Ubiquitous Computing and Communication Journal
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Abstract
Title: AIR-TO-GROUND INTEGRATED FUZZY GUIDANCE SYSTEM
Authors: Dr. Mohamed Rizk, Mr. Ahmed Abdelsalam
Abstract:
In this paper we consider the problem of air to ground missile guidance system using fuzzy controller. The missile model is assumed as three degree of freedom (3DOF) (assuming the analysis in the vertical plane only).The homing guidance method is used. This paper presents numerical results for applying the fuzzy controller to the missile in different situations of control parameters in different positions.