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The aim of this pro ect will be focused on creating two different types of flight controllers for the Airbus A320 using AT AB Simulink. The flight controller used for the aircraft has a decoupled flight controller and a coupled flight controller; a decoupled flight controller means the longitudinal stability derivatives and lateral stability derivatives will have their own state-space dynamic model,...
This paper is to model an Airbus A320 by using a computer; before this can be done research of the aircraft manufacture data needs to be done first. Therefore the data results can be applied to values from equation and formulae to calculate the flight results for the aircraft. From these, the calculated data is then computed in to software known as MATLAB in order to develop a program which can fit...
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