Representation and analysis of control surface freeplay nonlinearity
Abstract
Different representations for a control surface freeplay nonlinearity in a three degree of freedom aeroelastic system are assessed. These are the discontinuous, polynomial and hyperbolic tangent representations. The Duhamel formulation is used to model the aerodynamic loads. Assessment of the validity of these representations is performed through comparison with previous experimental observations. The results show that the instability and...
Paper Details
Title
Representation and analysis of control surface freeplay nonlinearity
Published Date
May 1, 2012
Volume
31
Pages
79 - 91
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