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Design and analysis of hybrid thrust magnetic bearing for magnetically suspended reaction wheel

科研成果: 书/报告/会议事项章节会议稿件同行评审

摘要

Introduced the structure of a magnetic bearing reaction wheel for stabilization of spacecraft attitude, its rotation speed is from -5000rpm to 5000rpm (rating angular momentum is 20Nms). The main scope of this paper is to calculate and analyze the performance and parameters of the hybrid thrust magnetic bearing with permanent magnet bias for the magnetic bearing momentum wheel. Its magnetic force, current stiffness, and position stiffness are derived by using the equivalent magnetic circuit and their non-linearity are shown by the curves of force-current-position characteristic. The ranges of bearing capacity is obtained.

源语言英语
主期刊名Seventh International Symposium on Instrumentation and Control Technology
主期刊副标题Sensors and Instruments, Computer Simulation, and Artificial Intelligence
DOI
出版状态已出版 - 2008
活动7th International Symposium on Instrumentation and Control Technology: Sensors and Instruments, Computer Simulation, and Artificial Intelligence - Beijing, 中国
期限: 10 10月 200813 10月 2008

出版系列

姓名Proceedings of SPIE - The International Society for Optical Engineering
7127
ISSN(印刷版)0277-786X

会议

会议7th International Symposium on Instrumentation and Control Technology: Sensors and Instruments, Computer Simulation, and Artificial Intelligence
国家/地区中国
Beijing
时期10/10/0813/10/08

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