WEKO3
アイテム
{"_buckets": {"deposit": "43c47b37-8a4b-40b0-b5c8-9fe25d04203b"}, "_deposit": {"created_by": 1, "id": "45264", "owners": [1], "pid": {"revision_id": 0, "type": "depid", "value": "45264"}, "status": "published"}, "_oai": {"id": "oai:jaxa.repo.nii.ac.jp:00045264", "sets": ["1893", "1917"]}, "author_link": ["473796", "473799", "473797", "473798"], "item_3_alternative_title_2": {"attribute_name": "その他のタイトル(英)", "attribute_value_mlt": [{"subitem_alternative_title": "Study on a Highly Sensitive Electro-static Suspended Accelerometer (I)"}]}, "item_3_biblio_info_10": {"attribute_name": "書誌情報", "attribute_value_mlt": [{"bibliographicIssueDates": {"bibliographicIssueDate": "1988-10", "bibliographicIssueDateType": "Issued"}, "bibliographicPageStart": "15", "bibliographicVolumeNumber": "1005", "bibliographic_titles": [{"bibliographic_title": "航空宇宙技術研究所報告"}, {"bibliographic_title": "Technical Report of National Aerospace Laboratory TR-1005", "bibliographic_titleLang": "en"}]}]}, "item_3_description_17": {"attribute_name": "抄録(英)", "attribute_value_mlt": [{"subitem_description": "An artificial satellite in orbit is not free from accelerations due to external forces such as : (1)gravitational anomalies of the earth’s oblateness, (2)gravitational attractions of the sun and the moon, (3)pressure of solar wind, (4)aerodynamic drags. The accelerations are very small ; however, they disturb precise position keeping of a satellite, attitude control of a large space system and also micro-gravity experiments such as IML in the Space lab. A highly sensitive electro-static suspended accelerometer was studied to measure such disturbances. The device has a hollow vacuum vessel. A non-magnetic metal sphere is suspended at the center of the vessel by means of three-dimensional electro-static fields. A small displacement of the position of the sphere due to external forces induces un-balanced electro-static forces in the fields. The force difference is measured as an electrical output. This paper presents an analysis of the design of the accelerometer. A series of preliminary experiments has been carried out to confirm the analysis by developing a two-axis accelerometer. The experimental result shows good stability for 10(exp -7)g with a threshold at the 10(exp -8)g level.", "subitem_description_type": "Other"}]}, "item_3_description_32": {"attribute_name": "資料番号", "attribute_value_mlt": [{"subitem_description": "資料番号: NALTR1005000", "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: NAL TR-1005", "subitem_description_type": "Other"}]}, "item_3_publisher_8": {"attribute_name": "出版者", "attribute_value_mlt": [{"subitem_publisher": "航空宇宙技術研究所"}]}, "item_3_publisher_9": {"attribute_name": "出版者(英)", "attribute_value_mlt": [{"subitem_publisher": "National Aerospace Laboratory(NAL)"}]}, "item_3_source_id_21": {"attribute_name": "ISSN", "attribute_value_mlt": [{"subitem_source_identifier": "0389-4010", "subitem_source_identifier_type": "ISSN"}]}, "item_3_text_34": {"attribute_name": "メタデータ提供者", "attribute_value_mlt": [{"subitem_text_value": "メタデータ提供者: NAL-MATCH"}]}, "item_3_text_35": {"attribute_name": "JAXAカテゴリ", "attribute_value_mlt": [{"subitem_text_value": "JAXAカテゴリ: 航空宇宙技術研究所"}]}, "item_3_text_36": {"attribute_name": "JAXAカテゴリ2", "attribute_value_mlt": [{"subitem_text_value": "JAXAカテゴリ2: AP"}]}, "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: 9"}]}, "item_3_text_6": {"attribute_name": "著者所属", "attribute_value_mlt": [{"subitem_text_value": "航空宇宙技術研究所制御部"}, {"subitem_text_value": "航空宇宙技術研究所制御部"}]}, "item_3_text_7": {"attribute_name": "著者所属(英)", "attribute_value_mlt": [{"subitem_text_language": "en", "subitem_text_value": "Control Systems Division, National Aerospace Laboratory(NAL)"}, {"subitem_text_language": "en", "subitem_text_value": "Control Systems Division, National Aerospace Laboratory(NAL)"}]}, "item_creator": {"attribute_name": "著者", "attribute_type": "creator", "attribute_value_mlt": [{"creatorNames": [{"creatorName": "円居, 繁治"}], "nameIdentifiers": [{"nameIdentifier": "473796", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "大月, 正男"}], "nameIdentifiers": [{"nameIdentifier": "473797", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "ENKYO, Shigeharu", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "473798", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "OOTSUKI, Masao", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "473799", "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": "2020-01-29"}], "displaytype": "detail", "download_preview_message": "", "file_order": 0, "filename": "naltr01005.pdf", "filesize": [{"value": "1.0 MB"}], "format": "application/pdf", "future_date_message": "", "is_thumbnail": false, "licensetype": "license_free", "mimetype": "application/pdf", "size": 1000000.0, "url": {"label": "naltr01005.pdf", "url": "https://jaxa.repo.nii.ac.jp/record/45264/files/naltr01005.pdf"}, "version_id": "58c1513c-5f24-44c9-8f6c-4e42decdd6a0"}]}, "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": "静電気支持による高感度加速度計の研究(I)-基本的解析と実験的検討-", "item_titles": {"attribute_name": "タイトル", "attribute_value_mlt": [{"subitem_title": "静電気支持による高感度加速度計の研究(I)-基本的解析と実験的検討-"}]}, "item_type_id": "3", "owner": "1", "path": ["1893", "1917"], "permalink_uri": "https://jaxa.repo.nii.ac.jp/records/45264", "pubdate": {"attribute_name": "公開日", "attribute_value": "2015-03-26"}, "publish_date": "2015-03-26", "publish_status": "0", "recid": "45264", "relation": {}, "relation_version_is_last": true, "title": ["静電気支持による高感度加速度計の研究(I)-基本的解析と実験的検討-"], "weko_shared_id": -1}
静電気支持による高感度加速度計の研究(I)-基本的解析と実験的検討-
https://jaxa.repo.nii.ac.jp/records/45264
https://jaxa.repo.nii.ac.jp/records/4526477336c4c-e317-4093-952a-5313582bdac5
名前 / ファイル | ライセンス | アクション |
---|---|---|
naltr01005.pdf (1.0 MB)
|
|
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 | 静電気支持による高感度加速度計の研究(I)-基本的解析と実験的検討- | |||||
言語 | ||||||
言語 | jpn | |||||
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 | Study on a Highly Sensitive Electro-static Suspended Accelerometer (I) | |||||
著者 |
円居, 繁治
× 円居, 繁治× 大月, 正男× ENKYO, Shigeharu× OOTSUKI, Masao |
|||||
著者所属 | ||||||
航空宇宙技術研究所制御部 | ||||||
著者所属 | ||||||
航空宇宙技術研究所制御部 | ||||||
著者所属(英) | ||||||
en | ||||||
Control Systems Division, National Aerospace Laboratory(NAL) | ||||||
著者所属(英) | ||||||
en | ||||||
Control Systems Division, National Aerospace Laboratory(NAL) | ||||||
出版者 | ||||||
出版者 | 航空宇宙技術研究所 | |||||
出版者(英) | ||||||
出版者 | National Aerospace Laboratory(NAL) | |||||
書誌情報 |
航空宇宙技術研究所報告 en : Technical Report of National Aerospace Laboratory TR-1005 巻 1005, p. 15, 発行日 1988-10 |
|||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | An artificial satellite in orbit is not free from accelerations due to external forces such as : (1)gravitational anomalies of the earth’s oblateness, (2)gravitational attractions of the sun and the moon, (3)pressure of solar wind, (4)aerodynamic drags. The accelerations are very small ; however, they disturb precise position keeping of a satellite, attitude control of a large space system and also micro-gravity experiments such as IML in the Space lab. A highly sensitive electro-static suspended accelerometer was studied to measure such disturbances. The device has a hollow vacuum vessel. A non-magnetic metal sphere is suspended at the center of the vessel by means of three-dimensional electro-static fields. A small displacement of the position of the sphere due to external forces induces un-balanced electro-static forces in the fields. The force difference is measured as an electrical output. This paper presents an analysis of the design of the accelerometer. A series of preliminary experiments has been carried out to confirm the analysis by developing a two-axis accelerometer. The experimental result shows good stability for 10(exp -7)g with a threshold at the 10(exp -8)g level. | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 0389-4010 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: NALTR1005000 | |||||
レポート番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | レポート番号: NAL TR-1005 |