DocumentCode
3007624
Title
Temperature rise calculation and test of the wheel motor for satellite in vacuum
Author
HongWei, Zhu ; Jibin, Zou
Author_Institution
Dept. of Electr. Eng., Harbin Inst. of Technol., China
Volume
1
fYear
2005
fDate
27-29 Sept. 2005
Firstpage
695
Abstract
The wheel motor is a core part for the satellite attitude control. To design and use the motor in the outer space, it is necessary to calculate and test the temperature rise accurately. Based on the thermal circuit method and the FEM (finite element method), the steady and the dynamic temperature rise of the ironless armature brushless DC motor were calculated. And the calculated result was certified by experiment.
Keywords
attitude control; brushless DC motors; finite element analysis; machine control; machine testing; FEM; dynamic temperature rise calculation; finite element method; ironless armature brushless DC motor; satellite attitude control; thermal circuit method; wheel motor; Brushless DC motors; Circuits; DC motors; Permanent magnet motors; Rotors; Satellites; Stators; Temperature; Testing; Wheels;
fLanguage
English
Publisher
ieee
Conference_Titel
Electrical Machines and Systems, 2005. ICEMS 2005. Proceedings of the Eighth International Conference on
Print_ISBN
7-5062-7407-8
Type
conf
DOI
10.1109/ICEMS.2005.202621
Filename
1574854
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