On the development computer code for determining the root of equation for transient flight analysis

This thesis presents the governing equation of flight motions which can be used to describe the flight behavior of any type flying vehicles consist of 12 equations described 12 state – space variables involving the aircraft position and aircraft aptitude with respect to the inertial coordinate syste...

Full description

Saved in:
Bibliographic Details
Main Author: Elarosi, Muwfik Faidi Khaire
Format: Thesis
Published: 2013
Subjects:
Online Access:http://eprints.uthm.edu.my/5521/
http://eprints.uthm.edu.my/5521/1/MUWFIK_FAIDI_KHAIRE_ELAROSI.pdf
Tags: Add Tag
No Tags, Be the first to tag this record!