{"created":"2023-06-20T14:40:25.801539+00:00","id":7307,"links":{},"metadata":{"_buckets":{"deposit":"699d16f8-1aa5-4867-a4bd-8ae8e45b0160"},"_deposit":{"created_by":1,"id":"7307","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"7307"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00007307","sets":["1543:1544:1554","1887:1891"]},"author_link":["38612","38620","38622","38613","38619","38617","38610","38624","38615","38608","38621","38611","38616","38609","38614","38625","38623","38626","38607","38618"],"item_5_alternative_title_1":{"attribute_name":"その他のタイトル","attribute_value_mlt":[{"subitem_alternative_title":"干渉SAR 観測のための高精度自律軌道制御の高機能化"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2010-03","bibliographicIssueDateType":"Issued"},"bibliographicVolumeNumber":"2009","bibliographic_titles":[{"bibliographic_title":"アストロダイナミクスシンポジウム講演後刷り集"},{"bibliographic_title":"Proceedings of 19th workshop on JAXA Astrodynamics and Flight Mechanics","bibliographic_titleLang":"en"}]}]},"item_5_description_14":{"attribute_name":"会議概要（会議名, 開催地, 会期, 主催者等）","attribute_value_mlt":[{"subitem_description":"アストロダイナミクスシンポジウム (2009年7月30-31日. 宇宙航空研究開発機構宇宙科学研究本部))","subitem_description_type":"Other"}]},"item_5_description_15":{"attribute_name":"会議概要（会議名, 開催地, 会期, 主催者等）（英）","attribute_value_mlt":[{"subitem_description":"Workshop on JAXA Astrodynamics and Flight Mechanics, 2009 (July 30-31, 2009. Institute of Space and Astronautical Science (ISAS), Japan Aerospace Exploration Agency (JAXA)), Sagamihara, Kanagawa Japan","subitem_description_type":"Other"}]},"item_5_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"摘要: 合成開口レーダー衛星による干渉SAR 観測を確実に実施するためには、回帰軌道の精密な保持が必要である。これを実現するためには、詳細な摂動モデルによる軌道予測が必須である。また、精密な軌道保持を実現するためには、高頻度な軌道制御が必要となり、運用の負荷が増大するため、宇宙機の自律的な軌道制御が必要となる。これまでの検討では、一定間隔の軌道制御により要求される保持精度が達成できることを確認した。さらに検討を進めて、観測運用と軌道制御運用との干渉を避けるため、軌道制御を低頻度化し、増速位置を海域上空に限った場合でも要求精度が満足できることを確認した。本講演では、その高機能化検討結果について報告する。","subitem_description_type":"Abstract"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Precise maintenance of the recurrent orbit is necessary to execute certainly SAR interferometry observation by satellite. Orbit prediction with detailed perturbation models is required to efficient maintenance. In addition, high-frequency maneuver is necessary to precise maintenance. Because of these factors, operative load increases. To solve this problem, autonomous orbit control is needed. For the past examination, we confirmed that the spacecraft with constant cycle of maintenance fly autonomously less than 500m from the reference orbit which is relatively fixed to earth surface. Furthermore, for avoiding that the orbital maneuver operation conflicts with observation, we improved the control law to lower the frequency and to limit the control point on the sea. Under these conditions, we confirmed the orbit maintenance satisfied with the requirements. In this lecture, we report it about the examination result.","subitem_description_type":"Other"}]},"item_5_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_5_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_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0064734002","subitem_description_type":"Other"}]},"item_5_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"宇宙航空研究開発機構宇宙科学研究本部"}]},"item_5_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)"}]},"item_5_source_id_24":{"attribute_name":"書誌レコードID","attribute_value_mlt":[{"subitem_source_identifier":"AA11567475","subitem_source_identifier_type":"NCID"}]},"item_5_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"三菱スペース・ソフトウエア"},{"subitem_text_value":"三菱スペース・ソフトウエア"},{"subitem_text_value":"宇宙航空研究開発機構"},{"subitem_text_value":"宇宙航空研究開発機構"},{"subitem_text_value":"宇宙航空研究開発機構"},{"subitem_text_value":"宇宙航空研究開発機構"},{"subitem_text_value":"宇宙航空研究開発機構"},{"subitem_text_value":"宇宙航空研究開発機構"},{"subitem_text_value":"宇宙航空研究開発機構"},{"subitem_text_value":"宇宙航空研究開発機構"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Mitsubishi Space Software"},{"subitem_text_language":"en","subitem_text_value":"Mitsubishi Space Software"},{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency (JAXA)"},{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency (JAXA)"},{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency (JAXA)"},{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency (JAXA)"},{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency (JAXA)"},{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency (JAXA)"},{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency (JAXA)"},{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency (JAXA)"}]},"item_access_right":{"attribute_name":"アクセス権","attribute_value_mlt":[{"subitem_access_right":"metadata only access","subitem_access_right_uri":"http://purl.org/coar/access_right/c_14cb"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"山本, 昌幸"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"中嶋, 憲"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"河野, 功"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"山元, 透"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"巳谷, 真司"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"近藤, 義典"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"岩田, 隆敬"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"歌島, 昌由"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"大澤, 右二"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"島田, 政信"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Yamamoto, Masayuki","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Nakajima, Ken","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kawano, Isao","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Yamamoto, Toru","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Mitani, Shinji","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kondo, Yoshinori","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Iwata, Takanori","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Utashima, Masayoshi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Osawa, Yuji","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Shimada, Masanobu","creatorNameLang":"en"}],"nameIdentifiers":[{}]}]},"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":"conference paper","resourceuri":"http://purl.org/coar/resource_type/c_5794"}]},"item_title":"The improvement of the precise autonomous orbit control for SAR interferometer satellite","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"The improvement of the precise autonomous orbit control for SAR interferometer satellite","subitem_title_language":"en"}]},"item_type_id":"5","owner":"1","path":["1554","1891"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"7307","relation_version_is_last":true,"title":["The improvement of the precise autonomous orbit control for SAR interferometer satellite"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T07:41:31.886913+00:00"}