WEKO3
アイテム
{"_buckets": {"deposit": "a7918b96-863a-47d8-96dd-63f5dda42973"}, "_deposit": {"created_by": 1, "id": "7802", "owners": [1], "pid": {"revision_id": 0, "type": "depid", "value": "7802"}, "status": "published"}, "_oai": {"id": "oai:jaxa.repo.nii.ac.jp:00007802", "sets": ["1561", "1891"]}, "author_link": ["41997", "41995", "41998", "41999", "41996", "42002", "42001", "42000"], "item_5_alternative_title_1": {"attribute_name": "その他のタイトル", "attribute_value_mlt": [{"subitem_alternative_title": "PLANET-C軌道制御時の3軸姿勢保持制御"}]}, "item_5_biblio_info_10": {"attribute_name": "書誌情報", "attribute_value_mlt": [{"bibliographicIssueDates": {"bibliographicIssueDate": "2003-02", "bibliographicIssueDateType": "Issued"}, "bibliographicPageEnd": "245", "bibliographicPageStart": "240", "bibliographic_titles": [{"bibliographic_title": "平成14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 12th Workshop on Astrodynamics and Flight Mechanics 2002: A Collection of Technical Papers", "bibliographic_titleLang": "en"}]}]}, "item_5_description_16": {"attribute_name": "抄録", "attribute_value_mlt": [{"subitem_description": "PLANET-Cは文部科学省宇宙科学研究所初の金星探査機である。PLANET-Cは3軸制御安定の小さな探査機であり500Nの軌道制御エンジン(OME)の発生する擾乱トルクが姿勢制御にとって大きな脅威となる。この擾乱トルクを抑制するため、外乱抑制制御策が比較検討された結果、新しいタイプの制御(トランジェント抑制制御)に問題解決の可能性があることが判った。", "subitem_description_type": "Abstract"}]}, "item_5_description_17": {"attribute_name": "抄録(英)", "attribute_value_mlt": [{"subitem_description": "PLANET-C is the ISAS\u0027s first VENUS probe. Since PLANET-C is a small three-axis-stabilized spacecraft, the disturbance torque due to 500N Orbit Maneuver Engine (OME) is a big threat for attitude control. In order to manage the disturbance, various disturbance suppression control schemes have been designed for comparison. A new class of scheme, transient suppression compensator, may overcome the problem.", "subitem_description_type": "Other"}]}, "item_5_description_32": {"attribute_name": "資料番号", "attribute_value_mlt": [{"subitem_description": "資料番号: AA0045497040", "subitem_description_type": "Other"}]}, "item_5_publisher_8": {"attribute_name": "出版者", "attribute_value_mlt": [{"subitem_publisher": "宇宙科学研究所"}]}, "item_5_publisher_9": {"attribute_name": "出版者(英)", "attribute_value_mlt": [{"subitem_publisher": "The Institute of Space and Astronautical Science (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": "宇宙船設計、試験及び性能"}, {"subitem_text_value": "宇宙船の推進及び出力"}, {"subitem_text_value": "宇宙力学"}]}, "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": "NEC東芝スペースシステム"}, {"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": "宇宙科学研究所"}]}, "item_5_text_7": {"attribute_name": "著者所属(英)", "attribute_value_mlt": [{"subitem_text_language": "en", "subitem_text_value": "NEC TOSHIBA Space Systems Ltd."}, {"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": "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": "栗井, 俊弘"}], "nameIdentifiers": [{"nameIdentifier": "41995", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "日高, 智成"}], "nameIdentifiers": [{"nameIdentifier": "41996", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "木村, 雅文"}], "nameIdentifiers": [{"nameIdentifier": "41997", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "橋本, 樹明"}], "nameIdentifiers": [{"nameIdentifier": "41998", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Kurii, Toshihiro", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "41999", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Hidaka, Tomonari", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "42000", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Kimura, Masafumi", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "42001", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Hashimoto, Tatsuaki", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "42002", "nameIdentifierScheme": "WEKO"}]}]}, "item_keyword": {"attribute_name": "キーワード", "attribute_value_mlt": [{"subitem_subject": "衛星姿勢制御", "subitem_subject_scheme": "Other"}, {"subitem_subject": "軌道投入操作", "subitem_subject_scheme": "Other"}, {"subitem_subject": "衛星姿勢撹乱", "subitem_subject_scheme": "Other"}, {"subitem_subject": "3軸安定化", "subitem_subject_scheme": "Other"}, {"subitem_subject": "宇宙探査", "subitem_subject_scheme": "Other"}, {"subitem_subject": "擾乱トルク", "subitem_subject_scheme": "Other"}, {"subitem_subject": "軌道操作エンジン", "subitem_subject_scheme": "Other"}, {"subitem_subject": "PLANET-C探査機", "subitem_subject_scheme": "Other"}, {"subitem_subject": "火星", "subitem_subject_scheme": "Other"}, {"subitem_subject": "satellite attitude control", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "orbit injection maneuver", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "satellite attitude disturbance", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "three-axis stabilization", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "space exploration", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "disturbance torque", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "orbit maneuver engine", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "PLANET-C prove", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "Mars", "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": "Attitude control during orbit injection maneuver for venus probe PLANET-C", "item_titles": {"attribute_name": "タイトル", "attribute_value_mlt": [{"subitem_title": "Attitude control during orbit injection maneuver for venus probe PLANET-C", "subitem_title_language": "en"}]}, "item_type_id": "5", "owner": "1", "path": ["1561", "1891"], "permalink_uri": "https://jaxa.repo.nii.ac.jp/records/7802", "pubdate": {"attribute_name": "公開日", "attribute_value": "2015-03-26"}, "publish_date": "2015-03-26", "publish_status": "0", "recid": "7802", "relation": {}, "relation_version_is_last": true, "title": ["Attitude control during orbit injection maneuver for venus probe PLANET-C"], "weko_shared_id": -1}
Attitude control during orbit injection maneuver for venus probe PLANET-C
https://jaxa.repo.nii.ac.jp/records/7802
https://jaxa.repo.nii.ac.jp/records/780267da03bb-34b5-42d1-95f6-b2de0411ec18
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 | Attitude control during orbit injection maneuver for venus probe PLANET-C | |||||
言語 | ||||||
言語 | eng | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 衛星姿勢制御 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 軌道投入操作 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 衛星姿勢撹乱 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 3軸安定化 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 宇宙探査 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 擾乱トルク | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 軌道操作エンジン | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | PLANET-C探査機 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 火星 | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | satellite attitude control | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | orbit injection maneuver | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | satellite attitude disturbance | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | three-axis stabilization | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | space exploration | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | disturbance torque | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | orbit maneuver engine | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | PLANET-C prove | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Mars | |||||
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 | PLANET-C軌道制御時の3軸姿勢保持制御 | |||||
著者 |
栗井, 俊弘
× 栗井, 俊弘× 日高, 智成× 木村, 雅文× 橋本, 樹明× Kurii, Toshihiro× Hidaka, Tomonari× Kimura, Masafumi× Hashimoto, Tatsuaki |
|||||
著者所属 | ||||||
NEC東芝スペースシステム | ||||||
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 | ||||||
宇宙科学研究所 | ||||||
著者所属(英) | ||||||
en | ||||||
NEC TOSHIBA Space Systems Ltd. | ||||||
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 | ||||||
Institute of Space and Astronautical Science | ||||||
出版者 | ||||||
出版者 | 宇宙科学研究所 | |||||
出版者(英) | ||||||
出版者 | The Institute of Space and Astronautical Science (ISAS) | |||||
書誌情報 |
平成14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 12th Workshop on Astrodynamics and Flight Mechanics 2002: A Collection of Technical Papers p. 240-245, 発行日 2003-02 |
|||||
抄録 | ||||||
内容記述タイプ | Abstract | |||||
内容記述 | PLANET-Cは文部科学省宇宙科学研究所初の金星探査機である。PLANET-Cは3軸制御安定の小さな探査機であり500Nの軌道制御エンジン(OME)の発生する擾乱トルクが姿勢制御にとって大きな脅威となる。この擾乱トルクを抑制するため、外乱抑制制御策が比較検討された結果、新しいタイプの制御(トランジェント抑制制御)に問題解決の可能性があることが判った。 | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | PLANET-C is the ISAS's first VENUS probe. Since PLANET-C is a small three-axis-stabilized spacecraft, the disturbance torque due to 500N Orbit Maneuver Engine (OME) is a big threat for attitude control. In order to manage the disturbance, various disturbance suppression control schemes have been designed for comparison. A new class of scheme, transient suppression compensator, may overcome the problem. | |||||
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: AA0045497040 |