Basic Dynamical Systems Control of Aeroengine Flow

Details Basic Dynamical Systems Control of Aeroengine Flow Basic Dynamical Systems Control of Aeroengine Flow

2000-09-12

arxiv.org/abs/math/0009114v1

Mathematics

Dynamical Systems

6pages

Scientific paper

The notions of basic controllability and basic control are defined using dynamical systems theory of partial differential equations. A quadratic optimal control of the linearized viscous Moore-Greitzer equation is presented and it is confirmed that stall is uncontrollable in this model. A basic control is constructed for the nonlinear viscous Moore-Greitzer equation which can control both surge and stall. Numerical simulations of the basic control are presented.

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