Title :
Modelling flight dynamics for the Airbus A320
Author :
Cheung Chiu Wo;Zhu Quan Min
Author_Institution :
Department of Engineering Design and Mathematics, University of the West of England Bristol, England, BS16 1QY
Abstract :
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 with the proposed dynamic models. Moreover, operating the MATLAB can demonstrate the developed prototype and algorithm for the Airbus A320. Furthermore, the relevant data can be collected from operating MATLAB; the data will then run the program to show how the system works, after the program has computed this information, a graph diagram will show the motion of the aircraft.
Keywords :
"Aircraft","Mathematical model","Stability analysis","MATLAB","Oscillators","Atmospheric modeling","Damping"
Conference_Titel :
Modelling, Identification and Control (ICMIC), 2015 7th International Conference on
DOI :
10.1109/ICMIC.2015.7409340