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

Research output: Chapter in Book/Report/Conference proceedingConference contributionpeer-review

Abstract

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.

Original languageEnglish
Title of host publicationSeventh International Symposium on Instrumentation and Control Technology
Subtitle of host publicationSensors and Instruments, Computer Simulation, and Artificial Intelligence
DOIs
StatePublished - 2008
Event7th International Symposium on Instrumentation and Control Technology: Sensors and Instruments, Computer Simulation, and Artificial Intelligence - Beijing, China
Duration: 10 Oct 200813 Oct 2008

Publication series

NameProceedings of SPIE - The International Society for Optical Engineering
Volume7127
ISSN (Print)0277-786X

Conference

Conference7th International Symposium on Instrumentation and Control Technology: Sensors and Instruments, Computer Simulation, and Artificial Intelligence
Country/TerritoryChina
CityBeijing
Period10/10/0813/10/08

Keywords

  • Current stiffness
  • Equivalent magnetic circuit
  • Magnetically suspended reaction wheel
  • Position stiffness
  • Thrust magnetic bearing

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