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人工衛星の姿勢制御ホイール用磁気軸受の剛性の解析
https://jaxa.repo.nii.ac.jp/records/44821
https://jaxa.repo.nii.ac.jp/records/44821b5bd4566-b113-4ca9-be1c-ef7f6695ac4e
名前 / ファイル | ライセンス | アクション |
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Item type | テクニカルレポート / Technical Report(1) | |||||||||
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公開日 | 2015-03-26 | |||||||||
タイトル | ||||||||||
タイトル | 人工衛星の姿勢制御ホイール用磁気軸受の剛性の解析 | |||||||||
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 | Analysis on the Stiffness of Magnetic Suspensions for Spacecraft Attitude Control Flywheels | |||||||||
著者 |
木田, 隆
× 木田, 隆
× KIDA, Takashi
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著者所属 | ||||||||||
航空宇宙技術研究所宇宙研究グループ | ||||||||||
著者所属(英) | ||||||||||
en | ||||||||||
Space Technology Research Group, 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-567 巻 567, p. 12, 発行日 1979-04 |
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抄録(英) | ||||||||||
内容記述タイプ | Other | |||||||||
内容記述 | Magnetic suspensions for spacecraft attitude control flywheels have such advantages as lower friction/stiction torque, higher reliability and longer life. It is considered that they will be widely used in the near future. This paper presents an analytical estimation method of the axial unbalance stiffness and radial stiffness, of a flywheel rotor, suspended by an axially controlled and radially passive, magnetic bearing. The axial unbalance stiffness is calculated by the utilization of equivalent electric circuits, in which magnetic permeances at air gaps are estimated, using the Roters’method. In the case of the radial stiffness calculation, however, it turns out that this method cannot be easily applied. Therefore, the Laplace equation is numerically solved to yield a potential function, and then the magnetic lines of force are estimated by solving another set of ordinary differential equations. From these results, the radial stiffness is calculated, by integrating the forces along the given boundary. The validity of thse methods is confirmed by the measured values of a laboratory modeled, magnetic suspension. | |||||||||
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: NALTR0567000 | |||||||||
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-567 |