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