Micro air vehicle performance, stability and control

Project Details


Masters thesis project: aerodynamic and control design and testing towards a functional micro air vehicle testbed. Airframe design, prototyping and wind tunnel testing, control system development using COTS components, integration on RPV testbed, transfer to MAV, mission profile evaluation.
Effective start/end date30/09/0530/07/06


Explore the research topics touched on by this project. These labels are generated based on the underlying awards/grants. Together they form a unique fingerprint.