Title : 
H∞ robust control synthesis for a fighter performing a coordinated bank turn
         
        
            Author : 
Thompson, Peter M. ; Chiang, Richard Y.
         
        
            Author_Institution : 
Syst. Technol. Inc., Hawthorne, CA, USA
         
        
        
        
        
            Abstract : 
H∞ synthesis techniques are used to design a bank angle autopilot which commands a coordinated bank turn. Two variations of the H∞ design are compared to a multivariable classical design. Both of the H∞  designs have better performance and actuator robustness measures. The first H∞ design, however, contains an undesirable cancellation of a lightly damped Dutch roll mode, which causes a poor parameter robustness measure. The second H∞ design corrects this problem by using the same inner loop yaw damper as used by the classical design
         
        
            Keywords : 
aerospace computer control; aircraft control; control system synthesis; military equipment; optimal control; stability; H∞ robust control synthesis; bank angle autopilot; coordinated bank turn; fighter aircraft; inner loop yaw damper; lightly damped Dutch roll; Actuators; Aircraft; Control system synthesis; Cost function; Feedback control; H infinity control; Optimal control; Robust control; Robustness; System performance;
         
        
        
        
            Conference_Titel : 
Decision and Control, 1990., Proceedings of the 29th IEEE Conference on
         
        
            Conference_Location : 
Honolulu, HI
         
        
        
            DOI : 
10.1109/CDC.1990.203419