Please use this identifier to cite or link to this item: https://hdl.handle.net/10356/160155
Title: In-flight simulation of tilt-rotor VTOL UAV using open loop wind tunnel
Authors: Wong, Amos Timothy Jun Han
Keywords: Engineering::Aeronautical engineering::Flight simulation
Engineering::Aeronautical engineering::Aircraft
Issue Date: 2022
Publisher: Nanyang Technological University
Source: 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
Project: A122
Abstract: 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.
URI: https://hdl.handle.net/10356/160155
Schools: School of Mechanical and Aerospace Engineering 
Fulltext Permission: restricted
Fulltext Availability: With Fulltext
Appears in Collections:MAE Student Reports (FYP/IA/PA/PI)

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