{"created":"2023-06-20T15:10:18.367417+00:00","id":39891,"links":{},"metadata":{"_buckets":{"deposit":"3023e449-00e9-4cc6-ba9e-c2d51ea4586d"},"_deposit":{"created_by":1,"id":"39891","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"39891"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00039891","sets":["1887:1893","1896:1898:1913:1916"]},"author_link":["445481","445482","445480","445485","445483","445484","445478","445479"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Evaluation of an IMU using fiber optic gyros in dynamic wind tunnel tests"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1996-11","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"16","bibliographicPageStart":"1","bibliographicVolumeNumber":"705","bibliographic_titles":[{"bibliographic_title":"航空宇宙技術研究所資料"},{"bibliographic_title":"Technical Memorandum of National Aerospace Laboratory","bibliographic_titleLang":"en"}]}]},"item_3_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"NAL(航空宇宙技術研究所)が提案しているスペースプレーンの5％モデルを用いたケーブルマウント方式による動的風洞試験の研究が、その空力パラメータを同定するために行われた。本研究において、光ファイバージャイロ(測定範囲:±100度/s、精度:±1％FS)を用いるIMU(慣性計測装置)が動的風洞試験用として製作され、模型の計測・制御系に装着されて模型の機軸まわりの角速度および機軸方向の加速度を計測するために使用された。本報告では、使用した光ファイバージャイロの概要、本IMUの較正試験および動的風洞試験について述べる。結論として、本IMUは模型の運動制御系において有効に使用された。","subitem_description_type":"Abstract"}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"A study of dynamic wind tunnel tests using a five percent NAL (National Aerospace Laboratory) spaceplane model was conducted to identify the aerodynamic parameters of the spaceplane model. In this study, an IMU (Inertial Measurement Unit) using fiber optic gyros (measurement range: +/- 100 deg/s, accuracy: +/- 1 percent FS) was developed for dynamic wind tunnel tests and installed on the control system of the model to measure both angular rates about three axes of the model and accelerations along three axes. In this paper the outline of the fiber optic gyro, the calibration test and the dynamic wind tunnel tests for the IMU are described. In conclusion the IMU was used effectively on the control system of the spaceplane model.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0000869000","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 TM-705","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":"0452-2982","subitem_source_identifier_type":"ISSN"}]},"item_3_source_id_24":{"attribute_name":"書誌レコードID","attribute_value_mlt":[{"subitem_source_identifier":"AN00314334","subitem_source_identifier_type":"NCID"}]},"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 制御部"},{"subitem_text_value":"航空宇宙技術研究所 制御部"},{"subitem_text_value":"航空宇宙技術研究所 制御部"},{"subitem_text_value":"航空宇宙技術研究所 制御部"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Control Systems Division"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Control Systems Division"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Control Systems Division"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Control Systems Division"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"滝沢, 実"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"佐々, 修一"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"永安, 正彦"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"木村, 武雄"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Takizawa, Minoru","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Sasa, Shuichi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Nagayasu, Masahiko","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kimura, Takeo","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":"2020-01-27"}],"displaytype":"detail","filename":"naltm00705.pdf","filesize":[{"value":"2.3 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"naltm00705.pdf","url":"https://jaxa.repo.nii.ac.jp/record/39891/files/naltm00705.pdf"},"version_id":"b6112c24-2414-4fe2-81d6-6185d3d2cee3"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"IMU","subitem_subject_scheme":"Other"},{"subitem_subject":"慣性計測装置","subitem_subject_scheme":"Other"},{"subitem_subject":"FOG","subitem_subject_scheme":"Other"},{"subitem_subject":"光ファイバージャイロ","subitem_subject_scheme":"Other"},{"subitem_subject":"動的風洞試験","subitem_subject_scheme":"Other"},{"subitem_subject":"SP","subitem_subject_scheme":"Other"},{"subitem_subject":"スペースプレーン","subitem_subject_scheme":"Other"},{"subitem_subject":"FOG-IMU較正試験","subitem_subject_scheme":"Other"},{"subitem_subject":"ケーブルマウント方式","subitem_subject_scheme":"Other"},{"subitem_subject":"位相変調方式","subitem_subject_scheme":"Other"},{"subitem_subject":"IMU","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"inertial measurement unit","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"FOG","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"fiber optic gyro","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"dynamic wind tunnel test","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"SP","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"spaceplane","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"FOG IMU calibration test","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"cable mount method","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"phase modulation method","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":"光ファイバージャイロを用いたIMUの動的風洞試験による性能評価","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"光ファイバージャイロを用いたIMUの動的風洞試験による性能評価"}]},"item_type_id":"3","owner":"1","path":["1893","1916"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"39891","relation_version_is_last":true,"title":["光ファイバージャイロを用いたIMUの動的風洞試験による性能評価"],"weko_creator_id":"1","weko_shared_id":1},"updated":"2023-06-20T19:18:32.900591+00:00"}