Design and Performance Evaluation of Thrust Stand for Electric UAV Propulsion Using Brushless DC Motor

Key Points

• The aim is to design a thrust stand and assess its performance for electric UAV propulsion systems using brushless DC motors.
• Designed a thrust stand for testing electric UAV propulsion systems.
• Utilized brushless DC motors in the propulsion system.
• Conducted performance evaluations to measure thrust output and efficiency.
• The thrust stand demonstrated effective measurement of propulsion performance.
• Results indicated improved efficiency and thrust characteristics in electric UAV systems.