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
2003-07-01
6 pages
Article (Journal)
English
stability , robustness , closed loop systems , velocity control , landing aircraft control , variable structure systems , aircraft control , reduced equivalent systems , closed-loop poles , sliding mode control , parameter uncertainties , integral sliding mode , robust vertical takeoff , speed control , robust control
Robust vertical takeoff and landing aircraft control via integral sliding mode
Tema Archive | 2003
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