2004 Volume 47 Issue 156 Pages 138-145
This paper proposes an exact polytopic model for the linear parameter varying (LPV) system of aircraft. The LPV system of the linearized equation of aircraft is represented by a descriptor form which reserves physical features of the equation. A polytopic model, called descriptor polytopic model, is derived through a variable transformation to satisfy conditions for the polytope. Using the obtained descriptor polytopic model, a gain scheduling state feedback law is then designed by means of a linear matrix inequality (LMI) formulation. It is shown in a numerical example of a longitudinal flight control that the proposed descriptor polytopic model of aircraft had no model error and exactly represented the original LPV system without any unnecessary flight region.