Model-Based Aeroengine Nonlinear Set Point Control

Aeroengine control systems consist of fuel pump systems, burner and afterburner fuel metering devices, bleeding valves, variable geometry actuators, sensors, tip clearance controls, generators and engine control units etc., to fulfil but not limited with functions such as power management, start logic, idle control, takeoff control, climbing control, fuel metering, acceleration and deceleration control, limit protection control, variable stator vane control, valve bleeding control, tip clearance control, anti-surge control, together with monitoring, fault detection and other intelligent functions etc.