Adaptive Incremental Backstepping Flight Control

This thesis deals with the development of Adaptive Incremental Backstepping control laws for a high-performance aircraft model (F-16), in order to make the airplane robustly seek references in roll rate and angle of attack at a constant airspeed while minimizing sideslip. An Incremental Backstepping scheme that relies on estimates of the angular...

From data to performance system; identification uncertainty and robust control design

System identification for rubust process control. Nominal models and error bounds

Identification of model uncertainty for control design