Learning air-to-ground integrated fuzzy guidance system using simulated annealing

In this paper we consider the problem of air to ground missile guidance system using fuzzy controller which uses Pure Pursuit method. The fuzzy controller's rules are defined using Simulated Annealing (SA). The missile model is assumed as three degree of freedom (3DOF) (assuming the analysis in the vertical plane only). This paper presents numerical results for applying the learned fuzzy controller to the missile in different situations of control parameters.