DocumentCode :
3075685
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
fYear :
1990
fDate :
5-7 Dec 1990
Firstpage :
3362
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;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Decision and Control, 1990., Proceedings of the 29th IEEE Conference on
Conference_Location :
Honolulu, HI
Type :
conf
DOI :
10.1109/CDC.1990.203419
Filename :
203419
Link To Document :
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