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Design of flight control system for quad-rotor helicopter based on ARM core microcontroller

  • 2014-03-05
  • 1.41MB
  • Points it Requires : 1

The quadcopter has four propellers arranged in a cross structure. Its unique configuration can meet the mission requirements in complex environments. This paper designs a quadcopter flight control system hardware and software solution. The sensor collects the attitude, altitude, position and other information of the quadcopter in real time, uses the PID algorithm to design the flight control law, and uses the ARM Cortex-M3 core high-performance microcontroller as the main controller. Finally, the ground station software developed by CVI is used to realize online data collection and parameter adjustment, and the feasibility and stability of this solution are verified through actual flight.

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