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CUAV Pixhawk V6X

Product codeCV027
Availability In stock (can be backordered)

$329.00

  • H7 Double-precision floating-point processor
  • High-performance ARM M3 coprocessor
  • Low noise Car-grade IMUs
  • Triple redundant IMUs and dual redundant barometer designs
  • Car-grade RM3100 magnetic compass
  • New built-in shock absorption design
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CUAV Pixhawk V6X Autopilot Flight Controller

Pixhawk V6X® is a new generation of Pixhawk® designed by CUAV and PX4; it is designed based on the Pixhawk FMU V6X standard and pursues ultimate security and stability; it adopts H7 double-precision floating-point arithmetic unit and Cortex®-M3 coprocessor, independent bus and power supply. Three redundant IMU, IMU temperature factory pre-calibration technology, dual redundant barometer design, all-round guarantee of UAV flight safety and rich expansion capabilities; integrated 100M Ethernet PHY, can communicate with the mission computer (Airborne computer), fiber optic inertial navigation, high-end surveying and mapping cameras and other industrial UAV-mounted equipment for high-speed communication, which meets the needs of high-end UAVs.

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Pixhawk V6X Features

  • H7 Double-precision floating-point processor
  • High-performance ARM M3 coprocessor
  • Low-noise Car-grade IMUs.
  • Triple redundant IMUs and dual redundant barometer designs.
  • Car-grade RM3100 magnetic compass
  • New built-in shock absorption design

H7 Double Precision Floating-Point Arithmetic Unit Processor

Using STM32H753IIK6 processor, double precision floating point arithmetic unit (DSP&FPU), the main frequency up to 480MHz; 2M FLASH,1 MB RAM; For flight controller to bring powerful computing power, rapid data processing ability, for more functional development and flight stability to provide more possibilities.

M3 Coprocessor to Enhance the Expansion Capacity

The high performance ARM® Cortex®-M3 coprocessor adds more security and external scalability capabilities to UAVs

Multiple Redundancy Design Ensures Flight Safety

With three redundant IMUs and two redundant barometers on separate buses, when one set of IMUs fails, the system seamlessly switches to another reliable IMU, making the flight safer.

Integrated 100M Ethernet Interface

High-speed communication with task computers through Ethernet; In the future, high-end links, INS and high-end mapping cameras can be connected through Ethernet to meet the needs of high-end UAVs

Adapt to More Complex Magnetic Environments

In order to adapt to the complex magnetic field environment, the RM3100 magnetic compass is selected, which supports the GPS direction finding function, and completely solves the trouble of magnetic compass interference

Pixhawk V6X Autopilot Flight Controller Modular Design

The V6X adopts a modular design, and the core module contains the processor and all IMUs. Users can design their own baseboard according to the design reference, to meet the personalized customization needs.

Compatibility with PX4/ArduPilot All Models

CUAV Pixhawk V6X supports all models for PX4&ArduPilot firmware,3-8 Copter/Plane/Helicopter/VTOL/unmanned vehicle/Rover, etc.

Implement Open Source Standard, Enrich Open Source Ecosystem

As a professional drone accessories supplier, besides the CUAV Pixhawk V6X flight controller, we also have other drone accessories on sale. Visit World Drone Market to get CUAV GPS to pair with The CUAV Pixhawk V6X.

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Weight 0.6 kg

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Pixhawk V6X Specification
Hardware Standard Pixhawk FMUv6x Standard DS-010 Pixhawk AutoPilot Bus Standard DS-012 Pixhawk AutoPilot V6X Standard
Processor STM32H753IIK6 32-bit Arm® Cortex®-M7 480MHz MCUs, 2MB Flash,1MB RAM
Coprocessor STM32F10X
Accelerometer&Gyroscope ICM42688-P ICM-20649 BMI088
Compass RM3100
Barometer 2×ICP-20100
Interfaces
PWM I/O 16
Power 4 2 for UAVCAN,2 for SMBUS (I2C)
GPS 2 1 GPS port with I2C and safety switch (GPS1) 1 interface with I2C and GPS (GPS2)
TELEM 3
CAN 2
PPM RC 1 for PPM receiver
SBUS/DSM/RSSI 1 for SBUS/DSM/Spektrum in and Analog (3.3V)/PWM input
SBUS outs 1
FMU Debug 1
IO Debug 1
Ethernet 1
SPI EXTERNAL1 1 (SPI6 interface,for expanding external sensors)
ADIO 1 AD3.3/ADC6.6
UART4 1
USB 2 1 for Type C 1 for GH interface USB
TF Slot 1
Physical characteristics
Operating voltage 4.75~5.45V
Servo input voltage 0~9.9V
Operating temperature -20~85
Size 45×90×33.2mm
Weight 98g

Size

Flight control CORE

Pinouts

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