Aero Engine Multivariable Robust Control

ABSTRACT: In this study evaluating the performance and power consumption of a least effort controller for an aero engine is analyzed. This paper presents an application of robust stability analysis tool to solve the problem of  H for aero engine. A study of part of the control system for aircraft engines and for general multivariable applications is applied, and it is shown how this method can assist in developing the robust stability and performance of the engine.