Fault Analysis and Controlling in Drone Control System

Authors

  • Nutan Dattaray Waghmode UG Student, Department of Electrical Engineering, Jaywant College of Engineering and Polytechnic Killemachindragad, India
  • Shivram Shankar Dhanavade UG Student, Department of Electrical Engineering, Jaywant College of Engineering and Polytechnic Killemachindragad, India
  • Sanket Ananda Uthale UG Student, Department of Electrical Engineering, Jaywant College of Engineering and Polytechnic Killemachindragad, India
  • Sanjay Soma Palkar UG Student, Department of Electrical Engineering, Jaywant College of Engineering and Polytechnic Killemachindragad, India

Keywords:

Fault analysis, Drone control system

Abstract

The most common use of motors for drones and unmanned aerial vehicles (UAVs) is to spin the propellers of multi-rotor drones so they can fly. Any aircraft or flying machine operated without a human pilot is called an unmanned aerial vehicle (UAV). Drone engines can also be found in other unmanned vehicle subsystems, such as camera and payload gimbals, flight surfaces, antenna rotators, and landing gear. The drive system of electric cars uses different electric motors. The performance of brushed direct current (DC) motors, induction motors, switched reluctance motors and brushless DC (BLDC) motors is compared according to the requirements of in-wheel motor technology under normal and critical conditions through simulation. This study shows that BLDC motors are the most suitable electric motor for a high-performance drone motor system. To investigate BLDC motor performance under different control algorithms, an accurate motor model is required.

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Published

22-05-2023

Issue

Section

Articles

How to Cite

[1]
N. D. Waghmode, S. S. Dhanavade, S. A. Uthale, and S. S. Palkar, “Fault Analysis and Controlling in Drone Control System”, IJRESM, vol. 6, no. 5, pp. 104–106, May 2023, Accessed: Oct. 11, 2024. [Online]. Available: https://journal.ijresm.com/index.php/ijresm/article/view/2705