Basic Dynamical Systems Control of Aeroengine Flow
Dynamical Systems
2007-05-23 v1
Abstract
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.
Cite
@article{arxiv.math/0009114,
title = {Basic Dynamical Systems Control of Aeroengine Flow},
author = {Bjorn Birnir and Hoskuldur A. Hauksson},
journal= {arXiv preprint arXiv:math/0009114},
year = {2007}
}
Comments
6pages