Basic Dynamical Systems Control of Aeroengine Flow

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dc.creatorBirnir, Bjorn
dc.creatorHauksson, Hoskuldur A.
dc.date2000-09-12
dc.date.accessioned2026-07-07T04:37:20Z
dc.date.available2026-07-07T04:37:20Z
dc.descriptionThe 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.
dc.description6pages
dc.identifierhttps://arxiv.org/abs/math/0009114
dc.identifierhttp://arxiv.org/abs/math/0009114
dc.identifier.urihttp://salesiana.dossiersoluciones.com/handle/123456789/59917
dc.subjectDynamical Systems
dc.subject49K20, 93B05, 93B27, 35K40, 35K55
dc.titleBasic Dynamical Systems Control of Aeroengine Flow
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