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Openpilot CC3D Flight Controller

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The flight controller then uses this data to

  • Stabilize the drone: Maintain level flight, correcting for wind, turbulence, and other external factors.
  • Navigate: Follow pre-programmed routes, waypoints, and missions.
  • Respond to user input: Translate manual commands from the remote control into flight actions.
  • Monitor system status: Monitor battery voltage, motor speed, and other vital system parameters.

Key Features

  • Open-source architecture: Allows developers to modify and customize the firmware to suit specific needs.
  • High-performance processing: Utilizes a 32-bit ARM Cortex-M3 processor, ensuring fast and efficient processing of sensor data.
  • Multiple flight modes: Supports various flight modes, including manual, stabilize, altitude, and autonomous modes.
  • Real-time telemetry: Provides real-time data transmission to the ground station, enabling monitoring and analysis of flight performance.
  • Support for multiple sensors: Can integrate with a wide range of sensors, including GPS, barometers, and magnetometers.
  • Customizable: Allows users to tailor the flight controller to their specific needs through parameter adjustments and custom firmware modifications.
  • Robust communication protocols: Supports multiple communication protocols, including serial, I2C, and SPI.
  • Expandable: Can be expanded with additional components, such as GPS modules, accelerometers, and gyroscopes.
The Openpilot CC3D Flight Controller boasts an impressive array of features, including

Technical Specifications

Processor

32-bit ARM Cortex-M3

Clock Speed

72 MHz

Memory

128 KB Flash, 20 KB SRAM

Interfaces

UART, I2C, SPI, ADC, PWM

Weight

Approximately 12 grams

Dimensions

36 mm x 36 mm x 10 mm

Conclusion

The Openpilot CC3D Flight Controller is a powerful, flexible, and highly customizable component, ideal for developers, researchers, and enthusiasts building advanced UAV systems. Its open-source architecture, high-performance processing, and extensive feature set make it an attractive choice for a wide range of applications, from aerial photography to search and rescue operations.

Pin Configuration

  • Openpilot CC3D Flight Controller Pinout Guide
  • The Openpilot CC3D Flight Controller is a popular open-source autopilot system used in unmanned aerial vehicles (UAVs). It features a 35mm x 35mm footprint and is designed to be highly customizable and adaptable to various flight scenarios. The CC3D has a total of 48 pins, which can be divided into several functional groups. Here's a detailed explanation of each pin, grouped by function:
  • Power Pins
  • 1. VIN ( pins 1 and 2 ): Input power supply for the flight controller, typically connected to a battery or power source (7-30V).
  • 2. 3V3 ( pins 3 and 4 ): 3.3V regulated power output for external components (e.g., sensors, GPS modules).
  • 3. 5V ( pins 5 and 6 ): 5V regulated power output for external components (e.g., cameras, LED indicators).
  • Serial Communication Pins
  • 4. UART1_TX ( pin 7 ): Transmit (TX) pin for the first UART port (typically used for serial console or telemetry).
  • 5. UART1_RX ( pin 8 ): Receive (RX) pin for the first UART port.
  • 6. UART2_TX ( pin 9 ): Transmit (TX) pin for the second UART port (typically used for sensors or peripherals).
  • 7. UART2_RX ( pin 10 ): Receive (RX) pin for the second UART port.
  • 8. UART3_TX ( pin 11 ): Transmit (TX) pin for the third UART port (typically used for GPS or other sensors).
  • 9. UART3_RX ( pin 12 ): Receive (RX) pin for the third UART port.
  • I2C Pins
  • 10. I2C_SCL ( pin 13 ): Clock (SCL) pin for the I2C bus.
  • 11. I2C_SDA ( pin 14 ): Data (SDA) pin for the I2C bus.
  • Analog Input Pins
  • 12. A1 ( pin 15 ): Analog input channel 1 (e.g., for sensors, potentiometers, or voltage dividers).
  • 13. A2 ( pin 16 ): Analog input channel 2.
  • 14. A3 ( pin 17 ): Analog input channel 3.
  • 15. A4 ( pin 18 ): Analog input channel 4.
  • Digital Input/Output Pins
  • 16. D1 ( pin 19 ): Digital input/output pin 1 (e.g., for switches, LEDs, or relay controls).
  • 17. D2 ( pin 20 ): Digital input/output pin 2.
  • 18. D3 ( pin 21 ): Digital input/output pin 3.
  • 19. D4 ( pin 22 ): Digital input/output pin 4.
  • 20. D5 ( pin 23 ): Digital input/output pin 5.
  • 21. D6 ( pin 24 ): Digital input/output pin 6.
  • 22. D7 ( pin 25 ): Digital input/output pin 7.
  • 23. D8 ( pin 26 ): Digital input/output pin 8.
  • PWM Output Pins
  • 24. PWM1 ( pin 27 ): Pulse-width modulation (PWM) output 1 (typically used for motor control or servo signals).
  • 25. PWM2 ( pin 28 ): PWM output 2.
  • 26. PWM3 ( pin 29 ): PWM output 3.
  • 27. PWM4 ( pin 30 ): PWM output 4.
  • 28. PWM5 ( pin 31 ): PWM output 5.
  • 29. PWM6 ( pin 32 ): PWM output 6.
  • 30. PWM7 ( pin 33 ): PWM output 7.
  • 31. PWM8 ( pin 34 ): PWM output 8.
  • Other Pins
  • 32. BOOT ( pin 35 ): Boot mode input (pull-up to enable boot mode).
  • 33. Reset ( pin 36 ): Reset input (active-low, pull-down to reset the flight controller).
  • 34. SDCARD_CLK ( pin 37 ): Clock signal for the SD card interface.
  • 35. SDCARD_CMD ( pin 38 ): Command signal for the SD card interface.
  • 36. SDCARD_D0 ( pin 39 ): Data line 0 for the SD card interface.
  • 37. SDCARD_D1 ( pin 40 ): Data line 1 for the SD card interface.
  • 38. SDCARD_D2 ( pin 41 ): Data line 2 for the SD card interface.
  • 39. SDCARD_D3 ( pin 42 ): Data line 3 for the SD card interface.
  • Unused Pins
  • 40. NC ( pins 43-48 ): No connect pins (not connected internally).
  • Connection Structure
  • When connecting the pins, ensure that:
  • Use suitable connectors, such as 0.1" headers or JST-XH connectors, to match the pin pitch and spacing.
  • Implement proper power supply decoupling and filtering to reduce noise and ensure stable operation.
  • Use twisted pair or shielded cables for sensitive signal lines (e.g., UART, I2C, and analog inputs).
  • Route digital signal lines away from power and analog signal lines to minimize interference.
  • Consult the Openpilot CC3D documentation and community resources for specific configuration and connection guidelines for your UAV setup.
  • Remember to handle the flight controller with care, as it is a sensitive electronic device. Always follow proper soldering and assembly techniques to ensure reliable and safe operation.

Code Examples

Openpilot CC3D Flight Controller Documentation
Overview
The Openpilot CC3D Flight Controller is a popular, open-source autopilot system designed for remote-controlled aircraft, drones, and other unmanned aerial vehicles (UAVs). The CC3D board is a compact, feature-rich flight controller that integrates a powerful microcontroller, sensors, and connectivity options to provide a robust and flexible platform for aerial robotics.
Key Features
32-bit STM32F103 microcontroller
 3-axis accelerometer and 3-axis gyroscope
 Barometer and temperature sensors
 uBlox GPS module
 Serial and I2C interfaces for sensor expansion
 USB interface for configuration and firmware updates
 Support for multiple flight modes, including stabilize, acro, and autopilot
Code Examples
### Example 1: Basic Flight Control using C++
This example demonstrates how to use the CC3D Flight Controller to read sensor data and control the motors of a quadcopter.
```c
#include <CC3D.h>
// Define motor pin assignments
#define MOTOR_FRONT_LEFT 1
#define MOTOR_FRONT_RIGHT 2
#define MOTOR_BACK_LEFT 3
#define MOTOR_BACK_RIGHT 4
void setup() {
  // Initialize the CC3D board
  CC3D.init();
  
  // Set up motor pins as outputs
  pinMode(MOTOR_FRONT_LEFT, OUTPUT);
  pinMode(MOTOR_FRONT_RIGHT, OUTPUT);
  pinMode(MOTOR_BACK_LEFT, OUTPUT);
  pinMode(MOTOR_BACK_RIGHT, OUTPUT);
}
void loop() {
  // Read accelerometer and gyroscope data
  int ax, ay, az, gx, gy, gz;
  CC3D.readAccel(ax, ay, az);
  CC3D.readGyro(gx, gy, gz);
  
  // Calculate roll, pitch, and yaw angles from sensor data
  float roll =atan2(ay, az);
  float pitch = atan2(ax, sqrt(ayay + azaz));
  float yaw = gx  0.01; // simple integration of gyroscope data
  
  // Control motor speeds based on desired angles
  int motor_speed_FL = map(roll + pitch, -1000, 1000, 1000, 2000);
  int motor_speed_FR = map(roll - pitch, -1000, 1000, 1000, 2000);
  int motor_speed_BL = map(-roll + pitch, -1000, 1000, 1000, 2000);
  int motor_speed_BR = map(-roll - pitch, -1000, 1000, 1000, 2000);
  
  // Update motor speeds
  analogWrite(MOTOR_FRONT_LEFT, motor_speed_FL);
  analogWrite(MOTOR_FRONT_RIGHT, motor_speed_FR);
  analogWrite(MOTOR_BACK_LEFT, motor_speed_BL);
  analogWrite(MOTOR_BACK_RIGHT, motor_speed_BR);
  
  delay(20);
}
```
### Example 2: GPS-based Autopilot using Python (with Openpilot-Python API)
This example demonstrates how to use the CC3D Flight Controller with GPS data to follow a predefined waypoints using the Openpilot-Python API.
```python
import openpilot
# Initialize the CC3D board and GPS module
op = openpilot.Openpilot()
gps = op.get_gps()
# Define waypoints
waypoints = [
  {"lat": 37.7749, "lon": -122.4194, "alt": 10},
  {"lat": 37.7859, "lon": -122.4364, "alt": 20},
  {"lat": 37.7963, "lon": -122.4573, "alt": 30}
]
while True:
  # Read current GPS location
  gps_data = gps.read()
  lat, lon, alt = gps_data["lat"], gps_data["lon"], gps_data["alt"]
  
  # Calculate distance to next waypoint
  next_waypoint = waypoints[0]
  distance_to_waypoint = openpilot.calculate_distance(lat, lon, next_waypoint["lat"], next_waypoint["lon"])
  
  # If near waypoint, switch to next one
  if distance_to_waypoint < 10:
    waypoints.pop(0)
    if not waypoints:
      break
  
  # Control aircraft to fly towards next waypoint
  op.set_roll(openpilot.calculate_roll(lat, lon, next_waypoint["lat"], next_waypoint["lon"]))
  op.set_pitch(openpilot.calculate_pitch(lat, lon, next_waypoint["lat"], next_waypoint["lon"], alt, next_waypoint["alt"]))
  op.set_throttle(openpilot.calculate_throttle(alt, next_waypoint["alt"]))
  
  # Wait for 1 second
  time.sleep(1)
```
Note: These code examples are simplified and intended to demonstrate the basic functionality of the Openpilot CC3D Flight Controller. In a real-world implementation, you should consider additional error handling, safety features, and tuning of the flight control parameters.