TP Model Based Control Design
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 .
KeywordsTP model transformation Control design LMI