Design of Transition Mode Control System of Tilt-Wing UAV
Tilt-Wing UAV (Unmanned Aerial Vehicle) is a type of aircraft which has wing that can be rotated. The tilt-wing mechanism is implemented to increase the performance of the aircraft. This aircraft is capable of doing vertical take-off and landing (VTOL) like a helicopter and flying horizontally like...
Saved in:
| Main Author: | |
|---|---|
| Format: | Final Project |
| Language: | Indonesia |
| Online Access: | https://digilib.itb.ac.id/gdl/view/21219 |
| Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
| Institution: | Institut Teknologi Bandung |
| Language: | Indonesia |
Be the first to leave a comment!