A novel integrated guidance and autopilot design method is proposed for homing missiles based on the adaptive block dynamic surface control approach.
The stability property of the closed-loop network is established via Lyapunov analysis, and transient property is quantified in terms of L2 norms of the derivatives of neural weights, which are shown to be smaller than the classical neural dynamic surface control approach.
Combining the backstepping technique with the dynamic surface control (DSC) approach, a novel adaptive fuzzy faults-tolerant control approach is constructed.
Moreover, a systematic procedure is developed for the synthesis of adaptive fuzzy dynamic surface control (DSC) approach.
The dynamic surface control (DSC) approach is used to solve the problem of 'explosion of complexity' in the backstepping design procedure.
Under the frame of a backstepping design, an adaptive sliding mode output-feedback dynamic surface control (DSC) approach is derived recursively by virtue of the estimated states.
Then, a novel distributed robust adaptive controller is developed by combining the backstepping method and the Dynamic Surface Control (DSC) approach.
This paper investigates the adaptive fuzzy output-feedback dynamic surface control (DSC) approach with prescribed performance for a class of uncertain switched nonlinear systems with unknown dead-zone.
Based on the backstepping design technique and the dynamic surface control (DSC) approach, a novel adaptive fuzzy decentralized output-feedback control scheme is developed.
