{"created":"2023-06-20T14:40:38.818184+00:00","id":7566,"links":{},"metadata":{"_buckets":{"deposit":"65f75aba-f545-45d7-80f1-8456d27d299f"},"_deposit":{"created_by":1,"id":"7566","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"7566"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00007566","sets":["1543:1544:1558","1887:1891"]},"author_link":["40504","40503"],"item_5_alternative_title_1":{"attribute_name":"その他のタイトル","attribute_value_mlt":[{"subitem_alternative_title":"太陽-地球系L2点周りのリサジュ基準軌道の設計"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2006-03","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"6","bibliographicPageStart":"1","bibliographic_titles":[{"bibliographic_title":"第15回アストロダイナミクスシンポジウム講演後刷り集　2005"},{"bibliographic_title":"Proceedings of 15th Workshop on JAXA Astrodynamics and Flight Mechanics","bibliographic_titleLang":"en"}]}]},"item_5_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"リサジュ軌道やハロー軌道は不安定なために数ヶ月間隔の軌道保持制御が必須であり、正確な摂動モデルの下でΔVゼロの基準軌道を前もって設計しておき、それに追従する様に保持制御が行なわれている。欧米では、3次以上の高次解析解を初期値として基準軌道が作成されているが、本論文では、線型解だけを使用してリサジュ基準軌道を作成する新しい方法を述べる。","subitem_description_type":"Abstract"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Since both Lissajous and halo orbits are unstable, orbital maintenance maneuvers at several month intervals are necessary. In order to perform orbital maintenance, a reference trajectory with zero Delta V is designed in advance under a precise model of perturbations. Orbital maintenance maneuvers are then performed such that the reference orbit is maintained. In Europe and the United States, a third- or higher-order analytical solution is used as an initial trajectory for obtaining a reference orbit. In this paper, we present a new method for reference Lissajous orbits which does not need higher-order solutions.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0063480001","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 総合技術研究本部"}]},"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 Institute of Space Technology and Aeronautics"}]},"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":"歌島, 昌由"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Utashima, Masayoshi","creatorNameLang":"en"}],"nameIdentifiers":[{}]}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"リサジュ基準軌道","subitem_subject_scheme":"Other"},{"subitem_subject":"軌道解析","subitem_subject_scheme":"Other"},{"subitem_subject":"衛星軌道","subitem_subject_scheme":"Other"},{"subitem_subject":"ラグランジュ平衡点","subitem_subject_scheme":"Other"},{"subitem_subject":"逐次2次計画法","subitem_subject_scheme":"Other"},{"subitem_subject":"SQP","subitem_subject_scheme":"Other"},{"subitem_subject":"L2点","subitem_subject_scheme":"Other"},{"subitem_subject":"軌道","subitem_subject_scheme":"Other"},{"subitem_subject":"2次計画法","subitem_subject_scheme":"Other"},{"subitem_subject":"3体問題","subitem_subject_scheme":"Other"},{"subitem_subject":"軌道決定","subitem_subject_scheme":"Other"},{"subitem_subject":"摂動","subitem_subject_scheme":"Other"},{"subitem_subject":"拘束条件","subitem_subject_scheme":"Other"},{"subitem_subject":"軌道","subitem_subject_scheme":"Other"},{"subitem_subject":"reference Lissajous trajectory","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"trajectory analysis","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"satellite orbit","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Lagrangian equilibrium point","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"sequential quadratic programming","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"SQP","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"L2 point","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"trajectory","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"quadratic programming","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"three body problem","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"orbit determination","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"perturbation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"constraint","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"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":"Design of reference Lissajous trajectories around the L2 point in the Sun-Earth system","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"Design of reference Lissajous trajectories around the L2 point in the Sun-Earth system","subitem_title_language":"en"}]},"item_type_id":"5","owner":"1","path":["1558","1891"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"7566","relation_version_is_last":true,"title":["Design of reference Lissajous trajectories around the L2 point in the Sun-Earth system"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T07:37:32.674593+00:00"}