Aim
Part 1 of this Simulation of Engineering Systems 3 Assignment involves the modeling, simulation, and validation of an Instrument Landing System (ILS) Lateral Beam Guidance System. This part of the assignment involves developing a mathematical model of the lateral dynamics of an aircraft
approaching using ILS for guidance. This model will be implemented in Matlab code and as a Simulink block diagram.

The responses from the Simulink block diagram will be used to analyze and validate the Matlab model and its associated simulation. This document provides background information about this system, followed by the problem specification for the mathematical model of the system and its simulation. Also, the Assignment Specifications are provided as a step-by-step guide for this part of the assignment.