WEKO3
アイテム
{"_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": ["1559", "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_20": {"attribute_name": "その他キーワード", "attribute_value_mlt": [{"subitem_text_value": "宇宙力学"}, {"subitem_text_value": "機械工学"}]}, "item_5_text_35": {"attribute_name": "JAXAカテゴリ", "attribute_value_mlt": [{"subitem_text_value": "JAXAカテゴリ: シンポジウム・研究会"}]}, "item_5_text_36": {"attribute_name": "JAXAカテゴリ2", "attribute_value_mlt": [{"subitem_text_value": "JAXAカテゴリ2: IS"}]}, "item_5_text_42": {"attribute_name": "シンポジウム区分", "attribute_value_mlt": [{"subitem_text_value": "シンポジウム区分: 001"}]}, "item_5_text_43": {"attribute_name": "DSpaceコレクション番号", "attribute_value_mlt": [{"subitem_text_value": "DSpaceコレクション番号: 7"}]}, "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": [{"nameIdentifier": "41059", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "斎藤, 徹"}], "nameIdentifiers": [{"nameIdentifier": "41060", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "前田, 健"}], "nameIdentifiers": [{"nameIdentifier": "41061", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "橋本, 樹明"}], "nameIdentifiers": [{"nameIdentifier": "41062", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Horike, Naoko", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "41063", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Saito, Tetsu", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "41064", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Maeda, Ken", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "41065", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Hashimoto, Tatsuaki", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "41066", "nameIdentifierScheme": "WEKO"}]}]}, "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"], "permalink_uri": "https://jaxa.repo.nii.ac.jp/records/7662", "pubdate": {"attribute_name": "公開日", "attribute_value": "2015-03-26"}, "publish_date": "2015-03-26", "publish_status": "0", "recid": "7662", "relation": {}, "relation_version_is_last": true, "title": ["In-flight estimation method of a satellite moment of inertia"], "weko_shared_id": -1}
In-flight estimation method of a satellite moment of inertia
https://jaxa.repo.nii.ac.jp/records/7662
https://jaxa.repo.nii.ac.jp/records/766271ef6e40-d7c0-446a-ad30-99b33f7dffee
Item type | 会議発表論文 / Conference Paper(1) | |||||
---|---|---|---|---|---|---|
公開日 | 2015-03-26 | |||||
タイトル | ||||||
言語 | en | |||||
タイトル | In-flight estimation method of a satellite moment of inertia | |||||
言語 | ||||||
言語 | eng | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 軌道上推定法 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 衛星慣性モーメント | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 飛行条件 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | X線検出器 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 姿勢制御 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 角運動量 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 保存則 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 極低温装置 | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | in-flight estimation method | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | satellite moment of inertia | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | flight condition | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | X-ray detector | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | attitude control | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | angular momentum | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | conservation law | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | cryogenic equipment | |||||
資源タイプ | ||||||
資源タイプ識別子 | http://purl.org/coar/resource_type/c_5794 | |||||
資源タイプ | conference paper | |||||
アクセス権 | ||||||
アクセス権 | metadata only access | |||||
アクセス権URI | http://purl.org/coar/access_right/c_14cb | |||||
その他のタイトル | ||||||
その他のタイトル | 衛星慣性モーメントの軌道上推定 | |||||
著者 |
堀家, 尚子
× 堀家, 尚子× 斎藤, 徹× 前田, 健× 橋本, 樹明× Horike, Naoko× Saito, Tetsu× Maeda, Ken× Hashimoto, Tatsuaki |
|||||
著者所属 | ||||||
日本電気航空宇宙システム | ||||||
著者所属 | ||||||
日本電気航空宇宙システム | ||||||
著者所属 | ||||||
NEC東芝スペースシステム | ||||||
著者所属 | ||||||
宇宙航空研究開発機構 宇宙科学研究本部 | ||||||
著者所属(英) | ||||||
en | ||||||
NEC Aerospace Systems Ltd. | ||||||
著者所属(英) | ||||||
en | ||||||
NEC Aerospace Systems Ltd. | ||||||
著者所属(英) | ||||||
en | ||||||
NEC TOSHIBA Space Systems Ltd. | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency Institute of Space and Astronautical Science | ||||||
出版者 | ||||||
出版者 | 宇宙航空研究開発機構宇宙科学研究本部 | |||||
出版者(英) | ||||||
出版者 | Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA/ISAS) | |||||
書誌情報 |
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 en : ISAS proceedings of 14th Workshop on Astrodynamics and Flight Mechanics 2004: A Collection of Technical Papers p. 164-169, 発行日 2005-03 |
|||||
抄録 | ||||||
内容記述タイプ | Abstract | |||||
内容記述 | 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。 | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | 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. | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 0918-8053 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA0047897029 |