Abstract
A mutivariable control concept for a jet engine is proposed and investigated in this paper. The feedback control law is based on H∞-design. The control concept is applied to the RM12 jet engine for the Swedish fighter aircraft JAS 39 Gripen in a research program for future advanced control. The controller has so far been developed for the core engine operating range, at sea level static conditions, and evaluated via simulation with a detailed non-linear model. This evaluation clearly shows the potential of using more advanced control methods in the area of jet engine control.
Published Version
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