On the development computer, code for determinig 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 sy...

全面介绍

Saved in:
书目详细资料
主要作者: Khaire Elarosi, Muwfik Faidi
格式: Thesis
语言:English
English
English
出版: 2013
主题:
在线阅读:http://eprints.uthm.edu.my/1991/1/24p%20MUWFIK%20FAIDI%20KHAIRE%20ELAROSI.pdf
http://eprints.uthm.edu.my/1991/2/MUWFIK%20FAIDI%20KHAIRE%20ELAROSI%20COPYRIGHT%20DECLARATION.pdf
http://eprints.uthm.edu.my/1991/3/MUWFIK%20FAIDI%20KHAIRE%20ELAROSI%20WATERMARK.pdf
标签: 添加标签
没有标签, 成为第一个标记此记录!
实物特征
总结: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 system and also with respect to their axis body system had been used. These twelve equations are coupling each to others and in the forms highly non linear equation; the numerical approach is required for solving such system equation. The coefficient of system equation can be said as a result of the combination between aircraft’s mass and inertia, aircraft geometry properties and also their aircraft aerodynamics derivatives. The present work is focused in the development computer code which allows in manner of determining the root of equation of the 12 equations which described the flight behavior for particular airplane. Through determining the root of equation one will able to carry out a non linear transient analysis such as aircraft at landing approaches gust response and pilot initiated maneuvers.