WEKO3
アイテム
{"_buckets": {"deposit": "252edf4e-6a5a-4a4d-bd77-7eb0d8f3ebef"}, "_deposit": {"created_by": 1, "id": "6065", "owners": [1], "pid": {"revision_id": 0, "type": "depid", "value": "6065"}, "status": "published"}, "_oai": {"id": "oai:jaxa.repo.nii.ac.jp:00006065", "sets": ["1028", "1893"]}, "author_link": ["30243", "30244"], "item_3_alternative_title_2": {"attribute_name": "その他のタイトル(英)", "attribute_value_mlt": [{"subitem_alternative_title": "ALOS precision attitude and orbit control system: On-orbit capability and performance"}]}, "item_3_biblio_info_10": {"attribute_name": "書誌情報", "attribute_value_mlt": [{"bibliographicIssueDates": {"bibliographicIssueDate": "2006-11-01", "bibliographicIssueDateType": "Issued"}, "bibliographicPageEnd": "390", "bibliographicPageStart": "385", "bibliographicVolumeNumber": "JAXA-SP-06-006", "bibliographic_titles": [{"bibliographic_title": "宇宙航空研究開発機構特別資料: 平成18年度 宇宙航空研究開発機構 総合技術研究本部 宇宙科学研究本部 研究成果報告書"}, {"bibliographic_title": "JAXA Special Publication: Report on Research Achievements for FY2006 Institute of Space and Astronautical Science, Institute of Aerospace Technology, Japan Aerospace Exploration Agency", "bibliographic_titleLang": "en"}]}]}, "item_3_description_17": {"attribute_name": "抄録(英)", "attribute_value_mlt": [{"subitem_description": "The Advanced Land Observing Satellite (ALOS) was launched on January 24, 2006. It has been operated successfully since then. Upon its development, ALOS is required to attain stringent attitude performances for providing precise geometric accuracy to high-resolution images. For achieving these requirements, a variety of technologies, including precision star tracker, high-performance computer, star-sensor based attitude determination and control, were developed and implemented to the ALOS\u0027s attitude and orbit control system. Since the launch, capabilities and performances of the attitude and orbit control system have been assessed and verified on orbit. This report presents the review of these technologies and the analyses of their flight results.", "subitem_description_type": "Other"}]}, "item_3_description_32": {"attribute_name": "資料番号", "attribute_value_mlt": [{"subitem_description": "資料番号: AA0049500081", "subitem_description_type": "Other"}]}, "item_3_description_33": {"attribute_name": "レポート番号", "attribute_value_mlt": [{"subitem_description": "レポート番号: JAXA-SP-06-006", "subitem_description_type": "Other"}]}, "item_3_publisher_8": {"attribute_name": "出版者", "attribute_value_mlt": [{"subitem_publisher": "宇宙航空研究開発機構"}]}, "item_3_publisher_9": {"attribute_name": "出版者(英)", "attribute_value_mlt": [{"subitem_publisher": "Japan Aerospace Exploration Agency (JAXA)"}]}, "item_3_source_id_21": {"attribute_name": "ISSN", "attribute_value_mlt": [{"subitem_source_identifier": "1349-113X", "subitem_source_identifier_type": "ISSN"}]}, "item_3_source_id_24": {"attribute_name": "書誌レコードID", "attribute_value_mlt": [{"subitem_source_identifier": "AA11984031", "subitem_source_identifier_type": "NCID"}]}, "item_3_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"}]}, "item_3_text_35": {"attribute_name": "JAXAカテゴリ", "attribute_value_mlt": [{"subitem_text_value": "JAXAカテゴリ: 特別資料"}]}, "item_3_text_40": {"attribute_name": "jaxa出版物種類", "attribute_value_mlt": [{"subitem_text_value": "jaxa出版物種類: SP"}]}, "item_3_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_3_text_6": {"attribute_name": "著者所属", "attribute_value_mlt": [{"subitem_text_value": "宇宙航空研究開発機構 総合技術研究本部"}]}, "item_3_text_7": {"attribute_name": "著者所属(英)", "attribute_value_mlt": [{"subitem_text_language": "en", "subitem_text_value": "Japan Aerospace Exploration Agency Institute of Aerospace Technology"}]}, "item_creator": {"attribute_name": "著者", "attribute_type": "creator", "attribute_value_mlt": [{"creatorNames": [{"creatorName": "岩田, 隆敬"}], "nameIdentifiers": [{"nameIdentifier": "30243", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Iwata, Takanori", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "30244", "nameIdentifierScheme": "WEKO"}]}]}, "item_files": {"attribute_name": "ファイル情報", "attribute_type": "file", "attribute_value_mlt": [{"accessrole": "open_date", "date": [{"dateType": "Available", "dateValue": "2020-01-16"}], "displaytype": "detail", "download_preview_message": "", "file_order": 0, "filename": "49500081.pdf", "filesize": [{"value": "838.7 kB"}], "format": "application/pdf", "future_date_message": "", "is_thumbnail": false, "licensetype": "license_free", "mimetype": "application/pdf", "size": 838700.0, "url": {"label": "49500081.pdf", "url": "https://jaxa.repo.nii.ac.jp/record/6065/files/49500081.pdf"}, "version_id": "539b4079-641b-4a29-b236-8e95aa138adf"}]}, "item_keyword": {"attribute_name": "キーワード", "attribute_value_mlt": [{"subitem_subject": "だいち", "subitem_subject_scheme": "Other"}, {"subitem_subject": "陸域観測技術衛星", "subitem_subject_scheme": "Other"}, {"subitem_subject": "地球観測", "subitem_subject_scheme": "Other"}, {"subitem_subject": "衛星姿勢制御", "subitem_subject_scheme": "Other"}, {"subitem_subject": "姿勢安定性", "subitem_subject_scheme": "Other"}, {"subitem_subject": "高分解能", "subitem_subject_scheme": "Other"}, {"subitem_subject": "スタートラッカ", "subitem_subject_scheme": "Other"}, {"subitem_subject": "精度", "subitem_subject_scheme": "Other"}, {"subitem_subject": "姿勢軌道制御系", "subitem_subject_scheme": "Other"}, {"subitem_subject": "ALOS", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "Advanced Land Observing Satellite", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "Earth observation", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "satellite attitude control", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "attitude stability", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "high resolution", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "star tracker", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "accuracy", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "attitude and orbit control system", "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": "technical report", "resourceuri": "http://purl.org/coar/resource_type/c_18gh"}]}, "item_title": "ALOS高精度姿勢軌道制御系の軌道上評価", "item_titles": {"attribute_name": "タイトル", "attribute_value_mlt": [{"subitem_title": "ALOS高精度姿勢軌道制御系の軌道上評価"}]}, "item_type_id": "3", "owner": "1", "path": ["1028", "1893"], "permalink_uri": "https://jaxa.repo.nii.ac.jp/records/6065", "pubdate": {"attribute_name": "公開日", "attribute_value": "2015-03-26"}, "publish_date": "2015-03-26", "publish_status": "0", "recid": "6065", "relation": {}, "relation_version_is_last": true, "title": ["ALOS高精度姿勢軌道制御系の軌道上評価"], "weko_shared_id": -1}
ALOS高精度姿勢軌道制御系の軌道上評価
https://jaxa.repo.nii.ac.jp/records/6065
https://jaxa.repo.nii.ac.jp/records/606555b5dfd1-9c83-4103-bf32-95814e6784d9
名前 / ファイル | ライセンス | アクション |
---|---|---|
49500081.pdf (838.7 kB)
|
|
Item type | テクニカルレポート / Technical Report(1) | |||||
---|---|---|---|---|---|---|
公開日 | 2015-03-26 | |||||
タイトル | ||||||
タイトル | ALOS高精度姿勢軌道制御系の軌道上評価 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | だいち | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 陸域観測技術衛星 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 地球観測 | |||||
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 | 姿勢安定性 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 高分解能 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | スタートラッカ | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 精度 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 姿勢軌道制御系 | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | ALOS | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Advanced Land Observing Satellite | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Earth observation | |||||
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 | attitude stability | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | high resolution | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | star tracker | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | accuracy | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | attitude and orbit control system | |||||
資源タイプ | ||||||
資源タイプ識別子 | http://purl.org/coar/resource_type/c_18gh | |||||
資源タイプ | technical report | |||||
その他のタイトル(英) | ||||||
その他のタイトル | ALOS precision attitude and orbit control system: On-orbit capability and performance | |||||
著者 |
岩田, 隆敬
× 岩田, 隆敬× Iwata, Takanori |
|||||
著者所属 | ||||||
宇宙航空研究開発機構 総合技術研究本部 | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency Institute of Aerospace Technology | ||||||
出版者 | ||||||
出版者 | 宇宙航空研究開発機構 | |||||
出版者(英) | ||||||
出版者 | Japan Aerospace Exploration Agency (JAXA) | |||||
書誌情報 |
宇宙航空研究開発機構特別資料: 平成18年度 宇宙航空研究開発機構 総合技術研究本部 宇宙科学研究本部 研究成果報告書 en : JAXA Special Publication: Report on Research Achievements for FY2006 Institute of Space and Astronautical Science, Institute of Aerospace Technology, Japan Aerospace Exploration Agency 巻 JAXA-SP-06-006, p. 385-390, 発行日 2006-11-01 |
|||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | The Advanced Land Observing Satellite (ALOS) was launched on January 24, 2006. It has been operated successfully since then. Upon its development, ALOS is required to attain stringent attitude performances for providing precise geometric accuracy to high-resolution images. For achieving these requirements, a variety of technologies, including precision star tracker, high-performance computer, star-sensor based attitude determination and control, were developed and implemented to the ALOS's attitude and orbit control system. Since the launch, capabilities and performances of the attitude and orbit control system have been assessed and verified on orbit. This report presents the review of these technologies and the analyses of their flight results. | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 1349-113X | |||||
書誌レコードID | ||||||
収録物識別子タイプ | NCID | |||||
収録物識別子 | AA11984031 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA0049500081 | |||||
レポート番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | レポート番号: JAXA-SP-06-006 |