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...
Saved in:
Main Author: | Ahmad Alaian, Ahmad Eshtiwey |
---|---|
Format: | Thesis |
Language: | English English English |
Published: |
2016
|
Subjects: | |
Online Access: | http://eprints.uthm.edu.my/818/1/24p%20AHMAD%20ESHTIWEY%20AHMAD%20ALAIAN.pdf http://eprints.uthm.edu.my/818/2/AHMAD%20ESHTIWEY%20AHMAD%20ALAIAN%20COPYRIGHT%20DECLARATION.pdf http://eprints.uthm.edu.my/818/3/AHMAD%20ESHTIWEY%20AHMAD%20ALAIAN%20WATERMARK.pdf http://eprints.uthm.edu.my/818/ |
Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
Similar Items
-
On the development of computer code for aircraft flight dynamics analysis
by: Mohamed Alazomui, Outman
Published: (2014) -
The aerodynamics analysis of type UAV aircraft with pusher engine configuration by use of DATCOM software
by: Al Aian, Ahmad Eshtiwey
Published: (2011) -
The flight trajectory analysis on the existing aircraft
by: M Khalifa, Tarek M.
Published: (2012) -
Real-time identification of an unmanned quadcopter flight dynamics using fully tuned radial basis function network
by: Pairan, Mohammad Fahmi
Published: (2018) -
ESA 366 – FLIGHT PERFORMANCE JANUARY 2014
by: PPKA, Pusat Pengajian Kejuruteraan Aeroangkasa
Published: (2014)