Project Details
Description
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.
| Status | Finished |
|---|---|
| Effective start/end date | 30/09/05 → 30/07/06 |
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