Holybro Pix32 v5
Last updated
Last updated
:::warning PX4 does not manufacture this (or any) autopilot. Contact the manufacturer for hardware support or compliance issues. :::
Pix32 v5® is an advanced autopilot flight controller designed and made by Holybro®. It is optimized to run on PX4 firmware, which is intended for both academic and commercial developers. It is based on the Pixhawk-project FMUv5 open hardware design and runs PX4 on the NuttX OS. It can be regarded as a variant version of Pixhawk4.
The Pix32 v5 is designed for pilots who need a high power, flexible and customisable flight control system. It is comprised of a separate flight controller and carrier (base) board, which are connected by a 100pin connector. This design allows users to either select a base board made by Holybro, or customize their own.
:::note This flight controller is manufacturer supported. :::
Main 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-20689
Accel/Gyro: BMI055 or ICM20602
Magnetometer: IST8310
Barometer: MS5611
GPS: u-blox Neo-M8N GPS/GLONASS receiver; integrated magnetometer IST8310
Interfaces:
8-16 PWM outputs (8 from IO, 8 from FMU)
3 dedicated PWM/Capture inputs on FMU
Dedicated R/C input for CPPM
Dedicated R/C input for Spektrum / DSM and S.Bus with analog / PWM RSSI input
Dedicated S.Bus servo output
5 general purpose serial ports
2 with full flow control
1 with separate 1.5A current limit
3 I2C ports
4 SPI buses
1 internal high speed SPI sensor bus with 4 chip selects and 6 DRDYs
1 internal low noise SPI bus dedicated for
Barometer with 2 chip selects, no DRDYs
1 internal SPI bus dedicated for FRAM
Supports dedicated SPI calibration EEPROM located on sensor module
1 external SPI buses
Up to 2 CANBuses for dual CAN with serial ESC
Each CANBus has individual silent controls or ESC RX-MUX control
Analog inputs for voltage / current of 2 batteries
2 additional analog inputs
Electrical System:
Power module output: 4.9~5.5V
Max input voltage: 6V
Max current sensing: 120A
USB Power Input: 4.75~5.25V
Servo Rail Input: 0~36V
Weight and Dimensions:
Dimensions: 45x45x13.5mm
Weight: 33.0g
Environmental Data, Quality & Reliability:
Operating temperature: -40 ~ 85°c
Storage temp. -40~85℃
CE
FCC
RoHS compliant (lead-free)
Additional information can be found in the Pix32 V5 Technical Data Sheet.
Order from Holybro website.
The Pix32 v5 Wiring Quick Start provides instructions on how to assemble required/important peripherals including GPS, Power Management Board etc.
Pix32 v5 can be triple-redundant on the power supply if three power sources are supplied. The three power rails are: POWER1, POWER2 and USB.
:::note The output power rails FMU PWM OUT and I/O PWM OUT (0V to 36V) do not power the flight controller board (and are not powered by it). You must supply power to one of POWER1, POWER2 or USB or the board will be unpowered. :::
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)
:::tip Most users will not need to build this firmware! It is pre-built and automatically installed by QGroundControl when appropriate hardware is connected. :::
To build PX4 for this target:
The system's serial console and SWD interface runs on the FMU Debug port
The pinout uses the standard Pixhawk Debug Mini interface defined in the Pixhawk Connector Standard.
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 Airframes Reference.