Skip to content

NXP MR-VMU-RT1176 Flight Controller

PX4 v1.15

WARNING

PX4 does not manufacture this (or any) autopilot. Contact the manufacturer for hardware support (https://community.nxp.com/) or compliance issues.

The MR-VMU-RT1176 reference design is based on the Pixhawk® FMUv6X-RT open standard, the latest update to the successful family of Pixhawk® flight controllers.

This is NXP's open source reference design for using FMUv6X-RT, and was designed and made in collaboration with industry partners®, NXP's mobile robotics team and the PX4 team. As a reference/evaluation design, it is intended to be replicated, modified or integrated in production volume by others. It has already gone through all FCC/CE ROHS REACH UKCA, EMI/RFI ESD certifications and is available globally Several 3rd party manufacturers (such as Holybro.com) provide this or derivative commercial products.

MR-VMU-RT1176 Upright Image

The board includes the same FMU module found on Pixhawk 6X-RT paired with an NXP-based carrier board. The carrier board offers 100Base-T1 (two-wire) automotive ethernet, an NFC antenna (Connected to SE051), and a third CAN bus. It also removes the IO processor to enable 12 PWM ports, with 8 providing Dshot capability.

This board takes advantage of multiple Pixhawk​​® open standards, such as the FMUv6X-RT Standard, Autopilot Bus Standard, and Connector Standard. Equipped with a high performance NXP i.mx RT1176 dual core Processor, modular design, triple redundancy, temperature-controlled IMU board, isolated sensor domains, delivering incredible performance, reliability, and flexibility.

TIP

This autopilot is supported by the PX4 maintenance and test teams.

Introduction

Inside the MR-VMU-RT1176, you can find an NXP i.MX RT1176, 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® 6X-RT's i.MX RT1176 Crossover dual-core MCU contain an Arm® Cortex®-M7 core running up to 1GHz and Arm® Cortex®-M4 core running up to 400MHz, has 2MB SRAM and external XIP Flash with 64MB. The PX4 Autopilot takes advantage of the increased processing power and RAM. Thanks to this increased processing power, developers can be more productive and efficient with their development work, allowing for complex algorithms and models.

The FMUv6X-RT open standard includes high-performance, low-noise IMUs on board, designed for better stabilization. Triple-redundant IMU & double-redundant barometer on separate buses. When PX4 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 vibration isolation System 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, high-speed communication with mission computers via ethernet is now possible.

The MR-VMU-RT1176 reference design is perfect for developers at corporate research labs, startups, academics (research, professors, students), and commercial application that like to try out T1 (2 wire) automotive ethernet.

Note that since it is a reference design, this particular board is not produced in high volume. Similar variants will be available from our licensees.

Key Design Points

  • High performance NXP i.MX RT1170 1GHz Crossover MCU with Arm® Cortex® cores
  • Hardware secure element NXP EdgeLock SE051. This is an extension to the widely trusted EdgeLock SE050 Plug & Trust secure element family, supports applet updates in the field and delivers proven security certified to CC EAL 6+, with AVA_VAN.5 up to the OS level, for strong protection against the most recent attack scenarios. This can be used, for example, to securely store operator ID or certificates.
  • Modular flight controller: separated IMU, FMU, and Base system connected by a 100-pin & a 50-pin Pixhawk® Autopilot Bus connector.
  • Redundancy: 3x IMU sensors & 2x Barometer sensors on separate buses
  • Triple-redundancy domains: Completely isolated sensor domains with separate buses and separate power control
  • Newly designed vibration isolation system to filter out high frequency vibration and reduce noise to ensure accurate readings
  • 100Base-T1 2-Wire Ethernet interface for high-speed mission computer integration
  • IMUs are temperature-controlled by onboard heating resistors, allowing optimum working temperature of IMUs

Processors & Sensors

  • FMU Processor: NXP i.MX RT1176
    • 32 Bit Arm® Cortex®-M7, 1GHz
    • 32 Bit Arm® Cortex®-M4, 400MHz secondary core
    • 64MB external flash memory
    • 2MB RAM
  • NXP EdgeLock SE051 hardware secure element
    • IEC62443-4-2 certified for the applicable requirements
    • 46 kB user memory with personalization options to go up to 104 kB
    • Groundbreaking CC EAL6+ certified solution for IoT deployments
    • AES and 3DES encryption and decryption
  • On-board sensors
    • Accel/Gyro: ICM-20649 or BMI088
    • Accel/Gyro: ICM-42688-P
    • Accel/Gyro: ICM-42670-P
    • Mag: BMM150
    • Barometer: 2x BMP388

Electrical data

  • Voltage Ratings:
    • Max input voltage: 6V
    • USB Power Input: 4.75~5.25V
    • Servo Rail Input: 0~36V
  • Current Ratings:
    • TELEM1 output current limiter: 1.5A
    • All other port combined output current limiter: 1.5A

Mechanical data

  • Dimensions
    • Flight Controller Module: 38.8 x 31.8 x 14.6mm
    • Standard Baseboard: 50 x 96 x 16.7mm
  • Weight
    • Flight Controller Module: 23g
    • Standard Baseboard: 51g

Interfaces

  • 12 PWM servo outputs, 8 with D-SHOT

  • 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 (Telem1)
    • 1 with I2C and additional GPIO line for external NFC reader
  • 2 GPS ports

    • 1 full GPS plus 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
  • 3 CAN Buses for CAN peripheral (2 currently supported by PX4)

    • 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

  • Other Characteristics:

    • Operating & storage temperature: -40 ~ 85°c

Where to Buy

Order from NXP.

Assembly/Setup

Wiring is similar to the Holybro Pixhawk 6X and other boards that follow the Pixhawk Connector Standard.

Connections

MR-VMU-RT1176 connectors (following Pixhawk Connector Standard)

MR-VMU-RT1176 Top ImageMR-VMU-RT1176 Front ImageMR-VMU-RT1176 Leftside ImageMR-VMU-RT1176 Rightside Image

For more information see:

Pinouts

NXP MR-VMU-RT1176 Baseboard Pinout (nxp.gitbook.io)

Notes:

Serial Port Mapping

UARTDevicePort
UART1/dev/ttyS0Debug
UART3/dev/ttyS1GPS
UART4/dev/ttyS2TELEM1
UART5/dev/ttyS3GPS2
UART6/dev/ttyS4PX4IO
UART8/dev/ttyS5TELEM2
UART10/dev/ttyS6TELEM3
UART11/dev/ttyS7External

Voltage Ratings

MR-VMU-RT1176 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 MR-VMU-RT1176 uses the 6 circuit 2.00mm Pitch CLIK-Mate Wire-to-Board PCB Receptacle.

Normal Operation Maximum Ratings

Under these conditions all power sources will be used in this order to power the system:

  1. POWER1 and POWER2 inputs (4.9V to 5.5V)
  2. 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.

  1. POWER1 and POWER2 inputs (operational range 4.1V to 5.7V, 0V to 10V undamaged)
  2. USB input (operational range 4.1V to 5.7V, 0V to 6V undamaged)
  3. Servo input: VDD_SERVO pin of FMU PWM OUT and I/O PWM OUT (0V to 42V undamaged)

Voltage monitoring

Digital I2C battery monitoring is enabled by default (see Quickstart > Power).

INFO

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.

Building Firmware

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:

sh
make px4_fmu-v6xrt_default

Debug Port

The PX4 System Console and SWD interface run on the FMU Debug port.

The pinouts and connector comply with the Pixhawk Debug Full interface defined in the Pixhawk Connector Standard interface (JST SM10B connector).

PinSignalVolt
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)GNDGND

For information about using this port see:

Peripherals

Supported Platforms / Airframes

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.

Further info