Search

Focuses on the nonfragile H[sub infinity] controller design problem for linear time-invariant systems. Assumption of the controller design to have norm-bounded uncertainties; Design methods for dynamic output feedback; Quadratic stability of the closed-loop system.

Presents an actuator fault estimation scheme based on the augmented error method for flight control system. Design of the flight control system of an F4-fighter aircraft; Details on the mathematical framework needed for optimizing the autopilot design; Effort to combine the use of robust control and fault detection and isolation techniques for fault-tolerant flight control.