ROBUST CONTROL FOR NON-MINIMUM PHASE SYSTEMS WITH ACTUATOR FAULTS: APPLICATION TO AIRCRAFT LONGITUDINAL FLIGHT CONTROL

Robust Control for Non-Minimum Phase Systems with Actuator Faults: Application to Aircraft Longitudinal Flight Control

This study is concerned with developing a robust tracking control system that merges the optimal control theory with fractional-order-based control and the heuristic optimization algorithms into a single framework for the non-minimum phase pitch angle dynamics of Boeing 747 aircraft.The main control objective is to deal with the non-minimum phase n

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