Abstract
This chapter focuses on the most recent version of the 3DoF nonlinear aeroelastic wing section model generated from a real measurement and including Stribeck friction model. The goal is to describe and prepare a complex example for the next chapters, in order to study the usability and the effectiveness of the TP model transformation based design frameworks.
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Z. Prime, B. Cazzolato, C. Doolan, T. Strganac, Linear-parameter-varying control of an improved three-degree-of-freedom aeroelastic model. J. Guid. Control Dyn. 33(2), 615–619 (2010)
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© 2016 Springer International Publishing Switzerland
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Baranyi, P. (2016). qLPV Model of the 3DoF Prototypical Aeroelastic Wing Section. In: TP-Model Transformation-Based-Control Design Frameworks. Springer, Cham. https://doi.org/10.1007/978-3-319-19605-3_8
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DOI: https://doi.org/10.1007/978-3-319-19605-3_8
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Publisher Name: Springer, Cham
Print ISBN: 978-3-319-19604-6
Online ISBN: 978-3-319-19605-3
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