{"created":"2023-06-20T15:13:52.707959+00:00","id":43849,"links":{},"metadata":{"_buckets":{"deposit":"68a88a64-64a6-4664-a6a3-146153076598"},"_deposit":{"created_by":1,"id":"43849","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"43849"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00043849","sets":["1887:1893","1896:1898:1913:1916"]},"author_link":["465930","465927","465928","465931","465929"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Simulation Program for Rocket Trajectory and Guidance Error Analysis Using Kalman Filter"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1974-11","bibliographicIssueDateType":"Issued"},"bibliographicPageStart":"66","bibliographicVolumeNumber":"266","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_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"In this report we present one phase of a study on error analysis of space trajectories,that is to say,how to build an error analysis program based on the modern estimation theory.The proposed method plays an essential role in the post-flight evaluations of the GN＆C system of a space vehicle,and is applicable as well to the mission planning phase.The simulation program thus constructed has the following capabilities:(1) generating any guided trajectories, noisy radar tracking data and IMU outputs(by DATA GENERATOR),and (2)conducting sensitivity analysis and guidance error recovery with regard to almost all guidance parameters in the “consider” option as well as in the “solve-for” option(by TRAJECTORY RE-CONSTRUCTOR).In the appendices,the basic subroutines and some of the application programs for space guidance are presented with the lists for user′s information.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: NALTM0266000","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-266","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計測部"},{"subitem_text_value":"航空宇宙技術研究所計測部"},{"subitem_text_value":"航空宇宙技術研究所計測部"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"村田, 正秋"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"志甫, 徹"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"吉田, 正廣"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"MURATA, Masaaki","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"SHIHO, Toru","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":"2020-01-28"}],"displaytype":"detail","filename":"naltm00266.pdf","filesize":[{"value":"3.0 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"naltm00266.pdf","url":"https://jaxa.repo.nii.ac.jp/record/43849/files/naltm00266.pdf"},"version_id":"29c7ddeb-2cfc-4247-bb00-577ab12c6fa4"}]},"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":"カルマンフィルターによる軌道および誘導誤差解析のためのシミュレーションプログラム","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"カルマンフィルターによる軌道および誘導誤差解析のためのシミュレーションプログラム"}]},"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":"43849","relation_version_is_last":true,"title":["カルマンフィルターによる軌道および誘導誤差解析のためのシミュレーションプログラム"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T22:06:51.328494+00:00"}