| Article ID | Journal | Published Year | Pages | File Type |
|---|---|---|---|---|
| 708321 | European Journal of Control | 2008 | 11 Pages |
Abstract
Application of the passification-based adaptive control technique for control of Quanser/LAAS “Helicopter” laboratory setup is presented. Two adaptive control laws for pitch angle control are designed and experimentally tested. The MATLAB/Simulink and WinCon software environment is used for adaptive control laws implementation and the real-world experiments. The experimental results demonstrate high closed loop system performance and robustness of the suggested control laws with respect to parametric uncertainties and unmodeled plant dynamics and actuator faults.
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