Fixed order mixed-norm controllers for the F-18 aircraft ape designed
to minimize the effects of wind and sensor noise while following a nor
mal acceleration command. The basic objective was to develop a control
ler of low order that provides good wind and noise response while exhi
biting robust performance in terms of command-following in the face of
changing Fight conditions. Controllers were designed using single nor
m methods as well as mixed H-2/H-infinity control with single and mult
iple constraints and mixed H-2/mu optimization. Comparisons illustrate
the advantages of mixed H-2/mu optimization with respect to noise res
ponse and controller order while guaranteeing robust performance.