Enhanced Fighter Jet Super-Maneuverability Control Using Preset Performance Design

This research focuses on improving the control quality of fighter jet supermaneuverability. To achieve this, a preset performance control method is employed to quantitatively design the tracking error. This method integrates a disturbance observer and an improved dynamic surface control approach to design a robust preset performance controller. Simulation studies demonstrate that the tracking accuracy of the aircraft attitude angle has been significantly enhanced. Furthermore, both the steady-state and transient performance consistently meet the predetermined requirements, leading to a substantial improvement in flight control quality.