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:

• Design and prototype a hybrid VTOL vehicle capable of both vertical take-off and efficient forward flight.
• Develop low-level control algorithms to ensure stability during transition between hover and forward flight modes.
• Optimize the mechanical structure for weight, durability, and aerodynamic efficiency.
• Test and evaluate the performance of the hybrid VTOL under different operational conditions.
• Implement and validate control strategies to improve energy efficiency and maneuverability across flight modes.
• Write-up of MSc dissertation.

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)

Funding:

Partial bursary funding may be available through an Imperial College grant.