Abstract
A continuous sliding mode control method based on feedback linearization is presented to realize the coupling control for a MIMO nonlinear system such as helicopter. A discontinuous sliding mode control can be changed into a continuous one by extending the nonlinear system. Thus the system robustness can be enhanced. The control system for the vertical flight mode of a helicopter is designed. Simulation results are in agreement with the theoretical analysis results and the system can track the given input.
| Original language | English |
|---|---|
| Pages (from-to) | 378-381 |
| Number of pages | 4 |
| Journal | Xibei Gongye Daxue Xuebao/Journal of Northwestern Polytechnical University |
| Volume | 18 |
| Issue number | 3 |
| State | Published - Aug 2000 |
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