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🚁 FPV Drone Flight Controller

Dive deep into aerodynamics. Build a flight controller from scratch to stabilize a quadcopter.

📋 Overview

Flight controllers process thousands of calculations per second to keep a drone in the air. You will read receiver inputs, compute the drone's 3D orientation, and drive four Electronic Speed Controllers (ESCs).

What you'll learn: Reading PWM receiver signals via interrupts, mixing thrust for roll/pitch/yaw, and implementing cascaded PID controllers.

Estimated time: 10+ hours. Difficulty: ⭐⭐⭐⭐⭐ Expert.

🧩 Components Needed

ComponentSpecificationQtyNotes
STM32 Blue PillARM Cortex-M31Fast enough for flight loops
MPU60506-DOF IMU1
Brushless MotorsHigh KV4
ESCs30A4Electronic Speed Controllers
RC ReceiverPWM/PPM/SBUS1

📖 Step-by-Step Tutorial

1

Read the Receiver

Use hardware interrupts (or input capture) to read the PWM width of the Throttle, Roll, Pitch, and Yaw channels from your RC receiver.
2

Calibrate ESCs

ESCs need to know the min and max throttle ranges. Write a utility script to send max PWM, wait for the beep, then min PWM.
3

Cascaded PID

Drones use two PID loops per axis: an "Angle" loop (outer) that asks for a specific rotation rate, and a "Rate" loop (inner) that uses the gyro to hit that rate.
4

Motor Mixing

Combine the PID outputs to determine individual motor speeds. E.g. Motor1 = Throttle + PitchPID - RollPID - YawPID.
💡
ALWAYS remove the propellers when testing flight controller code on the bench. Brushless motors can cause serious injury if they spin up unexpectedly.

💻 Code / Configuration

flight_controller.ino
INO
// Flight Controller Motor Mixing (Snippet) - Volt X
int throttle, roll_pid, pitch_pid, yaw_pid;
int motor1, motor2, motor3, motor4;

void calculateMotorPulses() {
  // Motor 1: Front Right (CCW)
  motor1 = throttle - pitch_pid - roll_pid - yaw_pid;
  
  // Motor 2: Rear Right (CW)
  motor2 = throttle + pitch_pid - roll_pid + yaw_pid;
  
  // Motor 3: Rear Left (CCW)
  motor3 = throttle + pitch_pid + roll_pid - yaw_pid;
  
  // Motor 4: Front Left (CW)
  motor4 = throttle - pitch_pid + roll_pid + yaw_pid;
  
  // Constrain outputs to valid ESC PWM range (usually 1000-2000us)
  motor1 = constrain(motor1, 1000, 2000);
  motor2 = constrain(motor2, 1000, 2000);
  motor3 = constrain(motor3, 1000, 2000);
  motor4 = constrain(motor4, 1000, 2000);
  
  // Send pulses to ESCs...
}

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