Abstract
This chapter discusses a very simple use of the TP model transformation without any convex hull manipulation to derive a controller to the 3DoF aeroelastic wing section. More complex design approaches are discussed later. The design procedure applied in this chapter has two steps. First, a TP model is derived that defines a tight convex hull. In the second step, the LMI design framework is directly executed on the vertex LTI components of the TP model. Following a description of these two steps, the chapter discusses and evaluates the resulting control performance via numerical simulations. The chapter is based on the works [6].
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Baranyi, P. (2016). TP Model Based Control Design. In: TP-Model Transformation-Based-Control Design Frameworks. Springer, Cham. https://doi.org/10.1007/978-3-319-19605-3_9
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DOI: https://doi.org/10.1007/978-3-319-19605-3_9
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