SIMULATION OF FLIGHT THROUGH GUST
A flight simulation programme has been developed on a personal computer using Microsoft FORTRAN to simulate flight trajectories of a light aircraft by using Six-Degree-of-Freedom equation of motion. The simulation has been made realistic through pre-programmed the input to the control surfaces, atm...
Main Author: | |
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Format: | Article |
Language: | English |
Published: |
University of Baghdad
2011-12-01
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Series: | Journal of Engineering |
Online Access: | https://joe.uobaghdad.edu.iq/index.php/main/article/view/3046 |
_version_ | 1797350997825159168 |
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author | Kareem Jawad Kadhum |
author_facet | Kareem Jawad Kadhum |
author_sort | Kareem Jawad Kadhum |
collection | DOAJ |
description |
A flight simulation programme has been developed on a personal computer using Microsoft
FORTRAN to simulate flight trajectories of a light aircraft by using Six-Degree-of-Freedom
equation of motion. The simulation has been made realistic through pre-programmed the input to
the control surfaces, atmospheric gust during the flight mode. The programme plays an important
role in the evaluation and validation of the aircraft design process. A light aircraft (Cessna 182T)
has been tested through free flight, gliding flight, flight with gust. The results show good trend and
show that the programme could be dependent as a realistic flight test programme.
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first_indexed | 2024-03-08T12:54:08Z |
format | Article |
id | doaj.art-4451a539500648679917a61fa6898004 |
institution | Directory Open Access Journal |
issn | 1726-4073 2520-3339 |
language | English |
last_indexed | 2024-03-08T12:54:08Z |
publishDate | 2011-12-01 |
publisher | University of Baghdad |
record_format | Article |
series | Journal of Engineering |
spelling | doaj.art-4451a539500648679917a61fa68980042024-01-19T19:43:17ZengUniversity of BaghdadJournal of Engineering1726-40732520-33392011-12-01170610.31026/j.eng.2011.08.08SIMULATION OF FLIGHT THROUGH GUSTKareem Jawad Kadhum A flight simulation programme has been developed on a personal computer using Microsoft FORTRAN to simulate flight trajectories of a light aircraft by using Six-Degree-of-Freedom equation of motion. The simulation has been made realistic through pre-programmed the input to the control surfaces, atmospheric gust during the flight mode. The programme plays an important role in the evaluation and validation of the aircraft design process. A light aircraft (Cessna 182T) has been tested through free flight, gliding flight, flight with gust. The results show good trend and show that the programme could be dependent as a realistic flight test programme. https://joe.uobaghdad.edu.iq/index.php/main/article/view/3046 |
spellingShingle | Kareem Jawad Kadhum SIMULATION OF FLIGHT THROUGH GUST Journal of Engineering |
title | SIMULATION OF FLIGHT THROUGH GUST |
title_full | SIMULATION OF FLIGHT THROUGH GUST |
title_fullStr | SIMULATION OF FLIGHT THROUGH GUST |
title_full_unstemmed | SIMULATION OF FLIGHT THROUGH GUST |
title_short | SIMULATION OF FLIGHT THROUGH GUST |
title_sort | simulation of flight through gust |
url | https://joe.uobaghdad.edu.iq/index.php/main/article/view/3046 |
work_keys_str_mv | AT kareemjawadkadhum simulationofflightthroughgust |