WEKO3
アイテム
{"_buckets": {"deposit": "fc99eed8-d3ae-4cfc-85c5-e9e001f478cb"}, "_deposit": {"created_by": 1, "id": "8035", "owners": [1], "pid": {"revision_id": 0, "type": "depid", "value": "8035"}, "status": "published"}, "_oai": {"id": "oai:jaxa.repo.nii.ac.jp:00008035", "sets": ["1574", "1891"]}, "author_link": ["44047", "44041", "44038", "44039", "44043", "44045", "44046", "44049", "44042", "44040", "44044", "44048"], "item_5_alternative_title_2": {"attribute_name": "その他のタイトル(英)", "attribute_value_mlt": [{"subitem_alternative_title": "Experimental study of vibration control by minute tension actuator to flexible space structure"}]}, "item_5_biblio_info_10": {"attribute_name": "書誌情報", "attribute_value_mlt": [{"bibliographicIssueDates": {"bibliographicIssueDate": "2008-05", "bibliographicIssueDateType": "Issued"}, "bibliographicPageEnd": "111", "bibliographicPageStart": "107", "bibliographic_titles": [{"bibliographic_title": "第27回宇宙エネルギーシンポジウム 平成19年度"}, {"bibliographic_title": "The Twenty-seventh Space Energy Symposium", "bibliographic_titleLang": "en"}]}]}, "item_5_description_17": {"attribute_name": "抄録(英)", "attribute_value_mlt": [{"subitem_description": "In this paper, the effectiveness of vibration control is examined by employing tether on the flexible space structures like SSPS (Space Solar Power System). The vibration control is analyzed numerically to simulate the behavior of flexible space structure in a flexible panel-tether system with mathematical description in the partial differential equation, and the effectiveness is shown for the tether tension control. Vibration control experiment is also examined on an experiment model and the result is compared with that of numerical analysis. An actuator is analyzed in its performance to generate a very low tension employed for the experiment of vibration control experiment of this model. It aimed to make a numeric model about the actuator used when the vibration was controlled, to compare with an actual performance, and to optimize it to the control experiment.", "subitem_description_type": "Other"}]}, "item_5_description_32": {"attribute_name": "資料番号", "attribute_value_mlt": [{"subitem_description": "資料番号: AA0063965022", "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": "機械工学"}, {"subitem_text_value": "電子及び電気工学"}, {"subitem_text_value": "宇宙船設計、試験及び性能"}]}, "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: 002"}]}, "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": "首都大学東京"}, {"subitem_text_value": "首都大学東京"}, {"subitem_text_value": "首都大学東京"}, {"subitem_text_value": "首都大学東京"}, {"subitem_text_value": "首都大学東京"}, {"subitem_text_value": "東京都立科学技術大学"}]}, "item_5_text_7": {"attribute_name": "著者所属(英)", "attribute_value_mlt": [{"subitem_text_language": "en", "subitem_text_value": "Tokyo Metropolitan University"}, {"subitem_text_language": "en", "subitem_text_value": "Tokyo Metropolitan University"}, {"subitem_text_language": "en", "subitem_text_value": "Tokyo Metropolitan University"}, {"subitem_text_language": "en", "subitem_text_value": "Tokyo Metropolitan University"}, {"subitem_text_language": "en", "subitem_text_value": "Tokyo Metropolitan University"}, {"subitem_text_language": "en", "subitem_text_value": "Tokyo Metropolitan Institute of Technology"}]}, "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": "小島, 幸高"}], "nameIdentifiers": [{"nameIdentifier": "44038", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "藤井, 裕矩"}], "nameIdentifiers": [{"nameIdentifier": "44039", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "草谷, 大郎"}], "nameIdentifiers": [{"nameIdentifier": "44040", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "渡部, 武夫"}], "nameIdentifiers": [{"nameIdentifier": "44041", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "皆川, 洋平"}], "nameIdentifiers": [{"nameIdentifier": "44042", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "中野, 美琴"}], "nameIdentifiers": [{"nameIdentifier": "44043", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Kojima, Yukitaka", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "44044", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Fujii, Hironori A.", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "44045", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Kusagaya, Tairo", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "44046", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Watanabe, Takeo", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "44047", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Minagawa, Yohei", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "44048", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Nakano, Mikoto", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "44049", "nameIdentifierScheme": "WEKO"}]}]}, "item_keyword": {"attribute_name": "キーワード", "attribute_value_mlt": [{"subitem_subject": "太陽発電衛星", "subitem_subject_scheme": "Other"}, {"subitem_subject": "テザー衛星", "subitem_subject_scheme": "Other"}, {"subitem_subject": "マイクロ波パワービーミング", "subitem_subject_scheme": "Other"}, {"subitem_subject": "衛星姿勢制御", "subitem_subject_scheme": "Other"}, {"subitem_subject": "構造振動", "subitem_subject_scheme": "Other"}, {"subitem_subject": "大型宇宙構造物", "subitem_subject_scheme": "Other"}, {"subitem_subject": "柔軟宇宙機", "subitem_subject_scheme": "Other"}, {"subitem_subject": "振動減衰", "subitem_subject_scheme": "Other"}, {"subitem_subject": "アクチュエータ", "subitem_subject_scheme": "Other"}, {"subitem_subject": "solar power satellite", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "tethered satellite", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "microwave power beaming", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "satellite attitude control", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "structural vibration", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "large space structure", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "flexible spacecraft", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "vibration damping", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "actuator", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}]}, "item_language": {"attribute_name": "言語", "attribute_value_mlt": [{"subitem_language": "jpn"}]}, "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": "微小張力アクチュエータを用いた柔軟宇宙構造物の振動制御の実験的研究", "item_titles": {"attribute_name": "タイトル", "attribute_value_mlt": [{"subitem_title": "微小張力アクチュエータを用いた柔軟宇宙構造物の振動制御の実験的研究"}]}, "item_type_id": "5", "owner": "1", "path": ["1574", "1891"], "permalink_uri": "https://jaxa.repo.nii.ac.jp/records/8035", "pubdate": {"attribute_name": "公開日", "attribute_value": "2015-03-26"}, "publish_date": "2015-03-26", "publish_status": "0", "recid": "8035", "relation": {}, "relation_version_is_last": true, "title": ["微小張力アクチュエータを用いた柔軟宇宙構造物の振動制御の実験的研究"], "weko_shared_id": -1}
微小張力アクチュエータを用いた柔軟宇宙構造物の振動制御の実験的研究
https://jaxa.repo.nii.ac.jp/records/8035
https://jaxa.repo.nii.ac.jp/records/8035a4f45436-ee9b-47e6-a10c-0b35bd7e61d4
Item type | 会議発表論文 / Conference Paper(1) | |||||
---|---|---|---|---|---|---|
公開日 | 2015-03-26 | |||||
タイトル | ||||||
タイトル | 微小張力アクチュエータを用いた柔軟宇宙構造物の振動制御の実験的研究 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 太陽発電衛星 | |||||
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 | マイクロ波パワービーミング | |||||
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 | 構造振動 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 大型宇宙構造物 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 柔軟宇宙機 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 振動減衰 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | アクチュエータ | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | solar power satellite | |||||
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 | microwave power beaming | |||||
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 | structural vibration | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | large space structure | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | flexible spacecraft | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | vibration damping | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | actuator | |||||
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(英) | ||||||
その他のタイトル | Experimental study of vibration control by minute tension actuator to flexible space structure | |||||
著者 |
小島, 幸高
× 小島, 幸高× 藤井, 裕矩× 草谷, 大郎× 渡部, 武夫× 皆川, 洋平× 中野, 美琴× Kojima, Yukitaka× Fujii, Hironori A.× Kusagaya, Tairo× Watanabe, Takeo× Minagawa, Yohei× Nakano, Mikoto |
|||||
著者所属 | ||||||
首都大学東京 | ||||||
著者所属 | ||||||
首都大学東京 | ||||||
著者所属 | ||||||
首都大学東京 | ||||||
著者所属 | ||||||
首都大学東京 | ||||||
著者所属 | ||||||
首都大学東京 | ||||||
著者所属 | ||||||
東京都立科学技術大学 | ||||||
著者所属(英) | ||||||
en | ||||||
Tokyo Metropolitan University | ||||||
著者所属(英) | ||||||
en | ||||||
Tokyo Metropolitan University | ||||||
著者所属(英) | ||||||
en | ||||||
Tokyo Metropolitan University | ||||||
著者所属(英) | ||||||
en | ||||||
Tokyo Metropolitan University | ||||||
著者所属(英) | ||||||
en | ||||||
Tokyo Metropolitan University | ||||||
著者所属(英) | ||||||
en | ||||||
Tokyo Metropolitan Institute of Technology | ||||||
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27回宇宙エネルギーシンポジウム 平成19年度 en : The Twenty-seventh Space Energy Symposium p. 107-111, 発行日 2008-05 |
|||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | In this paper, the effectiveness of vibration control is examined by employing tether on the flexible space structures like SSPS (Space Solar Power System). The vibration control is analyzed numerically to simulate the behavior of flexible space structure in a flexible panel-tether system with mathematical description in the partial differential equation, and the effectiveness is shown for the tether tension control. Vibration control experiment is also examined on an experiment model and the result is compared with that of numerical analysis. An actuator is analyzed in its performance to generate a very low tension employed for the experiment of vibration control experiment of this model. It aimed to make a numeric model about the actuator used when the vibration was controlled, to compare with an actual performance, and to optimize it to the control experiment. | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA0063965022 |