Holybro Pixhawk 5X (FMUv5X)
Last updated
Last updated
:::warning PX4 does not manufacture this (or any) autopilot. Contact the for hardware support or compliance issues. :::
Pixhawk 5X® is the latest update to the successful family of Pixhawk® flight controllers designed and made in collaboration with Holybro® and the PX4 team.
It is based on the , , and . It comes with the latest PX4 Autopilot​® pre-installed, triple redundancy, temperature-controlled, isolated sensor domain, delivering incredible performance and reliability.
Inside the Pixhawk® 5X, you can find an STMicroelectronics® based STM32F7, paired with sensor technology from Bosch®, InvenSense®, giving you flexibility and reliability for controlling any autonomous vehicle, suitable for both academic and commercial applications. The Pixhawk® 5X’s F7 microcontroller has 2MB flash memory and 512KB RAM. The PX4 Autopilot takes advantage of the increased power and RAM. Thanks to the updated processing power, developers can be more productive and efficient with their development work, allowing for complex algorithms and models.
The FMUv5X open standard includes high-performance, low-noise IMUs on board, designed for better stabilization. Triple redundant IMU & double redundant barometer on separate buses. When the PX4 Autopilot detects a sensor failure, the system seamlessly switches to another to maintain flight control reliability.
An independent LDO powers every sensor set with independent power control. A newly designed vibration isolations to filter out high-frequency vibration and reduce noise to ensure accurate readings, allowing vehicles to reach better overall flight performances. External sensor bus (SPI5) has two chip select lines and data-ready signals for additional sensors and payload with SPI-interface, and with an integrated Microchip Ethernet PHY (LAN8742AI-CZ-TR), high-speed communication with mission computers via ethernet is now supported. Two smart battery monitoring ports (SMBus), support for INA226 SMBus Power module.
The Pixhawk® 5X is perfect for developers at corporate research labs, startups, academics (research, professors, students), and commercial application.
Modular flight controller
separated IMU, FMU, and Base system connected by a 100-pin & a 50-pin Pixhawk® Autopilot Bus connector, designed for flexible and customizable systems
Redundancy
3x IMU sensors & 2x Barometer sensors on separate buses, allowing parallel and continuous operation even in the event of a hardware failure
Triple redundancy domains
Completely isolated sensor domains with separate buses and separate power control
Temperature-controlled IMUs
Onboard IMU heating resistors, allowing optimum working temperature of IMUs
Vibration isolation system
Newly designed system to filter out high frequency vibration and reduce noise to ensure accurate readings
Ethernet interface
For high-speed mission computer integration
Automated sensor calibration eliminating varying signals and temperature
Two smart batteries monitoring on SMBus
Additional GPIO line and 5V for the external NFC reader
Secure element for secure authentication of the drone (SE050)
FMU Processor: STM32F765
32 Bit Arm® Cortex®-M7, 216MHz, 2MB memory, 512KB RAM
IO Processor: STM32F100
32 Bit Arm® Cortex®-M3, 24MHz, 8KB SRAM
On-board Sensors:
Accel/Gyro: ICM-20649
Accel/Gyro: ICM-42688P
Accel/Gyro: ICM-20602
Magnetometer: BMM150
Barometer: 2x BMP388
Interfaces
16- PWM servo outputs
R/C input for Spektrum / DSM
Dedicated R/C input for PPM and S.Bus input
Dedicated analog / PWM RSSI input and S.Bus output
4 general purpose serial ports
3 with full flow control
1 with separate 1.5A current limit
1 with I2C and additional GPIO line for external NFC reader
2 GPS ports
1 full GPS & Safety Switch Port
1 basic GPS port
1 I2C port
1 Ethernet port
Transformerless Applications
100Mbps
1 SPI bus
2 chip select lines
2 data-ready lines
1 SPI SYNC line
1 SPI reset line
2 CAN Buses for CAN peripheral
CAN Bus has individual silent controls or ESC RX-MUX control
2 Power input ports with SMBus
1 AD & IO port
2 additional analog input
1 PWM/Capture input
2 Dedicated debug and GPIO lines
Voltage Ratings
Max input voltage: 6V
USB Power Input: 4.75~5.25V
Servo Rail Input: 0~36V
Dimensions
Flight Controller Module: 38.8 x 31.8 x 14.6mm
Standard Baseboard: 52.4 x 103.4 x 16.7mm
Weight
Flight Controller Module: 23g
Standard Baseboard: 51g
Other Characteristics:
Operating & storage temperature: -40 ~ 85°c
:::note Connector pin assignments are left to right (i.e. Pin 1 is the left-most pin). :::
Notes:
USART1
/dev/ttyS0
GPS
USART2
/dev/ttyS1
TELEM3
USART3
/dev/ttyS2
Debug Console
UART4
/dev/ttyS3
UART4 & I2C
UART5
/dev/ttyS4
TELEM2
USART6
/dev/ttyS5
PX4IO/RC
UART7
/dev/ttyS6
TELEM1
UART8
/dev/ttyS7
GPS2
Normal Operation Maximum Ratings
Under these conditions all power sources will be used in this order to power the system:
POWER1 and POWER2 inputs (4.9V to 5.5V)
USB input (4.75V to 5.25V)
Absolute Maximum Ratings
Under these conditions the system will not draw any power (will not be operational), but will remain intact.
POWER1 and POWER2 inputs (operational range 4.1V to 5.7V, 0V to 10V undamaged)
USB input (operational range 4.1V to 5.7V, 0V to 6V undamaged)
Servo input: VDD_SERVO pin of FMU PWM OUT and I/O PWM OUT (0V to 42V undamaged)
Voltage monitoring
:::note Analog battery monitoring via an ADC is not supported on this particular board, but may be supported in variations of this flight controller with a different baseboard. :::
:::tip Most users will not need to build this firmware! It is pre-built and automatically installed by QGroundControl when appropriate hardware is connected. :::
1 (red)
Vtref
+3.3V
2 (blk)
Console TX (OUT)
+3.3V
3 (blk)
Console RX (IN)
+3.3V
4 (blk)
SWDIO
+3.3V
5 (blk)
SWCLK
+3.3V
6 (blk)
SWO
+3.3V
7 (blk)
NFC GPIO
+3.3V
8 (blk)
PH11
+3.3V
9 (blk)
nRST
+3.3V
10 (blk)
GND
GND
For information about using this port see:
:::tip This autopilot is by the PX4 maintenance and test teams. :::
Order from .
The provides instructions on how to assemble required/important peripherals including GPS, Power Module etc.
The (PI0) is pin 2 on the AD&IO port, marked above as FMU_CAP1.
Pixhawk 5X pinouts can be downloaded in PDF from from or .
Pixhawk 5X can be triple-redundant on the power supply if three power sources are supplied. The three power rails are: POWER1, POWER2 and USB. The POWER1 & POWER2 ports on the Pixhawk 5X uses the 6 circuit .
Digital I2C battery monitoring is enabled by default (see ).
To for this target:
The and run on the FMU Debug port.
The pinouts and connector comply with the interface defined in the interface (JST SM10B connector).
(Note, the FMU console maps to USART3).
Any multicopter / airplane / rover or boat that can be controlled with normal RC servos or Futaba S-Bus servos. The complete set of supported configurations can be seen in the .
(Holybro)
(Holybro)
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