{"created":"2023-06-20T15:11:29.422963+00:00","id":41159,"links":{},"metadata":{"_buckets":{"deposit":"bbd9bec7-d0ac-4355-bc9c-c0a1957576e0"},"_deposit":{"created_by":1,"id":"41159","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"41159"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00041159","sets":["1887:1893","1896:1898:1913:1917"]},"author_link":["450834","450833","450835","450832"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Calculation of the required sensor accuracy to obtain a specified state estimation accuracy"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1992-07","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"6","bibliographicPageStart":"1","bibliographicVolumeNumber":"1173","bibliographic_titles":[{"bibliographic_title":"航空宇宙技術研究所報告"},{"bibliographic_title":"Technical Report of National Aerospace Laboratory","bibliographic_titleLang":"en"}]}]},"item_3_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"飛行試験データの取得などに用いられる計測用センサシステムの設計においては、センサの必要精度の決定が重要である。本報では計測されたデータを用いてカルマンフィルタにより状態推定を行うとき、指定された状態推定精度を達成するために必要となるセンサ系の精度を計算する一手法を示す。これは状態推定問題における逆問題に相当し、観測側センサ精度と入力側センサ精度が、指定された推定誤差分散に対して最適化手法により求められる。Gauss-Newton法が繰り返し計算による最適化計算に用いられ、3次系での数値例により基本特性が示される。","subitem_description_type":"Abstract"}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"For the design of sensor systems for flight test data acquisition, the determination of necessary accuracy of the sensors is important. In this report, one method is presented to calculate the sensor accuracy to obtain a specified state estimation accuracy by a Kalman filter. This is an inverse problem of a state estimation problem in which observation sensor or input sensor accuracy is obtained by optimization method. Gauss-Newton method is applied in the iterative optimization calculation, and the basic performance is presented by numerical example using 3rd order linear system model.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0004189000","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 TR-1173","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":"0389-4010","subitem_source_identifier_type":"ISSN"}]},"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"}]},"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"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"佐々, 修一"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"永安, 正彦"}],"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":"naltr01173.pdf","filesize":[{"value":"440.0 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"naltr01173.pdf","url":"https://jaxa.repo.nii.ac.jp/record/41159/files/naltr01173.pdf"},"version_id":"4d22bdd6-bbaf-4f39-af4b-262b15806e1d"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"誤差解析","subitem_subject_scheme":"Other"},{"subitem_subject":"信号解析","subitem_subject_scheme":"Other"},{"subitem_subject":"誤差極小化","subitem_subject_scheme":"Other"},{"subitem_subject":"入出力最適化","subitem_subject_scheme":"Other"},{"subitem_subject":"センサ精度","subitem_subject_scheme":"Other"},{"subitem_subject":"状態推定精度","subitem_subject_scheme":"Other"},{"subitem_subject":"計測理論","subitem_subject_scheme":"Other"},{"subitem_subject":"観測理論","subitem_subject_scheme":"Other"},{"subitem_subject":"カルマンフィルタ","subitem_subject_scheme":"Other"},{"subitem_subject":"拘束条件付き最適化","subitem_subject_scheme":"Other"},{"subitem_subject":"数値的探索アルゴリズム","subitem_subject_scheme":"Other"},{"subitem_subject":"飛行試験","subitem_subject_scheme":"Other"},{"subitem_subject":"データ取得","subitem_subject_scheme":"Other"},{"subitem_subject":"ユークリッドノルム","subitem_subject_scheme":"Other"},{"subitem_subject":"リカッチ方程式","subitem_subject_scheme":"Other"},{"subitem_subject":"error analysis","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"signal analysis","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"error minimization","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"input output optimization","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"sensor accuracy","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"state estimation accuracy","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"instrumentation theory","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"observation theory","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Kalman filter","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"constrained optimization","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"numerical search algorithm","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"flight test","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"data aquisition","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Euclidean norm","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Riccatti equation","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":"指定された状態推定精度実現のためのセンサ要求精度の導出","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"指定された状態推定精度実現のためのセンサ要求精度の導出"}]},"item_type_id":"3","owner":"1","path":["1893","1917"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"41159","relation_version_is_last":true,"title":["指定された状態推定精度実現のためのセンサ要求精度の導出"],"weko_creator_id":"1","weko_shared_id":1},"updated":"2023-06-20T19:12:57.284572+00:00"}