LINEAR AND NONLINEAR FUZZY CONTROLLERS FOR GUIDED MISSILE SYSTEM

Abstract

In recent years control system has gained an increasingly important role in development of advance systems for military applications This thesis entitled Linear and Non-linear Fuzzy Controller for Guided Missile System deals with the design of controller for highly efficient actuation and positioning of the guided missile system, when the parameters of missile system vary with time. The controller gives the required direction to the actuation system for missile mounted on the moving vehicle. This guiding system is established with the help of the controller which analyses the performance of the system and helps it to attain equilibrium position with the help of linear/non linear Proportional Derivative Fuzzy Controller. The analyses of guided missile system for both linear as well as non linear model, is presented. The applied controller use close loop Fuzzy Proportional Derivative controllers for vertical and horizontal positioning of the missile system when missile parameter vary...