Description:

This research focuses on the development and optimization of a hybrid VTOL aerial vehicle that combines the advantages of fixed-wing and rotorcraft designs. The project will address the mechanical design challenges involved in achieving efficient vertical take-off, stable hover, and smooth transition to forward flight. The low-level control strategies will ensure precise maneuverability and stability during various flight modes, with an emphasis on optimizing the integration of propulsion systems and control surfaces for hybrid operation.

Objectives:

Key skills/interests:

Mathematical modelling, mechanical design, simulation and control design

Expected outputs:

1x MSc (Eng), 1x Journal/Conference paper in a leading publication.

Supervisor:

Arnold Pretorius (UCT)

Sophie Armanini (Imperial College)

Student:

Araav Sojen

Funding: