Title :
Gain scheduling for H-infinity controllers: a flight control example
Author :
Nichols, Robert A. ; Reichert, Robert T. ; Rugh, Wilson J.
Author_Institution :
Dept. of Electr. & Comput. Eng., Johns Hopkins Univ., Baltimore, MD, USA
fDate :
6/1/1993 12:00:00 AM
Abstract :
A new approach to gain scheduling linear dynamic controllers is illustrated for a pitch-axis autopilot design problem. In this application the linear controllers are designed at distinct operating conditions by H∞ methods. The gain scheduling procedure uses particular features of both the linear dynamic controllers and the controller configuration to remove so-called hidden coupling terms that can occur in scheduled controllers. Potential performance improvement is demonstrated by comparing simulation results to those for a naive gain scheduled controller that ignores the coupling terms
Keywords :
aerospace control; control system synthesis; optimal control; scheduling; H-infinity controllers; flight control; gain scheduling linear dynamic controllers; hidden coupling terms; pitch-axis autopilot; Acceleration; Aerodynamics; Aerospace control; Dynamic scheduling; H infinity control; Laboratories; Missiles; Performance gain; Physics; Tail;
Journal_Title :
Control Systems Technology, IEEE Transactions on