Abstract
In the design of control and simulation system of flexible satellite, the dynamic model of satellite was built based on mathematic function mostly. A new method based on virtual prototype technology was proposed. With this method, the modeling and control of flexible satellite are based on the ADAMS and MATLAB. The feasibility and advantages about the method were revealed, and the main process about it was introduced in detail. A case about flexible satellite controlled by three-axis zero momentum reaction flywheel validates the effect of the method.
| Original language | English |
|---|---|
| Pages (from-to) | 590-593+598 |
| Journal | Xitong Fangzhen Xuebao / Journal of System Simulation |
| Volume | 21 |
| Issue number | 2 |
| Publication status | Published - 20 Jan 2009 |
Keywords
- ADAMS
- FEA
- MATLAB
- Solid modeling
- United-simulation