Control system development for unconventional aerobatic unmanned aerial vehicle with variable incidence wing
This final year project covers the design and development processes of control system for unconventional unmanned aerial vehicle (UAV). An aerobatic aircraft is designed to be equipped with variable incidence wing with an expectation to be able to perform both conventional aerobatic maneuvers as wel...
| Main Author: | |
|---|---|
| Other Authors: | |
| Format: | Final Year Project (FYP) |
| Language: | English |
| Published: |
2010
|
| Subjects: | |
| Online Access: | http://hdl.handle.net/10356/40046 |