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.
| Original language | English |
|---|---|
| Title of host publication | ICEMS 2005 |
| Subtitle of host publication | Proceedings of the Eighth International Conference on Electrical Machines and Systems |
| Pages | 695-698 |
| Number of pages | 4 |
| State | Published - 2005 |
| Event | ICEMS 2005: 8th International Conference on Electrical Machines and Systems - Ninjing, China Duration: 27 Sep 2005 → 29 Sep 2005 |
Publication series
| Name | ICEMS 2005: Proceedings of the Eighth International Conference on Electrical Machines and Systems |
|---|---|
| Volume | 1 |
Conference
| Conference | ICEMS 2005: 8th International Conference on Electrical Machines and Systems |
|---|---|
| Country/Territory | China |
| City | Ninjing |
| Period | 27/09/05 → 29/09/05 |
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