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...
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| Format: | Thesis |
| Language: | English English English |
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2013
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| Online Access: | 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 |
| _version_ | 1796868563380731904 |
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| author | Khaire Elarosi, Muwfik Faidi |
| author_facet | Khaire Elarosi, Muwfik Faidi |
| author_sort | Khaire Elarosi, Muwfik Faidi |
| collection | UTHM |
| description | 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. |
| first_indexed | 2024-03-05T21:41:39Z |
| format | Thesis |
| id | uthm.eprints-1991 |
| institution | Universiti Tun Hussein Onn Malaysia |
| language | English English English |
| last_indexed | 2024-03-05T21:41:39Z |
| publishDate | 2013 |
| record_format | dspace |
| spelling | uthm.eprints-19912021-10-14T05:52:54Z http://eprints.uthm.edu.my/1991/ On the development computer, code for determinig the root of equation for transient flight analysis Khaire Elarosi, Muwfik Faidi TL Motor vehicles. Aeronautics. Astronautics TL500-777 Aeronautics. Aeronautical engineering 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. 2013-12 Thesis NonPeerReviewed text en http://eprints.uthm.edu.my/1991/1/24p%20MUWFIK%20FAIDI%20KHAIRE%20ELAROSI.pdf text en http://eprints.uthm.edu.my/1991/2/MUWFIK%20FAIDI%20KHAIRE%20ELAROSI%20COPYRIGHT%20DECLARATION.pdf text en http://eprints.uthm.edu.my/1991/3/MUWFIK%20FAIDI%20KHAIRE%20ELAROSI%20WATERMARK.pdf Khaire Elarosi, Muwfik Faidi (2013) On the development computer, code for determinig the root of equation for transient flight analysis. Masters thesis, Universiti Tun Hussein Malaysia. |
| spellingShingle | TL Motor vehicles. Aeronautics. Astronautics TL500-777 Aeronautics. Aeronautical engineering Khaire Elarosi, Muwfik Faidi On the development computer, code for determinig the root of equation for transient flight analysis |
| title | On the development computer, code for determinig the root of equation for transient flight analysis |
| title_full | On the development computer, code for determinig the root of equation for transient flight analysis |
| title_fullStr | On the development computer, code for determinig the root of equation for transient flight analysis |
| title_full_unstemmed | On the development computer, code for determinig the root of equation for transient flight analysis |
| title_short | On the development computer, code for determinig the root of equation for transient flight analysis |
| title_sort | on the development computer code for determinig the root of equation for transient flight analysis |
| topic | TL Motor vehicles. Aeronautics. Astronautics TL500-777 Aeronautics. Aeronautical engineering |
| url | 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 |
| work_keys_str_mv | AT khaireelarosimuwfikfaidi onthedevelopmentcomputercodefordeterminigtherootofequationfortransientflightanalysis |