Fully 3D-Printed and Assembled

The project focused on understanding aerodynamic principles and flight dynamics, including the implementation of gyro-stabilized flight control systems, improving stability, control accuracy and autonomous flight navigation.

Securing the fuselage together

Wiring of the ESC and testing the Aileron, elevator and Rudder functions of the vehicle

Aiming to have a stable take-off without autopilot or any gyro systems enabled.

Test Flight

During earlier stages of testing

Micro Fixed Wing UAV

Compact and Agile FW - UAV

FW - UAV

Lightweight fixed-wing airframe

Energy-efficient long-range operation

Achievements

Science Exhibhition

1st Place

QNL Exhibhition

Presented by United States Embassy

Presented by the United States Ambassador

Earlier Iterations of the FW-UAV

Future Enhancements

Vision/LIDAR-based tracking and obstacle avoidance

Vision/LIDAR based take-off and landing assistance

VTOL integration, capable of mid flight standby. Which would provide enhanced speed, range and precision

Increased flight time