Design and Development of Quadcopter

Authors

  • Deo Raj Biswa Jigme Namgyel Engineering College, Royal University of Bhutan
  • Dawa Tshering Jigme Namgyel Engineering College, Royal University of Bhutan
  • Tshering Dargay Jigme Namgyel Engineering College, Royal University of Bhutan
  • Tandin Wangchuk Jigme Namgyel Engineering College, Royal University of Bhutan
  • Bir Bahadur Duklung Rai Jigme Namgyel Engineering College, Royal University of Bhutan
  • Dechen Dorji Jigme Namgyel Engineering College, Royal University of Bhutan
  • Bir Bahadur Rai Jigme Namgyel Engineering College, Royal University of Bhutan
  • Dechen Dorji Jigme Namgyel Engineering College, Royal University of Bhutan

Keywords:

UAV, quadcopter, BLDC motor, Electronics Speed Controller, Technology

Abstract

This project basically deals with the design and development of a quadcopter using a readily available flight controller which has inbuilt and integrated components such as an inertial measurement unit (IMU). These Sensors are crucial for developing any drones as they provide data related to acceleration, gyroscope, and magnetometer which plays a vital role in obtaining drones orientation, angular velocity, and acceleration, and maintaining stability and control. A lithium polymer battery, which provides high current density and has a capacity of 11 powers, the quadcopter.1V and a discharge capacity of about 66A.

Author Biography

Deo Raj Biswa, Jigme Namgyel Engineering College, Royal University of Bhutan

Lecturer, Electronics and Communication Engineering, Jigme Namgyel Engineering College, Royal University of Bhutan

Downloads

Published

2025-02-28

How to Cite

Raj Biswa, D., Tshering, D., Dargay, T., Wangchuk, T., Rai, B. B. D., Dorji, D., … Dorji, D. (2025). Design and Development of Quadcopter. JNEC Thruel Rig Sar Toed , 7(1), 59–70. Retrieved from https://trst.jnec.edu.bt/index.php/thruelrigsartoed/article/view/41