{"created":"2023-06-20T14:40:50.628959+00:00","id":7802,"links":{},"metadata":{"_buckets":{"deposit":"a7918b96-863a-47d8-96dd-63f5dda42973"},"_deposit":{"created_by":1,"id":"7802","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"7802"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00007802","sets":["1543:1544:1561","1887:1891"]},"author_link":["41997","41995","41998","41999","41996","42002","42001","42000"],"item_5_alternative_title_1":{"attribute_name":"その他のタイトル","attribute_value_mlt":[{"subitem_alternative_title":"PLANET-C軌道制御時の3軸姿勢保持制御"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2003-02","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"245","bibliographicPageStart":"240","bibliographic_titles":[{"bibliographic_title":"平成14年度アストロダイナミクスシンポジウム:講演後刷り集"},{"bibliographic_title":"ISAS Proceedings of 12th Workshop on Astrodynamics and Flight Mechanics 2002: A Collection of Technical Papers","bibliographic_titleLang":"en"}]}]},"item_5_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"PLANET-Cは文部科学省宇宙科学研究所初の金星探査機である。PLANET-Cは3軸制御安定の小さな探査機であり500Nの軌道制御エンジン(OME)の発生する擾乱トルクが姿勢制御にとって大きな脅威となる。この擾乱トルクを抑制するため、外乱抑制制御策が比較検討された結果、新しいタイプの制御(トランジェント抑制制御)に問題解決の可能性があることが判った。","subitem_description_type":"Abstract"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"PLANET-C is the ISAS's first VENUS probe. Since PLANET-C is a small three-axis-stabilized spacecraft, the disturbance torque due to 500N Orbit Maneuver Engine (OME) is a big threat for attitude control. In order to manage the disturbance, various disturbance suppression control schemes have been designed for comparison. A new class of scheme, transient suppression compensator, may overcome the problem.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0045497040","subitem_description_type":"Other"}]},"item_5_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"宇宙科学研究所"}]},"item_5_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"The Institute of Space and Astronautical Science (ISAS)"}]},"item_5_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"0918-8053","subitem_source_identifier_type":"ISSN"}]},"item_5_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"NEC東芝スペースシステム"},{"subitem_text_value":"日本電気航空宇宙システム"},{"subitem_text_value":"日本電気航空宇宙システム"},{"subitem_text_value":"宇宙科学研究所"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"NEC TOSHIBA Space Systems Ltd."},{"subitem_text_language":"en","subitem_text_value":"NEC Aerospace Systems Ltd."},{"subitem_text_language":"en","subitem_text_value":"NEC Aerospace Systems Ltd."},{"subitem_text_language":"en","subitem_text_value":"Institute of Space and Astronautical Science"}]},"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":"栗井, 俊弘"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"日高, 智成"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"木村, 雅文"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"橋本, 樹明"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kurii, Toshihiro","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Hidaka, Tomonari","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kimura, Masafumi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Hashimoto, Tatsuaki","creatorNameLang":"en"}],"nameIdentifiers":[{}]}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"衛星姿勢制御","subitem_subject_scheme":"Other"},{"subitem_subject":"軌道投入操作","subitem_subject_scheme":"Other"},{"subitem_subject":"衛星姿勢撹乱","subitem_subject_scheme":"Other"},{"subitem_subject":"3軸安定化","subitem_subject_scheme":"Other"},{"subitem_subject":"宇宙探査","subitem_subject_scheme":"Other"},{"subitem_subject":"擾乱トルク","subitem_subject_scheme":"Other"},{"subitem_subject":"軌道操作エンジン","subitem_subject_scheme":"Other"},{"subitem_subject":"PLANET-C探査機","subitem_subject_scheme":"Other"},{"subitem_subject":"火星","subitem_subject_scheme":"Other"},{"subitem_subject":"satellite attitude control","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"orbit injection maneuver","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"satellite attitude disturbance","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"three-axis stabilization","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"space exploration","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"disturbance torque","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"orbit maneuver engine","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"PLANET-C prove","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Mars","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":"conference paper","resourceuri":"http://purl.org/coar/resource_type/c_5794"}]},"item_title":"Attitude control during orbit injection maneuver for venus probe PLANET-C","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"Attitude control during orbit injection maneuver for venus probe PLANET-C","subitem_title_language":"en"}]},"item_type_id":"5","owner":"1","path":["1561","1891"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"7802","relation_version_is_last":true,"title":["Attitude control during orbit injection maneuver for venus probe PLANET-C"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T07:33:50.399978+00:00"}