Paper
9 October 2008 Design and analysis of hybrid thrust magnetic bearing for magnetically suspended reaction wheel
Bangcheng Han
Author Affiliations +
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.
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Bangcheng Han "Design and analysis of hybrid thrust magnetic bearing for magnetically suspended reaction wheel", Proc. SPIE 7127, Seventh International Symposium on Instrumentation and Control Technology: Sensors and Instruments, Computer Simulation, and Artificial Intelligence, 712708 (9 October 2008); https://doi.org/10.1117/12.806250
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KEYWORDS
Magnetism

Space operations

Nickel

Electromagnetism

Iron

Prototyping

Astronomical engineering

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