Technical Paper
Design, Manufacturing and Testing of a Long Endurance UAV - Effect of Control Simulations
2015-09-22
2015-36-0364
The design is based on a tailless, staggered tandem wing configuration, with a carbon fiber frame and electric propulsion. The developed aircraft has a maximum weight of 12.5 kg, well within the 25 kg limit outlined by Transport Canada for permission-free operation.