The development of a fixed wing aircraft analysis and design flight dynamic software

The present work focused on the development of computer software for flight dynamic analysis and controlling the behavior of a fixed-wing aircraft. For a given aircraft geometry, mass and inertia properties, and flight conditions, the software was designed in such a way to start the estimation of ae...

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Bibliographic Details
Main Author:	Ahmad Alaian, Ahmad Eshtiwey
Format:	Thesis
Language:	English English English
Published:	2016
Subjects:	TL500-777 Aeronautics. Aeronautical engineering
Online Access:	http://eprints.uthm.edu.my/818/
Abstract	Abstract here

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