Abstract
In order to improve the temperature control effect of micro spacecraft, an active temperature control system using thermoelectric cooler is presented. A dynamical model of spacecraft temperature change is built up, and the temperature control effect is simulated and analyzed. Simulation results show that the temperature change of spacecraft electronic equipment can be successfully controlled, and the dynamical models presented can be conveniently used in thermoelectric cooler temperature control system simulation and optimization.
| Original language | English |
|---|---|
| Pages (from-to) | 149-152 |
| Number of pages | 4 |
| Journal | Jixie Gongcheng Xuebao/Journal of Mechanical Engineering |
| Volume | 41 |
| Issue number | 10 |
| DOIs | |
| State | Published - Oct 2005 |
Keywords
- Active temperature control
- Micro spacecraft
- Thermoelectric cooler
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