{"created":"2023-06-20T14:40:45.551571+00:00","id":7687,"links":{},"metadata":{"_buckets":{"deposit":"d02e363d-b2c7-46ca-b872-98b776672ca3"},"_deposit":{"created_by":1,"id":"7687","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"7687"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00007687","sets":["1543:1544:1559","1887:1891"]},"author_link":["41207","41210","41208","41212","41211","41209"],"item_5_alternative_title_1":{"attribute_name":"その他のタイトル","attribute_value_mlt":[{"subitem_alternative_title":"楕円軌道上小惑星への最小燃料軌道"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2005-03","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"317","bibliographicPageStart":"314","bibliographic_titles":[{"bibliographic_title":"平成16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 14th Workshop on Astrodynamics and Flight Mechanics 2004: A Collection of Technical Papers","bibliographic_titleLang":"en"}]}]},"item_5_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"本稿は、多数ある小惑星の中から、目標惑星を選択する時に使用する情報を提供することを目的としている。電気推進などの低推力を用いた楕円軌道上の小惑星への最小燃料軌道に関して数値計算をもとにその特徴を示す。対象とする小惑星軌道は地球軌道と同一平面内の2次元問題とし、推力は太陽からの距離の2乗に反比例するモデルを使用する。出発時刻の変更が消費燃料の変化にどのように影響するかを中心にデータを示す。地球軌道の外側に小惑星軌道が存在する場合の結果を示す。離心率が高いと、消費燃料が少なく、出発時間の影響も少ないことが示される。","subitem_description_type":"Abstract"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"The purpose of this paper is to provide the information for selection of a target asteroid from many asteroids. The results of numerical calculation show the feature of trajectories to an asteroid on elliptic orbit with solar electric propulsion. It is assumed that the target orbit exists in the same plane of the earth's orbit and the maximum available thrust is inversely proportional to the square of distance from the sun. The results show how the minimum fuel is affected by the departure time. This paper shows the results of cases that orbits of asteroid are outside of the earth's orbit. It is concluded that orbits with higher eccentricity are less fuel and less affection of departure time.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0047897054","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_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":"横浜国立大学 大学院環境情報研究院"},{"subitem_text_value":"横浜国立大学 大学院環境情報学府"},{"subitem_text_value":"横浜国立大学 大学院環境情報学府"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Yokohama National University Graduate School of Environment and Information Sciences"},{"subitem_text_language":"en","subitem_text_value":"Yokohama National University Graduate School of Environment and Information Sciences"},{"subitem_text_language":"en","subitem_text_value":"Yokohama National University Graduate School of Environment and Information Sciences"}]},"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":"上野, 誠也"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"浅岡, 博則"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"古賀, 心太郎"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Ueno, Seiya","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Asaoka, Hironori","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Koga, Shintaro","creatorNameLang":"en"}],"nameIdentifiers":[{}]}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"小惑星","subitem_subject_scheme":"Other"},{"subitem_subject":"最小燃料軌道","subitem_subject_scheme":"Other"},{"subitem_subject":"楕円軌道","subitem_subject_scheme":"Other"},{"subitem_subject":"数値解析","subitem_subject_scheme":"Other"},{"subitem_subject":"最適軌道","subitem_subject_scheme":"Other"},{"subitem_subject":"太陽電気推進","subitem_subject_scheme":"Other"},{"subitem_subject":"極座標","subitem_subject_scheme":"Other"},{"subitem_subject":"離心率","subitem_subject_scheme":"Other"},{"subitem_subject":"asteroid","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"minimum fuel trajectory","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"elliptical orbit","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"numerical analysis","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"optimal trajectory","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"solar electric propulsion","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"polar coordinate","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"eccentricity","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":"Minimum fuel trajectory to an asteroid on elliptic orbit","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"Minimum fuel trajectory to an asteroid on elliptic orbit","subitem_title_language":"en"}]},"item_type_id":"5","owner":"1","path":["1559","1891"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"7687","relation_version_is_last":true,"title":["Minimum fuel trajectory to an asteroid on elliptic orbit"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T07:35:37.606252+00:00"}