{"created":"2023-06-20T15:15:13.882329+00:00","id":45291,"links":{},"metadata":{"_buckets":{"deposit":"7e8d310c-d2ce-4050-a9f7-b41f7b9028d4"},"_deposit":{"created_by":1,"id":"45291","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"45291"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00045291","sets":["1887:1893","1896:1898:1913:1917"]},"author_link":["473902","473901"],"item_3_alternative_title_1":{"attribute_name":"その他のタイトル","attribute_value_mlt":[{"subitem_alternative_title":"誘導制御を伴なう宇宙航行系プログラムの軌道推定に関する理論構成"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1989-08","bibliographicIssueDateType":"Issued"},"bibliographicPageStart":"38","bibliographicVolumeNumber":"1032","bibliographic_titles":[{"bibliographic_title":"航空宇宙技術研究所報告"},{"bibliographic_title":"Technical Report of National Aerospace Laboratory TR-1032","bibliographic_titleLang":"en"}]}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"The theoretical specifications of the trajectory estimation for a space navigation system (observation and trajectory estimation processes with the function of guidance and control) of STANPS-N are presented in this paper. STANPS-N is the abbreviation for Space Trajectory and Mission Analysis Program System (Navigation version) developed at National Aerospace Laboratory. Observation data from the range and range-rate rader are processed sequentially by the conventional Kalman filter or extended Kalman filter with the system noise compensation method. Unknown parameters(for example, observation bias, station location, astronomical and geophysical constants) can also be estimated by the enlarged system formulation. The eveluation algorithms for the effect of the impulsive velocity correction on the change of estimate and error covariance matrix are also presented.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: NALTR1032000","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-1032","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"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Control Systems Division, National Aerospace Laboratory(NAL)"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"志甫, 徹"}],"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":"2020-01-29"}],"displaytype":"detail","filename":"naltr01032.pdf","filesize":[{"value":"2.4 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"naltr01032.pdf","url":"https://jaxa.repo.nii.ac.jp/record/45291/files/naltr01032.pdf"},"version_id":"64b4d5ae-8ae7-4c78-a5f7-c95356ae8fef"}]},"item_language":{"attribute_name":"言語","attribute_value_mlt":[{"subitem_language":"eng"}]},"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":"Theoretical Specifications of the Trajectory Estimation for a Space Navigation System with the Function of Guidance and Control","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"Theoretical Specifications of the Trajectory Estimation for a Space Navigation System with the Function of Guidance and Control","subitem_title_language":"en"}]},"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":"45291","relation_version_is_last":true,"title":["Theoretical Specifications of the Trajectory Estimation for a Space Navigation System with the Function of Guidance and Control"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T21:41:56.298952+00:00"}