Abstract
A fuzzy attitude control based on subsection Lyapunov method for flexible satellites with solar paddles was proposed. For flexible spacecraft is characteristics with strong coupling, nonlinearities and uncertainties, using T-S model as an approximation for the nonlinear system, a subsection state feedback control was designed. Simulation results show that the presented control can ensure the precision of the attitude control performance, the suppression of the structure vibrations and the robustness of the control system.
| Original language | English |
|---|---|
| Pages (from-to) | 2197-2199+2205 |
| Journal | Xitong Fangzhen Xuebao / Journal of System Simulation |
| Volume | 19 |
| Issue number | 10 |
| State | Published - 20 May 2007 |
Keywords
- Flexible satellite attitude control
- Fuzzy control
- Subsection Lyapunov method
- T-S model
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