{"created":"2023-06-20T15:10:13.261984+00:00","id":39815,"links":{},"metadata":{"_buckets":{"deposit":"97c81108-390b-43af-81d9-95fdfcd4d28e"},"_deposit":{"created_by":1,"id":"39815","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"39815"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00039815","sets":["1887:1893","1896:1898:1913:1916"]},"author_link":["444622","444620","444618","444619","444623","444621"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Calibration tests and its results of on-board inertial sensors for a 5 percent model of the NAL spaceplane"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1996-11","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"19","bibliographicPageStart":"1","bibliographicVolumeNumber":"703","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":"スペースプレーン(Spaceplane:SP)は水平離着陸式の再使用型有人宇宙往還機であり、航空機と宇宙機の特性を合わせ持つものである。航空宇宙技術研究所では実機を想定したSPの0次型を設定し、空力、構造、エンジンおよび制御の各分野の基礎研究を進めている。本動的風洞試験はSPの着陸進入低速度飛行時の空力動安定微係数の同定や飛行制御則の評価などのために、0次型SPの約1/20模型(全長3.2m、全幅1.49m、重量約30kg)を大型低速風洞内にケーブルマウント方式で支持(5自由度運動が可。前後並進運動は不可。)して行うものである。本動的風洞試験では模型の運動計測系が用意され、模型には3舵を駆動する電動アクチュエータが取り付けられている。模型の運動は搭載計測系および地上計測系から出力されるデータを地上の制御計測用計算機に伝送し、同計算機によって算出された制御信号を模型上の舵面アクチュエータに伝送することによって模型を制御する仕組みになっている。本報告では模型搭載計測系(慣性計測装置およびバーチカルジャイロ)の概要およびその較正試験について述べる。","subitem_description_type":"Abstract"}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Dynamic wind tunnel tests using a five percent cable mounted model of the NAL spaceplane have been conducted in the NAL low-speed large scale wind tunnel. As onboard inertial sensors, an Inertial Measurement Unit (IMU) and a Vertical Gyro (VG) were installed on the model to measure angular rates about three axes of the model and accelerations along three axes, and to measure attitude angles of the model. In this report, the IMU and the VG are outlined, and the calibration tests of the inertial sensors are reported.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0000678000","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-703","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"}]},"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"}]},"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":"Takizawa, Minoru","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Sasa, Shuichi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Nagayasu, Masahiko","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":"naltm00703.pdf","filesize":[{"value":"2.6 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"naltm00703.pdf","url":"https://jaxa.repo.nii.ac.jp/record/39815/files/naltm00703.pdf"},"version_id":"2edc1c46-470d-4788-8072-562bc420af7f"}]},"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":"ケーブルマウント・モデル","subitem_subject_scheme":"Other"},{"subitem_subject":"バーチカルジャイロ","subitem_subject_scheme":"Other"},{"subitem_subject":"較正試験","subitem_subject_scheme":"Other"},{"subitem_subject":"風洞試験","subitem_subject_scheme":"Other"},{"subitem_subject":"角速度計","subitem_subject_scheme":"Other"},{"subitem_subject":"加速度計","subitem_subject_scheme":"Other"},{"subitem_subject":"スペースプレーン","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":"cable mounted model","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"vertical gyro","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"calibration test","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"wind tunnel test","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"angular velocimeter","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"accelerometer","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"space plane","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":"動的風洞試験に用いるスペースプレーン模型搭載運動計測系の較正","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"動的風洞試験に用いるスペースプレーン模型搭載運動計測系の較正"}]},"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":"39815","relation_version_is_last":true,"title":["動的風洞試験に用いるスペースプレーン模型搭載運動計測系の較正"],"weko_creator_id":"1","weko_shared_id":1},"updated":"2023-06-20T19:18:51.441633+00:00"}