WEKO3
アイテム
{"_buckets": {"deposit": "31549ab9-b816-44fb-ba0a-b756acb2dc2d"}, "_deposit": {"created_by": 1, "id": "22707", "owners": [1], "pid": {"revision_id": 0, "type": "depid", "value": "22707"}, "status": "published"}, "_oai": {"id": "oai:jaxa.repo.nii.ac.jp:00022707", "sets": ["1888"]}, "author_link": ["213085", "213084", "213089", "213088", "213090", "213086", "213083", "213087"], "item_7_biblio_info_10": {"attribute_name": "書誌情報", "attribute_value_mlt": [{"bibliographicIssueDates": {"bibliographicIssueDate": "2016-07-29", "bibliographicIssueDateType": "Issued"}, "bibliographicIssueNumber": "ists30", "bibliographicPageEnd": "Pd_13", "bibliographicPageStart": "Pd_7", "bibliographicVolumeNumber": "14", "bibliographic_titles": [{}, {"bibliographic_title": "Transactions of the Japan Society for Aeronautical and Space Sciences, Aerospace Technology Japan", "bibliographic_titleLang": "en"}]}]}, "item_7_description_17": {"attribute_name": "抄録(英)", "attribute_value_mlt": [{"subitem_description": "This paper presents attitude maneuver demonstration tests using control moment gyroscopes mounted in a three-axis free dynamics simulator that provides an on-ground test environment of free rotational movement around three axes using the air-floating method. The issue of torque error between the torque command and the actual output torque is discussed in relation to the singularity-robust based steering law for spacecraft maneuvers. The torque error is analyzed using singular value decomposition to determine its magnitude and direction. Based on the analysis, feedback control and steering laws are proposed to reduce the torque error. Before conducting the maneuver demonstration test, a preliminary simulation is performed using a simplified dynamics model, control law, and steering law. The maneuver test results indicate that the dynamics simulator successfully accomplishes agile, large angle, and rest-to-rest multitarget maneuvers as well as precision pointing.", "subitem_description_type": "Other"}]}, "item_7_description_18": {"attribute_name": "内容記述", "attribute_value_mlt": [{"subitem_description": "形態: カラー図版あり", "subitem_description_type": "Other"}]}, "item_7_description_19": {"attribute_name": "内容記述(英)", "attribute_value_mlt": [{"subitem_description": "Physical characteristics: Original contains color illustrations", "subitem_description_type": "Other"}]}, "item_7_description_32": {"attribute_name": "資料番号", "attribute_value_mlt": [{"subitem_description": "資料番号: PA1610097000", "subitem_description_type": "Other"}]}, "item_7_publisher_8": {"attribute_name": "出版者", "attribute_value_mlt": [{"subitem_publisher": "日本航空宇宙学会 (JSASS)"}]}, "item_7_publisher_9": {"attribute_name": "出版者(英)", "attribute_value_mlt": [{"subitem_publisher": "Japan Society for Aeronautical and Space Sciences(JSASS)"}]}, "item_7_relation_25": {"attribute_name": "DOI", "attribute_value_mlt": [{"subitem_relation_name": [{"subitem_relation_name_text": "info:doi/10.2322/tastj.14.Pd_7"}], "subitem_relation_type_id": {"subitem_relation_type_id_text": "http://dx.doi.org/10.2322/tastj.14.Pd_7", "subitem_relation_type_select": "DOI"}}]}, "item_7_source_id_21": {"attribute_name": "ISSN", "attribute_value_mlt": [{"subitem_source_identifier": "1884-0485", "subitem_source_identifier_type": "ISSN"}]}, "item_7_text_35": {"attribute_name": "JAXAカテゴリ", "attribute_value_mlt": [{"subitem_text_value": "JAXAカテゴリ: 学術雑誌論文"}]}, "item_7_text_36": {"attribute_name": "JAXAカテゴリ2", "attribute_value_mlt": [{"subitem_text_value": "JAXAカテゴリ2: TP"}]}, "item_7_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: 10"}]}, "item_7_text_6": {"attribute_name": "著者所属", "attribute_value_mlt": [{"subitem_text_value": "宇宙航空研究開発機構(JAXA)"}, {"subitem_text_value": "宇宙航空研究開発機構(JAXA)"}, {"subitem_text_value": "三菱電機株式会社"}, {"subitem_text_value": "宇宙航空研究開発機構(JAXA)"}]}, "item_7_text_7": {"attribute_name": "著者所属(英)", "attribute_value_mlt": [{"subitem_text_language": "en", "subitem_text_value": "Japan Aerospace Exploration Agency (JAXA)"}, {"subitem_text_language": "en", "subitem_text_value": "Japan Aerospace Exploration Agency (JAXA)"}, {"subitem_text_language": "en", "subitem_text_value": "Mitsubishi Electric Corporation"}, {"subitem_text_language": "en", "subitem_text_value": "Japan Aerospace Exploration Agency (JAXA)"}]}, "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": "神澤, 拓也"}], "nameIdentifiers": [{"nameIdentifier": "213083", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "春木, 美鈴"}], "nameIdentifiers": [{"nameIdentifier": "213084", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "遠藤, 達也"}], "nameIdentifiers": [{"nameIdentifier": "213085", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "山中, 浩二"}], "nameIdentifiers": [{"nameIdentifier": "213086", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Kanzawa, Takuya", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "213087", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Haruki, Misuzu", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "213088", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Endo, Tatsuya", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "213089", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Yamanaka, Koji", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "213090", "nameIdentifierScheme": "WEKO"}]}]}, "item_keyword": {"attribute_name": "キーワード", "attribute_value_mlt": [{"subitem_subject": "Control Moment Gyroscopes", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "Dynamics Simulator", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "Maneuver", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "Agile", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "Torque Error", "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": "journal article", "resourceuri": "http://purl.org/coar/resource_type/c_6501"}]}, "item_title": "Attitude Maneuver Tests Using CMGs Mounted in a Three-Axis Free Dynamics Simulator", "item_titles": {"attribute_name": "タイトル", "attribute_value_mlt": [{"subitem_title": "Attitude Maneuver Tests Using CMGs Mounted in a Three-Axis Free Dynamics Simulator", "subitem_title_language": "en"}]}, "item_type_id": "7", "owner": "1", "path": ["1888"], "permalink_uri": "https://jaxa.repo.nii.ac.jp/records/22707", "pubdate": {"attribute_name": "公開日", "attribute_value": "2016-08-15"}, "publish_date": "2016-08-15", "publish_status": "0", "recid": "22707", "relation": {}, "relation_version_is_last": true, "title": ["Attitude Maneuver Tests Using CMGs Mounted in a Three-Axis Free Dynamics Simulator"], "weko_shared_id": -1}
Attitude Maneuver Tests Using CMGs Mounted in a Three-Axis Free Dynamics Simulator
https://jaxa.repo.nii.ac.jp/records/22707
https://jaxa.repo.nii.ac.jp/records/227078d50569c-925b-4985-9a3c-7e162764dfbe
Item type | 学術雑誌論文 / Journal Article(1) | |||||
---|---|---|---|---|---|---|
公開日 | 2016-08-15 | |||||
タイトル | ||||||
言語 | en | |||||
タイトル | Attitude Maneuver Tests Using CMGs Mounted in a Three-Axis Free Dynamics Simulator | |||||
言語 | ||||||
言語 | eng | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Control Moment Gyroscopes | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Dynamics Simulator | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Maneuver | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Agile | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Torque Error | |||||
資源タイプ | ||||||
資源タイプ識別子 | http://purl.org/coar/resource_type/c_6501 | |||||
資源タイプ | journal article | |||||
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 |
神澤, 拓也
× 神澤, 拓也× 春木, 美鈴× 遠藤, 達也× 山中, 浩二× Kanzawa, Takuya× Haruki, Misuzu× Endo, Tatsuya× Yamanaka, Koji |
|||||
著者所属 | ||||||
宇宙航空研究開発機構(JAXA) | ||||||
著者所属 | ||||||
宇宙航空研究開発機構(JAXA) | ||||||
著者所属 | ||||||
三菱電機株式会社 | ||||||
著者所属 | ||||||
宇宙航空研究開発機構(JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency (JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency (JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Mitsubishi Electric Corporation | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency (JAXA) | ||||||
出版者 | ||||||
出版者 | 日本航空宇宙学会 (JSASS) | |||||
出版者(英) | ||||||
出版者 | Japan Society for Aeronautical and Space Sciences(JSASS) | |||||
書誌情報 |
en : Transactions of the Japan Society for Aeronautical and Space Sciences, Aerospace Technology Japan 巻 14, 号 ists30, p. Pd_7-Pd_13, 発行日 2016-07-29 |
|||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | This paper presents attitude maneuver demonstration tests using control moment gyroscopes mounted in a three-axis free dynamics simulator that provides an on-ground test environment of free rotational movement around three axes using the air-floating method. The issue of torque error between the torque command and the actual output torque is discussed in relation to the singularity-robust based steering law for spacecraft maneuvers. The torque error is analyzed using singular value decomposition to determine its magnitude and direction. Based on the analysis, feedback control and steering laws are proposed to reduce the torque error. Before conducting the maneuver demonstration test, a preliminary simulation is performed using a simplified dynamics model, control law, and steering law. The maneuver test results indicate that the dynamics simulator successfully accomplishes agile, large angle, and rest-to-rest multitarget maneuvers as well as precision pointing. | |||||
内容記述 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 形態: カラー図版あり | |||||
内容記述(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Physical characteristics: Original contains color illustrations | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 1884-0485 | |||||
DOI | ||||||
識別子タイプ | DOI | |||||
関連識別子 | http://dx.doi.org/10.2322/tastj.14.Pd_7 | |||||
関連名称 | info:doi/10.2322/tastj.14.Pd_7 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: PA1610097000 |