Результаты исследований: Материалы конференций › материалы › Рецензирование
The combined adaptive control (CAC) law for an autopilot of the unmanned aerial vehicle (UAV) attitude control is considered. The adaptive algorithm includes the variable-structure controller with forced sliding motion, parametric identification algorithm and the parallel feedforward compensator. The adaptation algorithm provides the prescribed dynamic properties of the attitude control system for various flight conditions of the UAV. The simulation results for nonlinear UAV dynamics model are presented.
Язык оригинала | английский |
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Страницы | 290-291 |
Число страниц | 2 |
Состояние | Опубликовано - 2002 |
Событие | Proceedings of the 2002 IEEE International Conference on Control Applications - Glasgow, Великобритания Продолжительность: 18 сен 2002 → 20 сен 2002 |
конференция | Proceedings of the 2002 IEEE International Conference on Control Applications |
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Страна/Tерритория | Великобритания |
Город | Glasgow |
Период | 18/09/02 → 20/09/02 |
ID: 88358490