出力を,また±90°の範囲で対応する極性の4V以上の出力電圧を得ている.飛しょう実験の結果この回路の出力オフセットは40mv(1'角)であり,太陽光強度の変化による太陽電池出力の不平衡を評価できた.","subitem_description_type":"Abstract"}]},"item_9_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"The data processing circuit to obtain sun orientation error voltage applied for the 3-axis attitude control system of the K-10-11 rocket is described. 2-set of four solar cells are utilized for sources of each fine and coarse attitude error sensors. A combination of sum and/or difference of 4 of solar cells produces pitch and yaw error voltage outputs. Then combination of fine and coarse error outputs provides the sensitivity of 2.5 V/degree about zero error position. and the output voltage greater than 4 volts having proper polarity up to ±90° error angle. From flight test results, the offset voltage appeared in the output of this processing circuit was about 40 mV (1 arc-sec in sun orientation error) and the unbalance in solar cell outputs induced from solar intensity variation was estimated.","subitem_description_type":"Other"}]},"item_9_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: SA0124696000","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":"日本電気株式会社,宇宙開発事業部"},{"subitem_text_value":"日本電気株式会社,宇宙開発事業部"}]},"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, 實"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"小尾, 新三"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"吉本, 聖志"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"HIGASHIGUCHI, MInoru","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"OBI, Shinzoo","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"YOSHIMOTO, Seiji","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":"SA0124696.pdf","filesize":[{"value":"476.6 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"SA0124696.pdf","url":"https://jaxa.repo.nii.ac.jp/record/31691/files/SA0124696.pdf"},"version_id":"a44ec403-82c8-4037-8000-898386a5113c"}]},"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":"K-10-11号機太陽センサデータ処理回路(SASE)","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"K-10-11号機太陽センサデータ処理回路(SASE)"}]},"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":"31691","relation_version_is_last":true,"title":["K-10-11号機太陽センサデータ処理回路(SASE)"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T00:53:16.254257+00:00"}