In-flight simulation of tilt-rotor VTOL UAV using open loop wind tunnel
This project covers the design of a TRUAV, its integration with the windshaper open loop wind tunnel and the characterisation of the UAV’s dynamics. Following that, these readings would be used to help develop a controller using the tilt corridor method that would be used to control the UAV durin...
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Nanyang Technological University
2022
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| Online Access: | https://hdl.handle.net/10356/160155 |
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sg-ntu-dr.10356-1601552023-03-04T20:19:38Z In-flight simulation of tilt-rotor VTOL UAV using open loop wind tunnel Wong, Amos Timothy Jun Han Mir Feroskhan School of Mechanical and Aerospace Engineering mir.feroskhan@ntu.edu.sg Engineering::Aeronautical engineering::Flight simulation Engineering::Aeronautical engineering::Aircraft This project covers the design of a TRUAV, its integration with the windshaper open loop wind tunnel and the characterisation of the UAV’s dynamics. Following that, these readings would be used to help develop a controller using the tilt corridor method that would be used to control the UAV during the transition phase of flight. Bachelor of Engineering (Aerospace Engineering) 2022-07-14T05:07:38Z 2022-07-14T05:07:38Z 2022 Final Year Project (FYP) Wong, A. T. J. H. (2022). In-flight simulation of tilt-rotor VTOL UAV using open loop wind tunnel. Final Year Project (FYP), Nanyang Technological University, Singapore. https://hdl.handle.net/10356/160155 https://hdl.handle.net/10356/160155 en A122 application/pdf Nanyang Technological University |
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Singapore Singapore |
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Engineering::Aeronautical engineering::Flight simulation Engineering::Aeronautical engineering::Aircraft |
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Engineering::Aeronautical engineering::Flight simulation Engineering::Aeronautical engineering::Aircraft Wong, Amos Timothy Jun Han In-flight simulation of tilt-rotor VTOL UAV using open loop wind tunnel |
| description |
This project covers the design of a TRUAV, its integration with the windshaper open
loop wind tunnel and the characterisation of the UAV’s dynamics. Following that, these
readings would be used to help develop a controller using the tilt corridor method that
would be used to control the UAV during the transition phase of flight. |
| author2 |
Mir Feroskhan |
| author_facet |
Mir Feroskhan Wong, Amos Timothy Jun Han |
| format |
Final Year Project |
| author |
Wong, Amos Timothy Jun Han |
| author_sort |
Wong, Amos Timothy Jun Han |
| title |
In-flight simulation of tilt-rotor VTOL UAV using open loop wind tunnel |
| title_short |
In-flight simulation of tilt-rotor VTOL UAV using open loop wind tunnel |
| title_full |
In-flight simulation of tilt-rotor VTOL UAV using open loop wind tunnel |
| title_fullStr |
In-flight simulation of tilt-rotor VTOL UAV using open loop wind tunnel |
| title_full_unstemmed |
In-flight simulation of tilt-rotor VTOL UAV using open loop wind tunnel |
| title_sort |
in-flight simulation of tilt-rotor vtol uav using open loop wind tunnel |
| publisher |
Nanyang Technological University |
| publishDate |
2022 |
| url |
https://hdl.handle.net/10356/160155 |
| _version_ |
1759853935538995200 |