Reduced equivalent systems have inherent closed-loop poles at the origin in the sliding mode for conventional sliding mode control (SMC). A systematic design strategy is developed for arbitrarily placing all SMC closed-loop poles. The speed control of a vertical takeoff and landing aircraft whose aerodynamic parameters vary considerably during flight is investigated. An outstanding output tracking performance and robustness against system parameter uncertainties and external disturbances are achieved.
Robust vertical takeoff and landing aircraft control via integral sliding mode
IEE Proceedings - Control Theory and Applications ; 150 , 4 ; 383-388
2003
6 Seiten, 10 Quellen
Aufsatz (Zeitschrift)
Englisch
Robust vertical takeoff and landing aircraft control via integral sliding mode
IET Digital Library Archive | 2003
|Europäisches Patentamt | 2023
|Europäisches Patentamt | 2025
|Europäisches Patentamt | 2023
|Europäisches Patentamt | 2024
|