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 |
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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 |