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LPV MODELING OF A TURBOFAN ENGINE
IFAC Postprint Volumes IPPV / International Federation of Automatic Control, 2005Abstract This article describes the application of quasi-LPV modeling techniques to an industrial military turbofan engine simulator developed by Snecma Moteurs, the French aerospace propulsion company. Two approaches are used, classical Jacobian linearization and velocity based linearization. First, we present briefly the theoretical aspects of both
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