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Design of a Quadcopter to Inspect the Power Transmission Lines

Transmission Lines Insection using Quadcopter / Drone by Muhammad Hassaan Electrical Engineer

1. Project Description

This project focuses on the design and development of a quadcopter system tailored for transmission line inspection. The quadcopter integrates a lightweight airframe, brushless DC motors, ESCs, and a DJI Naza-M Lite flight controller to ensure stable flight performance. Equipped with an onboard camera, the system enables real-time monitoring and detection of faults such as damaged insulators and corroded conductors. By combining aerial mobility with visual inspection capability, the project demonstrates a cost-effective and reliable alternative to traditional manual inspection methods, with scope for future scalability through AI-based fault detection, and autonomous navigation

2. Objectives

  • To design a stable quadcopter capable of monitoring high-voltage transmission lines

  • To detect wire breaks and insulator faults

  • To observe corrosion under insulators and rust on metallic components

3. System Design & Methodology

3.1 Mechanical Design

  • F450 Quadcopter Frame

The DJI F450 is a durable, lightweight quadcopter frame constructed from glass fiber and nylon-reinforced arms for extra strength. Its integrated PCB allows direct soldering of the ESCs, eliminating the need for a separate power distribution board. The design supports up to 4 motors, ensures stable flight, and provides flexible mounting for flight controllers, batteries, and sensors.

F450 Quadcopter Frame used in Transmission Line Inspection using Quadcopter Project by Muhammad Hassaan (Electrical Engineer)
  • 1045 Propeller

The 1045 propeller is made of ABS, offering a lightweight and durable design, and is employed in this project. With a 10-inch diameter and 4.5-inch pitch, it provides efficient thrust and stable flight. Its angled tips reduce air turbulence, improving aerodynamic performance and flight stability.

1045 Propeller used in Transmission Line Inspection using Quadcopter Project by Muhammad Hassaan (Electrical Engineer)

F450 Quadcopter Frame

1045 Propellers

PMU used in Transmission Line Inspection using Quadcopter Project by Muhammad Hassaan (Electrical Engineer)

3.2 Electrical & Electronic System

  • A2212/13T 1000KV Brushless DC Motor

The A2212/13T is a high-efficiency brushless outrunner motor designed for quadcopters and multirotor. Operating at 1000KV (RPM/Volt), it delivers reliable thrust and smooth performance with 8–10 inch propellers, making it ideal for medium-sized drones. It pairs effectively with the F450 frame and 30A ESCs for stable flight and power efficiency.
 

Key Specifications:

  • KV Rating: 1000 RPM/V

  • Max Thrust: Approximately 900 grams

  • Efficiency: ~80%

  • Operating Current: 4–10 A (typical)

  • Max Current Capacity: 12 A (≤60s)

  • Voltage Range: 7–12 V

Brushless DC motor used in Transmission Line Inspection using Quadcopter Project by Muhammad Hassaan (Electrical Engineer)
  • Electronic Speed Controller (ESC)

The 30A ESC is used for this quadcopter, ensuring smooth and responsive motor control for stable flight performance. It supports brushless motors with current demands up to 30A and operates efficiently with 2S–3S LiPo batteries. An integrated 5V/2A BEC provides regulated power for the flight controller and onboard modules, simplifying setup and wiring.

Electronic Speed Controller used in Transmission Line Inspection using Quadcopter Project by Muhammad Hassaan (Electrical Engineer)
  • Power Management Unit (PMU)

The DJI Naza-M Lite Power Management Unit (PMU) is designed to supply a stable 5V output at up to 3A for flight control systems. It operates with a wide input voltage range of 7.4–22.2V (2–6S LiPo), ensuring reliable power delivery to the controller and connected modules.

  • Li- Po Battery

3 Cells (3S) 11.1V 5200mAh Lithium-Polymer Battery is used to power the whole system. 

3 Cells (3S) 11.1V 5200mAh Li-Po Battery used in Transmission Lines Inepction using Quadcopter Project by Muhammad Hassaan - Electrical Engineer

Power Management Unit (PMU)

Electronic Speed Controller

Brushless DC Motor

3 Cells (3S) 11.1V 5200mAh Lithium-Polymer Battery

3.3 Flight Controller & Navigation

  • DJI NAZA-M LITE

  • Integrates 3-axis gyroscope, accelerometer, and barometer for stable flight.

  • Supports Manual, Atti, and GPS Atti modes with intelligent switching.

  • GPS module enables precise position hold, return-to-home, and hovering (±0.8 m vertical, ±2.5 m horizontal).

  • Voltage input: Main Controller 4.8–5.5 V; VU input 7.2–26.0 V (2S–6S LiPo).

  • Includes low-voltage protection, failsafe, motor arm/disarm, and S-Bus/PPM receiver support.

DJI NAZA-M LITE FLIGHT CONTROLLER  used in Quadcopter Project by Muhammad Hassaan (Electrical Engineer)
  • RC Transmitter & Receiver

The Flysky FS-i6 is a 6-channel 2.4 GHz radio transmitter with the FS-iA6B receiver, used in this project. It operates on the AFHDS 2A protocol, providing reliable control with a range of up to 1000 meters in open space. It also supports telemetry feedback for monitoring key flight parameters (such as battery voltage) via the receiver.

Flysky FS-i6 6-channel 2.4 GHz radio transmitter & FS-iA6B receiver used in Quadcopter Project by Muhammad Hassaan (Electrical Engineer)
Flysky FS-i6 6-channel 2.4 GHz radio transmitter & FS-iA6B receiver used in Quadcopter Project by Muhammad Hassaan (Electrical Engineer)

DJI NAZA-M Lite Flight Controller

Flysky FS-i6 6-channel 2.4 GHz radio transmitter & FS-iA6B receiver

3.4 System Integration Diagram

Overall system architecture showing interconnection of all components design by Muhammad Hassaan Electrical Engineer

Overall system architecture showing interconnection of all components

3.5 Methodology

The operational methodology of the quadcopter integrates its mechanical structure, electronic subsystems, and control architecture into a synchronized process. Upon powering the system with a Li-Po battery, the Power Management Unit (PMU) regulates the voltage to safely supply the DJI Naza-M Lite flight controller. The controller initializes by receiving pilot input signals from the transmitter via the paired receiver module.

The flight controller processes these inputs along with onboard sensor data (gyroscope, accelerometer, GPS) and translates them into precise motor commands. Electronic Speed Controllers (ESCs) then regulate the BLDC motors, adjusting the thrust of each propeller to maintain stability and maneuverability.

Navigation is achieved through GPS-assisted stabilization, enabling both manual and semi-autonomous flight (e.g. waypoint following, sensor-based adjustments). The system ensures fail-safes such as automatic return-to-home in case of signal loss. For inspection purposes, a mounted high-resolution camera provides real-time video transmission, allowing monitoring of transmission lines, detection of wire breaks, insulator faults, and early signs of corrosion.

Detailed wiring diagram showing the interconnections of the DJI Naza-M Lite flight controller with ESCs, BLDC motors, receiver, PMU, and 3S Li-Po battery for quadcopter operation design by Muhammad Hassaan Electrical Engineer

Detailed wiring diagram showing the interconnections of the DJI Naza-M Lite flight controller with ESCs, BLDC motors, receiver, PMU, and 3S Li-Po battery for quadcopter operation

Quadcopter fully assembled with frame, BLDC motors, propellers, flight controller, ESCs, and  Li-Po battery used in Quadcopter Project by Muhammad Hassaan (Electrical Engineer)

Quadcopter fully assembled with frame, BLDC motors, propellers, flight controller, ESCs, and

Li-Po battery

Quadcopter inspects 3-Phase Transmission Lines used in Quadcopter Project by Muhammad Hassaan (Electrical Engineer)
Quadcopter inspects 3-Phase Transmission Lines used in Quadcopter Project by Muhammad Hassaan (Electrical Engineer)

Quadcopter inspects 3-Phase Transmission Lines

Watch Demonstration Video

4. Implementation

The implementation of the quadcopter system was carried out in three major stages, ensuring that mechanical, electrical, and software aspects were properly integrated for stable and reliable operation.

Stage 1: Mechanical Assembly

All primary components were mounted on the DJI F450 frame. The brushless DC motors were installed on each arm using vibration-resistant mounts, followed by the attachment of propellers. The landing gear, power distribution board, and mounting platforms for the flight controller and Li-Po battery were also secured to ensure balanced weight distribution.

Initial assembly of quadcopter components on the F450 frame used in Quadcopter Project by Muhammad Hassaan (Electrical Engineer)

Initial assembly of quadcopter components on the F450 frame

Stage 2: Electrical Integration & Calibration

Electrical connections were established between the ESCs, motors, and power management system. The 3S Li-Po battery was interfaced through the PMU module, regulating the supply to the flight controller. The transmitter was paired with its receiver module to establish communication, followed by calibration of the ESCs and motor synchronization. Proper wire routing was implemented to minimize electromagnetic interference and maintain airflow.

Detailed wiring diagram showing the interconnections of the DJI Naza-M Lite flight controller with ESCs, BLDC motors, receiver, PMU, and 3S Li-Po battery for quadcopter operation used in Quadcopter Project by Muhammad Hassaan (Electrical Engineer)

Detailed wiring diagram showing the interconnections of the DJI Naza-M Lite flight controller with ESCs, BLDC motors, receiver, PMU, and 3S Li-Po battery for quadcopter operation

Stage 3: Flight Controller Programming

The DJI Naza-M Lite flight controller was configured using the DJI Naza Assistant software. Sensor calibration (accelerometer, compass, and gyroscope) was performed, and control parameters were fine-tuned. Motor mixing was set according to quadcopter geometry, and PID values were adjusted to achieve stability. GPS calibration was also carried out for enhanced flight accuracy. Final validation tests ensured correct mapping of transmitter input channels to the corresponding motor outputs.

DJI Naza-M Lite Assistant software interface for flight controller configuration and calibration used in Quadcopter Project by Muhammad Hassaan (Electrical Engineer)
DJI Naza-M Lite Assistant software interface for flight controller configuration and calibration used in Quadcopter Project by Muhammad Hassaan (Electrical Engineer)

DJI Naza-M Lite Assistant software interface for flight controller configuration and calibration

5. Results & Achievements

5.1 Flight Performance

  • Achieved stable hover and controlled flight for ~10 minutes using a 3S 5200mAh Li-Po battery.

  • Smooth response to pilot commands through FlySky i6 transmitter.

  • Reliable GPS hold and return-to-home functions via DJI Naza-M Lite controller.

Quadcopter performing stable outdoor flight test during field implementation used in Quadcopter Project by Muhammad Hassaan (Electrical Engineer)

Quadcopter performing stable outdoor flight test during field implementation

5.2 Inspection Capability

  • Successfully captured live video feed of overhead transmission lines.

  • Clear visibility of insulator conditions and conductor alignment during flight.

Detected insulator damage during quadcopter transmission line inspection used in Quadcopter Project by Muhammad Hassaan (Electrical Engineer)

Detected insulator damage during quadcopter transmission line inspection

Identification of rust and conductor degradation captured through aerial inspection used in Quadcopter Project by Muhammad Hassaan (Electrical Engineer)

Identification of rust and conductor degradation captured through aerial inspection

5.3 System Reliability

  • All onboard electronics (ESCs, motors, and PMU) functioned consistently under load.

  • Quadcopter maintained stability even under mild wind conditions

Demonstration of system reliability: quadcopter maintains controlled flight near transmission infrastructure used in Quadcopter Project by Muhammad Hassaan (Electrical Engineer)

Demonstration of system reliability: quadcopter maintains controlled flight near transmission infrastructure

5.4 Achievements

  • Demonstrated practical application of UAVs in power line monitoring.

  • Showcased integration of electrical and control engineering principles in a real-world system.

  • Opened opportunities for further research in autonomous UAV-based inspection

6. Future Improvements

  • AI-Based Fault Detection

Integration of machine learning algorithms to automatically identify faults such as cracked insulators, corrosion, or conductor damage from live video feeds.

  • Extended Battery Life

Employing higher-capacity Li-Po batteries or hybrid power systems to increase flight duration beyond current limits.

  • GPS-Based Autonomous Path Planning

Implementation of waypoint navigation and return-to-home features for fully autonomous inspection missions with minimal human intervention.

7. Conclusion

The developed quadcopter system successfully demonstrated its capability for reliable inspection of high-voltage transmission lines. With stable flight performance, real-time video transmission, and effective identification of faults such as damaged insulators and corroded conductors, the system proved its potential as a practical tool for modern power system monitoring.

The results highlight the reliability of the onboard electronics, flight stability under environmental conditions, and adaptability for inspection tasks. With future improvements such as AI-driven fault detection, extended flight time, and autonomous GPS-based navigation, this platform can evolve into a fully autonomous and scalable solution for large-scale transmission line inspections.

 

Designed & Developed by Muhammad Hassaan 

 

© 2025 Muhammad Hassaan. All rights reserved.
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