{"created":"2023-06-20T14:40:35.715126+00:00","id":7505,"links":{},"metadata":{"_buckets":{"deposit":"f3ec3e5f-10f2-46b8-83cf-e187f7013454"},"_deposit":{"created_by":1,"id":"7505","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"7505"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00007505","sets":["1543:1544:1557","1887:1891"]},"author_link":["40044","40042","40041","40043","40039","40040"],"item_5_alternative_title_1":{"attribute_name":"その他のタイトル","attribute_value_mlt":[{"subitem_alternative_title":"楕円軌道のフォーメーションフライトに関する考察"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2007-03","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"27","bibliographicPageStart":"22","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":"本稿では楕円軌道における宇宙機の編隊飛行制御について検討する。相対的なフォーメーション軌道において、楕円軌道と同じ対称性を仮定することによってフォーメーションの初期条件を導く。この初期条件から従宇宙機が主宇宙機の周りを少ない距離変動で周回するような軌道や、従宇宙機が局所水平面内で周回する軌道など、いくつかの特徴的な軌道を求めることができる。","subitem_description_type":"Abstract"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Formation flight of spacecraft in eccentric orbits is considered in this paper. Symmetry of the eccentric orbits is assumed in a relative formation trajectory, and under this assumption, relations of initial conditions in formation flight are derived. Some characteristic trajectories are obtained from these relations, such as a trajectory where a deputy spacecraft rotates around a chief spacecraft with relatively small variation in the distance between the two spacecraft, or a trajectory where the deputy spacecraft moves on a local horizontal plane on which the chief spacecraft exists. Formation flight by plural spacecraft is possible by combining these relative trajectories.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0063481004","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":"名古屋大学"},{"subitem_text_value":"三菱電機"},{"subitem_text_value":"三菱電機"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Nagoya University"},{"subitem_text_language":"en","subitem_text_value":"Mitsubishi Electric Corporation"},{"subitem_text_language":"en","subitem_text_value":"Mitsubishi Electric Corporation"}]},"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":"山田, 克彦"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"吉河, 章二"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"島, 岳也"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Yamada, Katsuhiko","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Yoshikawa, Shoji","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Shima, Takeya","creatorNameLang":"en"}],"nameIdentifiers":[{}]}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"編隊飛行","subitem_subject_scheme":"Other"},{"subitem_subject":"軌道計算","subitem_subject_scheme":"Other"},{"subitem_subject":"偏心軌道","subitem_subject_scheme":"Other"},{"subitem_subject":"対称性","subitem_subject_scheme":"Other"},{"subitem_subject":"数学モデル","subitem_subject_scheme":"Other"},{"subitem_subject":"参照軌道","subitem_subject_scheme":"Other"},{"subitem_subject":"相対軌道","subitem_subject_scheme":"Other"},{"subitem_subject":"編隊軌道","subitem_subject_scheme":"Other"},{"subitem_subject":"円軌道","subitem_subject_scheme":"Other"},{"subitem_subject":"楕円軌道","subitem_subject_scheme":"Other"},{"subitem_subject":"偏心率","subitem_subject_scheme":"Other"},{"subitem_subject":"運動方程式","subitem_subject_scheme":"Other"},{"subitem_subject":"宇宙機軌道","subitem_subject_scheme":"Other"},{"subitem_subject":"formation flying","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"orbit calculation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"eccentric orbit","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"symmetry","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"mathematical model","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"reference trajectory","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"relative trajectory","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"formation trajectory","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"circular orbit","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"elliptical orbit","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"eccentricity","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"equation of motion","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"spacecraft trajectory","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":"Spacecraft formation flying in eccentric orbits","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"Spacecraft formation flying in eccentric orbits","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":"7505","relation_version_is_last":true,"title":["Spacecraft formation flying in eccentric orbits"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T07:38:29.365080+00:00"}