Basic Dynamical Systems Control of Aeroengine Flow

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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.
6pages

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Dynamical Systems, 49K20, 93B05, 93B27, 35K40, 35K55

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http://salesiana.dossiersoluciones.com/handle/123456789/59917

Consulte el texto completo en el siguiente enlace:

https://arxiv.org/abs/math/0009114
 http://arxiv.org/abs/math/0009114

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arXiv