{"created":"2023-06-20T14:40:48.244899+00:00","id":7748,"links":{},"metadata":{"_buckets":{"deposit":"61d42933-bbe1-4ae6-b97c-0eb1a34fd3c2"},"_deposit":{"created_by":1,"id":"7748","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"7748"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00007748","sets":["1543:1544:1560","1887:1891"]},"author_link":["41662","41661","41664","41660","41663","41659"],"item_5_alternative_title_1":{"attribute_name":"その他のタイトル","attribute_value_mlt":[{"subitem_alternative_title":"インパルス的な速度変更による接近軌道の設計と制御"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2004-02","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"296","bibliographicPageStart":"290","bibliographic_titles":[{"bibliographic_title":"平成15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 13th Workshop on Astrodynamics and Flight Mechanics 2003: A Collection of Technical Papers","bibliographic_titleLang":"en"}]}]},"item_5_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"Hillの方程式を用いて、真円の衛星軌道上で故障衛星(ターゲット)の周りを飛行する宇宙ロボット(チェイサ)の動力学を考える。インパルス的な速度変更による接近軌道を提案する。また、軌道の誤差システムを提案し、最適レギュレータによって軌道を安定化する。ターゲットとチェイサ間の相対的な角度のみを観測する拡張カルマンフィルタを導入する。現実的な条件で、LQR、拡張カルマンフィルタ、VICを含む統合的なシミュレーションによって提案手法の有効性を示す。","subitem_description_type":"Abstract"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Based on the Hill's equation, orbital dynamics of a space robot (chaser) flying around a trouble satellite (target) on a circular orbit around the earth is considered. Approach trajectories by impulsive thrust are proposed. Moreover discrete modeling of error system is proposed and the trajectory is stabilized by LQR. An extended kalman filter which observes only the relative angle between the target and the chaser satellites is introduced. The effectiveness of proposed method is shown by an integrated simulation including LQR, EKF, and VIC (Velocity Increment Cutoff) under practical conditions.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0046652047","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":"大阪大学 大学院基礎工学研究科"},{"subitem_text_value":"大阪大学 大学院基礎工学研究科"},{"subitem_text_value":"大阪大学 大学院基礎工学研究科"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Osaka University Graduate School of Engineering Science"},{"subitem_text_language":"en","subitem_text_value":"Osaka University Graduate School of Engineering Science"},{"subitem_text_language":"en","subitem_text_value":"Osaka University Graduate School of Engineering 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":"菅原, 正行"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"升谷, 保博"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"宮崎, 文夫"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Sugahara, Masayuki","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Masutani, Yasuhiro","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Miyazaki, Fumio","creatorNameLang":"en"}],"nameIdentifiers":[{}]}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"標的","subitem_subject_scheme":"Other"},{"subitem_subject":"チェイサ","subitem_subject_scheme":"Other"},{"subitem_subject":"インパルス的速度変更","subitem_subject_scheme":"Other"},{"subitem_subject":"接近軌道","subitem_subject_scheme":"Other"},{"subitem_subject":"人工衛星","subitem_subject_scheme":"Other"},{"subitem_subject":"円軌道","subitem_subject_scheme":"Other"},{"subitem_subject":"カルマンフィルター","subitem_subject_scheme":"Other"},{"subitem_subject":"フィードバック制御","subitem_subject_scheme":"Other"},{"subitem_subject":"target","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"chaser","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"impulsive velocity change","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"approach trajectory","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"artificial satellite","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"circular orbit","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Kalman filter","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"feedback control","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 and control of approach trajectory by impulsive velocity change","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"Design and control of approach trajectory by impulsive velocity change","subitem_title_language":"en"}]},"item_type_id":"5","owner":"1","path":["1560","1891"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"7748","relation_version_is_last":true,"title":["Design and control of approach trajectory by impulsive velocity change"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T07:34:40.521207+00:00"}