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DESIGNING FLIGHT CONTROLLER OF QUADCOPTER USING STM32 MICROCONTROLLER.

  • Unique Paper ID: 167412
  • Volume: 11
  • Issue: 3
  • PageNo: 1163-1168
  • Abstract:
  • In order to achieve stable and responsive flight dynamics, designing a quadcopter flight controller with an STM32 microcontroller requires integrating sophisticated control algorithms, sensor fusion techniques, and effective hardware interfacing. This article offers a thorough method for creating and implementing a flight control system that makes use of the STM32 microcontroller, which is renowned for its potent computing capability and fast real-time performance. The choice and integration of sensors for accurate orientation and position monitoring, such as magnetometers, gyroscopes, and accelerometers, are important design elements. Proportional-Integral-Derivative (PID) controllers are among the flight control algorithms that have been fine-tuned for the STM32 architecture to guarantee a prompt and precise reaction to changing flying circumstances. Furthermore covered are the interfaces and communication protocols for telemetry, motor control, and user input. The resultant flight controller proves the STM32 microcontroller's efficacy in UAV applications with its sturdy performance throughout a range of test situations. The development of effective and dependable flight control systems for quadcopters and other unmanned aerial vehicles (UAVs) can benefit greatly from this study.
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Cite This Article

  • ISSN: 2349-6002
  • Volume: 11
  • Issue: 3
  • PageNo: 1163-1168

DESIGNING FLIGHT CONTROLLER OF QUADCOPTER USING STM32 MICROCONTROLLER.

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