An analytical design-optimization method for electric propulsion systems of multicopter UAVs with desired hovering endurance

X Dai, Q Quan, J Ren, KY Cai - IEEE/ASME Transactions on …, 2019 - ieeexplore.ieee.org
Multicopters are becoming increasingly important both in civil and military fields. Currently,
most multicopter propulsion systems are designed by experience and trial-and-error …

Innovative scaled test platform e-genius-mod—scaling methods and systems design

DP Bergmann, J Denzel, A Baden, L Kugler… - Aerospace, 2019 - mdpi.com
Future aircraft design highly depends on the successful implementation of new
technologies. However, the gap between conventional designs and new visions often …

Electric propulsion system optimization for long-endurance and solar-powered unmanned aircraft

OD Dantsker, M Caccamo… - 2019 AIAA/IEEE Electric …, 2019 - ieeexplore.ieee.org
The increase in popularity of unmanned aerial vehicles (UAVs) has been driven by their use
in civilian, education, government, and military applications. However, limited on-board …

Improving prediction capability of quadcopter through digital twin

HY Jeon, C Justin, DN Mavris - AIAA Scitech 2019 Forum, 2019 - arc.aiaa.org
In the quest to reduce performance uncertainties and improve our understanding of complex
system-of-systems, the concepts of digital engineering and digital twin have been proposed …

Drone propeller noise under static and steady inflow conditions

C Doolan, Y Yauwenas, D Moreau - … on Flow Induced Noise and Vibration …, 2019 - Springer
Drone propeller noise under static and steady inflow conditions has been studied. A
numerical model that couples a blade element momentum theory model with a frequency …

Coupled Analysis for 6-DOF Dynamics of UAV and Modified Blade Element Momentum Theory considering Gust and Flight Conditions

박선후 - 2019 - s-space.snu.ac.kr
New industries such as reconnaissance, surveillance, and courier services are attracting
attention as demand and supply of unmanned aerial vehicles increase. Accordingly, many …

[PDF][PDF] Design and Structural Analysis of Propeller Blade for High Altitude Search and Rescue Unmanned Aerial Vehicle

C Dahal, HB Dura, L Poudel - Proceedings of IOE Graduate …, 2019 - researchgate.net
The commercially available UAV are designed for sea level altitude range thus they are not
good enough for high altitude search and rescue flight. The objective of this research is to …