{"created":"2023-06-20T14:35:34.374205+00:00","id":1805,"links":{},"metadata":{"_buckets":{"deposit":"ccdde745-7629-4c85-ba05-d561234dac30"},"_deposit":{"created_by":1,"id":"1805","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"1805"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00001805","sets":["1887:1893","9:10:25:29"]},"author_link":["475915","475913","475914","475916"],"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2018-02-22","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"16","bibliographicPageStart":"1","bibliographicVolumeNumber":"JAXA-RR-17-010E","bibliographic_titles":[{"bibliographic_title":"宇宙航空研究開発機構研究開発報告"},{"bibliographic_title":"JAXA Research and Development Report","bibliographic_titleLang":"en"}]}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"A flight experiment using a stratospheric balloon, designated as D-SEND#2, was carried out in 2015. This paper describes a guidance law of the D-SEND#2 vehicle. A typical problem of flight experiment using a stratospheric balloon is that it has no nominal trajectory. Therefore, a new real-time trajectory prediction method is devised to overcome this problem. The method solves equations of motion directly for various load factor commands. The guidance law was evaluated using Monte Carlo simulation, and its result was the success rate of 98.1%. The guidance law has a little tolerance to the uncertainty of steady wind and of the model error of drag coefficient because the vehicle has no engine nor devices for velocity control. Actual flight experiments demonstrated that the guidance law satisfied all mission requirements and that it contributed greatly to the mission success.","subitem_description_type":"Other"}]},"item_3_description_18":{"attribute_name":"内容記述","attribute_value_mlt":[{"subitem_description":"形態: カラー図版あり","subitem_description_type":"Other"}]},"item_3_description_19":{"attribute_name":"内容記述（英）","attribute_value_mlt":[{"subitem_description":"Physical characteristics: Original contains color illustrations","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA1730019000","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: JAXA-RR-17-010E","subitem_description_type":"Other"}]},"item_3_identifier_registration":{"attribute_name":"ID登録","attribute_value_mlt":[{"subitem_identifier_reg_text":"10.20637/JAXA-RR-17-010E/0001","subitem_identifier_reg_type":"JaLC"}]},"item_3_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"宇宙航空研究開発機構(JAXA)"}]},"item_3_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"Japan Aerospace Exploration Agency (JAXA)"}]},"item_3_source_id_22":{"attribute_name":"ISSNONLINE","attribute_value_mlt":[{"subitem_source_identifier":"2433-2216","subitem_source_identifier_type":"ISSN"}]},"item_3_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"宇宙航空研究開発機構研究開発部門第一研究ユニット(JAXA)"},{"subitem_text_value":"宇宙航空研究開発機構航空技術部門飛行技術研究ユニット(JAXA)"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Research Unit I, Research and Development Directorate, Japan Aerospace Exploration Agency (JAXA)"},{"subitem_text_language":"en","subitem_text_value":"Flight Research Unit, Aeronautical Technology Directorate, Japan Aerospace Exploration Agency (JAXA)"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"鈴木, 広一"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"二宮, 哲次郎"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Suzuki, Hirokazu","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Ninomiya, Tetsujiro","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":"2020-01-31"}],"displaytype":"detail","filename":"AA1730019000.pdf","filesize":[{"value":"1.2 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"AA1730019000.pdf","url":"https://jaxa.repo.nii.ac.jp/record/1805/files/AA1730019000.pdf"},"version_id":"f23ef926-bdb3-43cd-b41f-ea89088f802f"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"Guidance and Control","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Real-time","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Trajectory Prediction","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"D-SEND","subitem_subject_language":"en","subitem_subject_scheme":"Other"}]},"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":"Guidance Law Based on Real-time Trajectory Prediction for D-SEND#2","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"Guidance Law Based on Real-time Trajectory Prediction for D-SEND#2","subitem_title_language":"en"}]},"item_type_id":"3","owner":"1","path":["29","1893"],"pubdate":{"attribute_name":"公開日","attribute_value":"2018-02-22"},"publish_date":"2018-02-22","publish_status":"0","recid":"1805","relation_version_is_last":true,"title":["Guidance Law Based on Real-time Trajectory Prediction for D-SEND#2"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T21:38:49.532654+00:00"}