Zak and Hui [1] proposed a sliding mode controller for linear multiple-inpu
t-multiple-output (MIMO) systems using static output feedback. The note in
[2] provided an improvement of the output feedback controller in [1] for a
class of linear single-input-single-output (SISO) systems that eliminated t
wo important limitations of [1]: (a) system uncertainties must be bounded b
y the system output; and (b) a requirement of a matrix inequality [1, eq. (
4-3)]. The controller in [2] can guarantee global closed-loop stability. Th
is note extends the results of [2] to linear MIMO systems. It is emphasized
that the proposed MIMO controller yields global closed-loop stability wher
eas the one in [1] can only guarantee local stability. An application of th
e proposed MIMO controller to an aircraft model is included to show the eff
ectiveness of the method.