Title :
Robustness improvement of the F-14 benchmark control problem using H∞ optimization
Author_Institution :
Minnesota Univ., Minneapolis, MN, USA
Abstract :
The problem of multivariable control system design has been studied by many researchers. Feedback has been used in control system engineering as a means for satisfying design requirements such as system stabilization, reduction of system response to external disturbances, realization of specified transient response and/or frequency response characteristics, and improvement of a system´s robustness against variations in open loop dynamics. The controller for the linearized model of the Grumman aircraft F-14 due to R. Rimer and D.K. Frederick (1987), is redesigned using H∞ optimisation. The overall system robustness can be improved by changing weights
Keywords :
aircraft control; control system synthesis; feedback; multivariable control systems; optimal control; stability; F-14; F-14 benchmark control problem; Grumman aircraft; H∞ optimization; feedback; frequency response characteristics; multivariable control system design; open loop dynamics variation; transient response;
Conference_Titel :
Control 1991. Control '91., International Conference on
Conference_Location :
Edinburgh
Print_ISBN :
0-85296-509-5
