Abstract
The adaptive fuzzy control is combined with input-output linearization control to constitute the hybrid controller. The control method is then applied to the attitude maneuver control of the flexible satellite. The basic control structure is given. The rules of the controller parameter selection, which guarantee the attitude stabilization of the satellite with parameter uncertainties, have been analyzed. Simulation results show that the precise attitude control is accomplished in spite of the uncertainty in the system.
| Original language | English |
|---|---|
| Pages (from-to) | 140-144 |
| Number of pages | 5 |
| Journal | Journal of Beijing Institute of Technology (English Edition) |
| Volume | 14 |
| Issue number | 2 |
| Publication status | Published - Jun 2005 |
Keywords
- Adaptive fuzzy control
- Attitude maneuver
- Flexible satellite
- Input-output linearization