WEKO3
アイテム
{"_buckets": {"deposit": "af12b116-4298-4166-9170-1fdd56bbb22f"}, "_deposit": {"created_by": 1, "id": "7468", "owners": [1], "pid": {"revision_id": 0, "type": "depid", "value": "7468"}, "status": "published"}, "_oai": {"id": "oai:jaxa.repo.nii.ac.jp:00007468", "sets": ["1556", "1891"]}, "author_link": ["39786", "39779", "39780", "39788", "39782", "39785", "39783", "39784", "39787", "39781"], "item_5_biblio_info_10": {"attribute_name": "書誌情報", "attribute_value_mlt": [{"bibliographicIssueDates": {"bibliographicIssueDate": "2008-03", "bibliographicIssueDateType": "Issued"}, "bibliographicPageEnd": "193", "bibliographicPageStart": "190", "bibliographic_titles": [{"bibliographic_title": "第17回アストロダイナミクスシンポジウム講演後刷り集 2007"}, {"bibliographic_title": "Proceedings of 17th Workshop on JAXA Astrodynamics and Flight Mechanics", "bibliographic_titleLang": "en"}]}]}, "item_5_description_17": {"attribute_name": "抄録(英)", "attribute_value_mlt": [{"subitem_description": "Here at L2, introduced a satellite formation flying consists of two satellites powered by solar sail, the Mirror SpaceCraft (MSC) and the Detector SpaceCraft (DSC). The two satellites are separated such that the operational detector is at the focus of the mirror. Due to the instability of the collinear Lagrangian points, the desired distance between the two satellites need to be maintained. This paper addresses the control design scheme for formation keeping control. The equation of motion is derived in Hill\u0027s frame and inertial frame and then control law formulated mathematically. Halo and Lissajous orbit are considered as options for reference orbit.", "subitem_description_type": "Other"}]}, "item_5_description_32": {"attribute_name": "資料番号", "attribute_value_mlt": [{"subitem_description": "資料番号: AA0063718031", "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_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": "宇宙力学"}, {"subitem_text_value": "宇宙船の推進及び出力"}]}, "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": "東京大学 大学院工学系研究科"}, {"subitem_text_value": "宇宙航空研究開発機構 宇宙科学研究本部"}, {"subitem_text_value": "宇宙航空研究開発機構 宇宙科学研究本部"}, {"subitem_text_value": "東京大学 大学院工学系研究科"}, {"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": "University of Tokyo School of Engineering"}, {"subitem_text_language": "en", "subitem_text_value": "Japan Aerospace Exploration Agency Institute of Space and Astronautical Science"}, {"subitem_text_language": "en", "subitem_text_value": "Japan Aerospace Exploration Agency Institute of Space and Astronautical Science"}, {"subitem_text_language": "en", "subitem_text_value": "University of Tokyo School of Engineering"}, {"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": "Simanjuntak, Triwanto"}], "nameIdentifiers": [{"nameIdentifier": "39779", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "津田, 雄一"}], "nameIdentifiers": [{"nameIdentifier": "39780", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "森本, 睦子"}], "nameIdentifiers": [{"nameIdentifier": "39781", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "川口, 淳一郎"}], "nameIdentifiers": [{"nameIdentifier": "39782", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "澤田, 弘崇"}], "nameIdentifiers": [{"nameIdentifier": "39783", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Simanjuntak, Triwanto", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "39784", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Tsuda, Yuichi", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "39785", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Morimoto, Mutsuko Y.", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "39786", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Kawaguchi, Junichiro", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "39787", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Sawada, Hirotaka", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "39788", "nameIdentifierScheme": "WEKO"}]}]}, "item_keyword": {"attribute_name": "キーワード", "attribute_value_mlt": [{"subitem_subject": "編隊飛行", "subitem_subject_scheme": "Other"}, {"subitem_subject": "ソーラーセイル", "subitem_subject_scheme": "Other"}, {"subitem_subject": "位置保持", "subitem_subject_scheme": "Other"}, {"subitem_subject": "3体問題", "subitem_subject_scheme": "Other"}, {"subitem_subject": "ミラー宇宙機", "subitem_subject_scheme": "Other"}, {"subitem_subject": "MSC", "subitem_subject_scheme": "Other"}, {"subitem_subject": "ディテクタ宇宙機", "subitem_subject_scheme": "Other"}, {"subitem_subject": "DSC", "subitem_subject_scheme": "Other"}, {"subitem_subject": "ラグランジュ平衡点", "subitem_subject_scheme": "Other"}, {"subitem_subject": "制御理論", "subitem_subject_scheme": "Other"}, {"subitem_subject": "運動方程式", "subitem_subject_scheme": "Other"}, {"subitem_subject": "数学モデル", "subitem_subject_scheme": "Other"}, {"subitem_subject": "衛星軌道", "subitem_subject_scheme": "Other"}, {"subitem_subject": "リブレーション", "subitem_subject_scheme": "Other"}, {"subitem_subject": "formation flying", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "solar sail", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "stationkeeping", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "three body problem", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "Mirror Spacecraft", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "MSC", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "Detector Spacecraft", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "DSC", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "Lagrangian equilibrium point", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "control theory", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "equation of motion", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "mathematical model", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "satellite orbit", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "libration", "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": "Preliminary study on satellite formation flying control around L(sub 2) using solar sail propulsion", "item_titles": {"attribute_name": "タイトル", "attribute_value_mlt": [{"subitem_title": "Preliminary study on satellite formation flying control around L(sub 2) using solar sail propulsion", "subitem_title_language": "en"}]}, "item_type_id": "5", "owner": "1", "path": ["1556", "1891"], "permalink_uri": "https://jaxa.repo.nii.ac.jp/records/7468", "pubdate": {"attribute_name": "公開日", "attribute_value": "2015-03-26"}, "publish_date": "2015-03-26", "publish_status": "0", "recid": "7468", "relation": {}, "relation_version_is_last": true, "title": ["Preliminary study on satellite formation flying control around L(sub 2) using solar sail propulsion"], "weko_shared_id": -1}
Preliminary study on satellite formation flying control around L(sub 2) using solar sail propulsion
https://jaxa.repo.nii.ac.jp/records/7468
https://jaxa.repo.nii.ac.jp/records/7468f03c2acc-e2c0-4759-bafc-208bc67bd8a1
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 | Preliminary study on satellite formation flying control around L(sub 2) using solar sail propulsion | |||||
言語 | ||||||
言語 | eng | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 編隊飛行 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | ソーラーセイル | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 位置保持 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 3体問題 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | ミラー宇宙機 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | MSC | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | ディテクタ宇宙機 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | DSC | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | ラグランジュ平衡点 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 制御理論 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 運動方程式 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 数学モデル | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 衛星軌道 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | リブレーション | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | formation flying | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | solar sail | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | stationkeeping | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | three body problem | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Mirror Spacecraft | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | MSC | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Detector Spacecraft | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | DSC | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Lagrangian equilibrium point | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | control theory | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | equation of motion | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | mathematical model | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | satellite orbit | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | libration | |||||
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 | |||||
著者 |
Simanjuntak, Triwanto
× Simanjuntak, Triwanto× 津田, 雄一× 森本, 睦子× 川口, 淳一郎× 澤田, 弘崇× Simanjuntak, Triwanto× Tsuda, Yuichi× Morimoto, Mutsuko Y.× Kawaguchi, Junichiro× Sawada, Hirotaka |
|||||
著者所属 | ||||||
東京大学 大学院工学系研究科 | ||||||
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 | ||||||
宇宙航空研究開発機構 宇宙科学研究本部 | ||||||
著者所属 | ||||||
東京大学 大学院工学系研究科 | ||||||
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 | ||||||
University of Tokyo School of Engineering | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency Institute of Space and Astronautical Science | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency Institute of Space and Astronautical Science | ||||||
著者所属(英) | ||||||
en | ||||||
University of Tokyo School of Engineering | ||||||
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 |
第17回アストロダイナミクスシンポジウム講演後刷り集 2007 en : Proceedings of 17th Workshop on JAXA Astrodynamics and Flight Mechanics p. 190-193, 発行日 2008-03 |
|||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Here at L2, introduced a satellite formation flying consists of two satellites powered by solar sail, the Mirror SpaceCraft (MSC) and the Detector SpaceCraft (DSC). The two satellites are separated such that the operational detector is at the focus of the mirror. Due to the instability of the collinear Lagrangian points, the desired distance between the two satellites need to be maintained. This paper addresses the control design scheme for formation keeping control. The equation of motion is derived in Hill's frame and inertial frame and then control law formulated mathematically. Halo and Lissajous orbit are considered as options for reference orbit. | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA0063718031 |