Результаты исследований: Научные публикации в периодических изданиях › статья › Рецензирование
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.
Язык оригинала | английский |
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Страницы (с-по) | 329-339 |
Число страниц | 11 |
Журнал | European Journal of Control |
Том | 14 |
Номер выпуска | 4 |
DOI | |
Состояние | Опубликовано - 2008 |
ID: 87379673