{"created":"2023-06-20T14:40:44.216056+00:00","id":7662,"links":{},"metadata":{"_buckets":{"deposit":"2b2d7a5e-e92c-4107-86be-24ceecf2d59a"},"_deposit":{"created_by":1,"id":"7662","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"7662"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00007662","sets":["1543:1544:1559","1887:1891"]},"author_link":["41063","41062","41065","41064","41066","41059","41060","41061"],"item_5_alternative_title_1":{"attribute_name":"その他のタイトル","attribute_value_mlt":[{"subitem_alternative_title":"衛星慣性モーメントの軌道上推定"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2005-03","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"169","bibliographicPageStart":"164","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":"一般に、衛星慣性モーメント(MOI)は地上での開発試験フェーズで測定される。しかし、ASTRO-E2衛星のように、衛星に大量の冷媒を搭載している場合などにおいては、軌道上でMOIを測定する必要性がでてくる。本稿では、衛星の保有する角運動量の保存則を基本とし、軌道上の姿勢マヌーバ時に得られるテレメトリデータを用いてMOIを推定する。","subitem_description_type":"Abstract"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Usually, the satellite moment of inertia (MOI) is measured in the satellite system test on the ground. However, it is sometimes required to be estimated in flight condition. For example, ASTRO-E2 satellite has large amount of coolant for the X-ray detector and the coolant evaporates gradually, which causes the change of MOI. In this paper, an estimation scheme of a satellite MOI in-flight is introduced. The estimation scheme uses the satellite telemetry data during attitude maneuver and it is based on the conservation law of a satellite angular momentum.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0047897029","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":"日本電気航空宇宙システム"},{"subitem_text_value":"日本電気航空宇宙システム"},{"subitem_text_value":"NEC東芝スペースシステム"},{"subitem_text_value":"宇宙航空研究開発機構 宇宙科学研究本部"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"NEC Aerospace Systems Ltd."},{"subitem_text_language":"en","subitem_text_value":"NEC Aerospace Systems Ltd."},{"subitem_text_language":"en","subitem_text_value":"NEC TOSHIBA Space Systems Ltd."},{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency Institute of Space and Astronautical 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":"堀家, 尚子"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"斎藤, 徹"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"前田, 健"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"橋本, 樹明"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Horike, Naoko","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Saito, Tetsu","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Maeda, Ken","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Hashimoto, Tatsuaki","creatorNameLang":"en"}],"nameIdentifiers":[{}]}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"軌道上推定法","subitem_subject_scheme":"Other"},{"subitem_subject":"衛星慣性モーメント","subitem_subject_scheme":"Other"},{"subitem_subject":"飛行条件","subitem_subject_scheme":"Other"},{"subitem_subject":"X線検出器","subitem_subject_scheme":"Other"},{"subitem_subject":"姿勢制御","subitem_subject_scheme":"Other"},{"subitem_subject":"角運動量","subitem_subject_scheme":"Other"},{"subitem_subject":"保存則","subitem_subject_scheme":"Other"},{"subitem_subject":"極低温装置","subitem_subject_scheme":"Other"},{"subitem_subject":"in-flight estimation method","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"satellite moment of inertia","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"flight condition","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"X-ray detector","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"attitude control","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"angular momentum","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"conservation law","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"cryogenic equipment","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":"In-flight estimation method of a satellite moment of inertia","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"In-flight estimation method of a satellite moment of inertia","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":"7662","relation_version_is_last":true,"title":["In-flight estimation method of a satellite moment of inertia"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T07:36:01.560935+00:00"}