This paper investigates the application of the gain-scheduling approach to
flight control tasks, where the conditions required by conventional techniq
ues need not be satisfied. The conditions required by conventional techniqu
es are progressively relaxed, and the design of gain-scheduled controllers
under a range of conditions Is addressed. In particular, the paper consider
s gain-scheduled control design in situations where the vehicle is maneuver
ing. aggressively far from equilibrium, the airspeed need not be slowly var
ying, and/or scheduling on the Instantaneous incidence angle is required.