WEKO3
アイテム
{"_buckets": {"deposit": "9dc961f2-e6ef-4b55-a6a8-22dfc4d546e7"}, "_deposit": {"created_by": 1, "id": "7480", "owners": [1], "pid": {"revision_id": 0, "type": "depid", "value": "7480"}, "status": "published"}, "_oai": {"id": "oai:jaxa.repo.nii.ac.jp:00007480", "sets": ["1556", "1891"]}, "author_link": ["39874", "39873", "39871", "39872"], "item_5_alternative_title_1": {"attribute_name": "その他のタイトル", "attribute_value_mlt": [{"subitem_alternative_title": "テザー長制御によるテザー衛星の軌道変換"}]}, "item_5_biblio_info_10": {"attribute_name": "書誌情報", "attribute_value_mlt": [{"bibliographicIssueDates": {"bibliographicIssueDate": "2008-03", "bibliographicIssueDateType": "Issued"}, "bibliographicPageEnd": "266", "bibliographicPageStart": "261", "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_16": {"attribute_name": "抄録", "attribute_value_mlt": [{"subitem_description": "本研究では、赤道面内におけるテザー衛星の軌道変換について研究する。非線形制御の手法を用いることにより、指定された軌道上位置でシステムの状態を所望の値にするテザー長の履歴を作成する方法を提案する。テザー長を制御することになるピッチ角運動量の制御、ピッチ角速度の制御、ピッチ角の制御、という3つのステップにより、1つの入力で3つの状態を制御する。提案する手法は、数値反復計算を必要としないだけでなく、テザー張力などの物理的拘束にも対応できる。また、システムの状態を正確に目標値に一致させることができる。", "subitem_description_type": "Abstract"}]}, "item_5_description_17": {"attribute_name": "抄録(英)", "attribute_value_mlt": [{"subitem_description": "This study discusses orbital transfer of a tethered satellite system in equatorial plane. By applying a nonlinear control method, this paper proposes a procedure to design a tether length profile which attains the designated states at a specified final position in orbit. The proposed procedure consisting of three steps adjusts the system\u0027s three states to the target values with one control input; control for the angular momentum of pitching motion, which leads to control of the tether length, control for the pitch angular rate, and control for the pitch angle. The proposed procedure does not require numerical iterations, and can cope with physical restrictions for the system, such as tether tension or the maximum tether length. Besides, the resulted final states are precisely coincident to the target values.", "subitem_description_type": "Other"}]}, "item_5_description_32": {"attribute_name": "資料番号", "attribute_value_mlt": [{"subitem_description": "資料番号: AA0063718043", "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"}]}, "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": "九州大学 大学院工学研究院"}, {"subitem_text_value": "九州大学 大学院工学府"}]}, "item_5_text_7": {"attribute_name": "著者所属(英)", "attribute_value_mlt": [{"subitem_text_language": "en", "subitem_text_value": "Kyushu University Faculty of Engineering"}, {"subitem_text_language": "en", "subitem_text_value": "Kyushu University Graduate School of Engineering"}]}, "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": "外本, 伸治"}], "nameIdentifiers": [{"nameIdentifier": "39871", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "柴田, 成豊"}], "nameIdentifiers": [{"nameIdentifier": "39872", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Hokamoto, Shinji", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "39873", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Shibata, Naritoyo", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "39874", "nameIdentifierScheme": "WEKO"}]}]}, "item_keyword": {"attribute_name": "キーワード", "attribute_value_mlt": [{"subitem_subject": "テザー衛星", "subitem_subject_scheme": "Other"}, {"subitem_subject": "軌道遷移", "subitem_subject_scheme": "Other"}, {"subitem_subject": "角運動量", "subitem_subject_scheme": "Other"}, {"subitem_subject": "角速度", "subitem_subject_scheme": "Other"}, {"subitem_subject": "離心率", "subitem_subject_scheme": "Other"}, {"subitem_subject": "テザー線", "subitem_subject_scheme": "Other"}, {"subitem_subject": "衛星軌道", "subitem_subject_scheme": "Other"}, {"subitem_subject": "制御理論", "subitem_subject_scheme": "Other"}, {"subitem_subject": "シミュレーション", "subitem_subject_scheme": "Other"}, {"subitem_subject": "テザー長制御", "subitem_subject_scheme": "Other"}, {"subitem_subject": "テザー張力", "subitem_subject_scheme": "Other"}, {"subitem_subject": "制御入力", "subitem_subject_scheme": "Other"}, {"subitem_subject": "tethered satellite", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "orbital transfer", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "angular momentum", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "angular velocity", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "eccentricity", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "tetherline", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "satellite orbit", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "control theory", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "simulation", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "tether length control", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "tether tension", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "control input", "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": "Tether length control for orbital transfer of tethered satellite", "item_titles": {"attribute_name": "タイトル", "attribute_value_mlt": [{"subitem_title": "Tether length control for orbital transfer of tethered satellite", "subitem_title_language": "en"}]}, "item_type_id": "5", "owner": "1", "path": ["1556", "1891"], "permalink_uri": "https://jaxa.repo.nii.ac.jp/records/7480", "pubdate": {"attribute_name": "公開日", "attribute_value": "2015-03-26"}, "publish_date": "2015-03-26", "publish_status": "0", "recid": "7480", "relation": {}, "relation_version_is_last": true, "title": ["Tether length control for orbital transfer of tethered satellite"], "weko_shared_id": -1}
Tether length control for orbital transfer of tethered satellite
https://jaxa.repo.nii.ac.jp/records/7480
https://jaxa.repo.nii.ac.jp/records/748068c229ee-c727-4635-beeb-aa7f13cf01e2
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 | Tether length control for orbital transfer of tethered satellite | |||||
言語 | ||||||
言語 | eng | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | テザー衛星 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 軌道遷移 | |||||
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 | 角速度 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 離心率 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | テザー線 | |||||
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 | 制御理論 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | シミュレーション | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | テザー長制御 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | テザー張力 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 制御入力 | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | tethered satellite | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | orbital transfer | |||||
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 | angular velocity | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | eccentricity | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | tetherline | |||||
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 | control theory | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | simulation | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | tether length control | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | tether tension | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | control input | |||||
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 | テザー長制御によるテザー衛星の軌道変換 | |||||
著者 |
外本, 伸治
× 外本, 伸治× 柴田, 成豊× Hokamoto, Shinji× Shibata, Naritoyo |
|||||
著者所属 | ||||||
九州大学 大学院工学研究院 | ||||||
著者所属 | ||||||
九州大学 大学院工学府 | ||||||
著者所属(英) | ||||||
en | ||||||
Kyushu University Faculty of Engineering | ||||||
著者所属(英) | ||||||
en | ||||||
Kyushu University Graduate School of Engineering | ||||||
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. 261-266, 発行日 2008-03 |
|||||
抄録 | ||||||
内容記述タイプ | Abstract | |||||
内容記述 | 本研究では、赤道面内におけるテザー衛星の軌道変換について研究する。非線形制御の手法を用いることにより、指定された軌道上位置でシステムの状態を所望の値にするテザー長の履歴を作成する方法を提案する。テザー長を制御することになるピッチ角運動量の制御、ピッチ角速度の制御、ピッチ角の制御、という3つのステップにより、1つの入力で3つの状態を制御する。提案する手法は、数値反復計算を必要としないだけでなく、テザー張力などの物理的拘束にも対応できる。また、システムの状態を正確に目標値に一致させることができる。 | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | This study discusses orbital transfer of a tethered satellite system in equatorial plane. By applying a nonlinear control method, this paper proposes a procedure to design a tether length profile which attains the designated states at a specified final position in orbit. The proposed procedure consisting of three steps adjusts the system's three states to the target values with one control input; control for the angular momentum of pitching motion, which leads to control of the tether length, control for the pitch angular rate, and control for the pitch angle. The proposed procedure does not require numerical iterations, and can cope with physical restrictions for the system, such as tether tension or the maximum tether length. Besides, the resulted final states are precisely coincident to the target values. | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA0063718043 |