The invention provides an improved Smith estimator-based H-infinity control method of an
aero engine, and belongs to the technical field of
aero engine control and
simulation. The improved Smith estimator-based H-infinity control method comprises the steps of building a reasonable small deviation
linear model for an
aero engine non-
linear model, and selecting data of a
state space model in a certain working condition as a controlled object designed by a controller; selecting an appropriate
performance index weighting function parameter, solving an H-infinity
output feedback controller, and adjusting the parameter to basically achieve control requirement; and designing an improved-structure Smith
estimation compensator according to a closed-loop
feedback control system designed according toan H-infinity control law so as to form a
composite controller, additionally arranging a deviation correction controller, designed according to a PID control law, in the
control system according to relatively large deviation between an
estimation model and the parameter of the controlled object and a true model and the parameter, employing the deviation correction controller to stabilize the controlled object, making adaptability correction according to comparison between the controlled object and a model output
signal so as to further improve robustness of the
system.