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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| Formato: | Final Year Project (FYP) |
| Idioma: | English |
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Nanyang Technological University
2022
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| Acceso en liña: | https://hdl.handle.net/10356/160155 |