The output feedback control strategy for the two-dimensional aeroelastic system that includes state feedback-controller and an observer, is discussed. The linear matrix inequality (LMI) techniques in the parallel distributed compensation (PDC) design framework can be executed to define controllers according to various different control specifications. Both the controller and the observer are designed with the help of the TP model transformation and the feasibility test of LMIs under the PDC framework. The extra constraints have been proposed on the coefficient functions of the TP model transformation with an extra step capable of satisfying the constraints to relax the observer design.
ASJC Scopus subject areas
- Control and Systems Engineering
- Aerospace Engineering
- Space and Planetary Science
- Electrical and Electronic Engineering
- Applied Mathematics