DSP based implementation of an input/output feedback linearization control technique applied to a three-phase three-level neutral point clamped boost rectifier

Author(s):  
L. Yacoubi ◽  
K. Al-Haddad ◽  
L.A. Dessaint ◽  
F. Fnaiech
Author(s):  
Hui Zhao ◽  
Jinfu Liu ◽  
Daren Yu

This paper aims to develop an applicable nonlinear control technique for aeroengines. An approximate nonlinear model is presented and a rational identification procedure is given. Exact input-output feedback linearization can be easily performed on this model. The controller derived can approximately linearize the plant such that the close-loop system exhibits linear input-output dynamics locally. Modeling and controlling are exemplified and validated by a small turbofan engine. Simulation results illustrate that the modeling accuracy is good and linear close-loop system dynamics are achieved.


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