In-flight simulation of tilt-rotor VTOL UAV using open loop wind tunnel

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...

Full description

Bibliographic Details
Main Author: Wong, Amos Timothy Jun Han
Other Authors: Mir Feroskhan
Format: Final Year Project (FYP)
Language:English
Published: Nanyang Technological University 2022
Subjects:
Engineering::Aeronautical engineering::Flight simulation
Engineering::Aeronautical engineering::Aircraft
Online Access:https://hdl.handle.net/10356/160155

Internet

https://hdl.handle.net/10356/160155

Similar Items