{"created":"2023-06-20T14:40:35.840265+00:00","id":7508,"links":{},"metadata":{"_buckets":{"deposit":"138e610d-d6ee-4bf7-b581-54c2f7849198"},"_deposit":{"created_by":1,"id":"7508","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"7508"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00007508","sets":["1543:1544:1557","1887:1891"]},"author_link":["40051","40052"],"item_5_alternative_title_1":{"attribute_name":"その他のタイトル","attribute_value_mlt":[{"subitem_alternative_title":"M-V7号機衛星分離後の軌道上運動解析"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2007-03","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"41","bibliographicPageStart":"37","bibliographic_titles":[{"bibliographic_title":"第16回アストロダイナミクスシンポジウム講演後刷り集　2006"},{"bibliographic_title":"Proceedings of 16th Workshop on JAXA Astrodynamics and Flight Mechanics","bibliographic_titleLang":"en"}]}]},"item_5_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"今年度夏期に打ち上げが予定されているM-V7号機では、主衛星であるSOLAR-Bと共に2つの小型衛星がサブペイロードとして搭載される。単純に軌道面外方向へ分離が行われると、軌道半周期後に衝突することになる。本研究では各衛星の分離後、軌道上において各衛星およびロケット上段の軌道運動を解析し、ノミナルのシーケンスから衛星分離速度および分離方向に誤差が生じたり、各衛星の弾道係数の見積もり誤差あるいは大気抵抗の変動がある場合にも、衝突が生じないことを検証する。","subitem_description_type":"Abstract"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"M-V-7 rocket, witch would be launched in this summer, bring main satellite 'SOLAR-B' and two small satellites as sub payload. If one of the small satellite separate from M-V-7 upper stage to normal direction as for velocity, the satellite would come into collision with M-V-7 upper stage after half period of orbit. In this paper, the on-orbit motion of each satellite and M-V-7 upper stage would by analyzed after separation. Under the consideration of several uncertainties like ballistic coefficient of each satellite and variation of air drag, the separation method witch doesn't happen to come into collision would be proposed.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0063481007","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/ISAS)"}]},"item_5_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"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":"Japan Aerospace Exploration Agency"}]},"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, 高行"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Yamamoto, Takayuki","creatorNameLang":"en"}],"nameIdentifiers":[{}]}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"ひので","subitem_subject_scheme":"Other"},{"subitem_subject":"SOLAR-B","subitem_subject_scheme":"Other"},{"subitem_subject":"太陽観測衛星","subitem_subject_scheme":"Other"},{"subitem_subject":"運動解析","subitem_subject_scheme":"Other"},{"subitem_subject":"軌道計算","subitem_subject_scheme":"Other"},{"subitem_subject":"軌道要素","subitem_subject_scheme":"Other"},{"subitem_subject":"距離","subitem_subject_scheme":"Other"},{"subitem_subject":"推力","subitem_subject_scheme":"Other"},{"subitem_subject":"衛星軌道","subitem_subject_scheme":"Other"},{"subitem_subject":"モンテカルロ法","subitem_subject_scheme":"Other"},{"subitem_subject":"計算機シミュレーション","subitem_subject_scheme":"Other"},{"subitem_subject":"衝突","subitem_subject_scheme":"Other"},{"subitem_subject":"弾道係数","subitem_subject_scheme":"Other"},{"subitem_subject":"HINODE","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"SOLAR-B","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Solar Physics Satellite","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"motion analysis","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"orbit calculation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"orbital element","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"distance","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"thrust","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"satellite orbit","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Monte Carlo method","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"computerized simulation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"collision","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"ballistic coefficient","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":"Motion analysis of satellites after separation from M-V-7 rocket","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"Motion analysis of satellites after separation from M-V-7 rocket","subitem_title_language":"en"}]},"item_type_id":"5","owner":"1","path":["1557","1891"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"7508","relation_version_is_last":true,"title":["Motion analysis of satellites after separation from M-V-7 rocket"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T07:38:26.363661+00:00"}