PX4 2.4.8 Autopilot Open Source Flight Controller Specification
PX4 2.4.8 Autopilot Open Source Flight Controller Specification
Microprocessor:
- 32-bit STM32F427 Cortex M4 core with FPU
- 168 MHz / 256 KB RAM / 2 MB Flash
- 32-bit STM32F103 failsafe co-processor
Sensors:
- L3GD20 3-axis 16-bit gyroscope
- LSM303D 3-axis 14-bit accelerometer / magnetometer
- MPU 6000 3-axis accelerometer / gyroscope
- 5611 barometer
Interfaces:
- 5x UART (serial ports), one high-power capable, 2x with HW flow control
- 2x CAN
- S.BUS input and output
- PPM sum signal
- RSSI (PWM or voltage) input
- I2C
- SPI
- 3.3 and 6.6V ADC inputs
- External micro-USB port
Power System:
- Ideal diode controller with automatic failover
- Servo rail high-power (7 V) and high-current ready
- All peripheral outputs over-current protected, all inputs ESD protected
Weight and Dimensions:
Weight: 38g (1.31oz)
Width: 50mm (1.96")
Thickness: 15.5mm (0.61")
Length: 81.5mm (3.21")
GPS Specifications
Velocity Precision: 0.1 m/s
Max Height: 50,000 m
Max Speed: 515 m/s
Max Acceleration: 4 G
Update Rate: 10 Hz
Time to First Fix: Cold start: 26s, Hot start: 1s
Power supply: voltage DC 5V±5%
Diameter: 54 mm / 2.126 inch
Thickness: 15 mm / 0.59 inch
For more details, please visit PX4 2.4.8 Autopilot Open Source Flight Controller for Drone Developers