# CUAV X25-SUPER
::: warning
PX4 does not manufacture this (or any) autopilot.
Contact the [manufacturer](https://store.cuav.net/) for hardware support or compliance issues.
:::
The _X25-SUPER_ is an advanced autopilot manufactured by CUAV®.
The autopilot is recommended for commercial system integration but is also suitable for academic research and any other applications.
The X25-SUPER brings you ultimate performance, stability, and reliability in every aspect.
::: info
These flight controllers are [manufacturer supported](../flight_controller/autopilot_manufacturer_supported.md).
:::
### Features
- Arm® Cortex-M7® processor (STM32H743XI) with Floating-Point Unit (FPU), operating at 480MHz, and featuring 2MB Flash memory.
Enables developers to enhance productivity and efficiency, allowing for more complex algorithms and models.
- Automotive-grade RM3100 compass.
Designed for better stability and anti-interference capability.
- Triple-redundant IMUs and dual-redundant barometers located on separate buses.
If the PX4 autopilot detects a sensor failure, the system seamlessly switches to another sensor to maintain flight control reliability.
- Independent LDO power control supplies power to each sensor group.
A vibration isolation system filters high-frequency vibrations and reduces noise to ensure accurate readings, enabling better overall flight performance for the vehicle.
- Integrated Microchip Ethernet PHY for high-speed communication with onboard devices like mission computers via Ethernet.
- Dual temperature compensation systems, located on the IMU board and FMU board respectively.
Temperature is controlled by onboard heating resistors to achieve the optimal operating temperature for the IMUs.
- PWM servo output voltage switchable between 3.3V or 5V.
- Modular design for DIY carrier boards.
### Processors & Sensors
- Main Processor: STM32H743XI
- 32-bit Arm® Cortex®-M7, 480MHz, 2MB Flash, 1MB RAM
- Onboard Sensors:
- Accel/Gyro: SCH16T
- Accel/Gyro: IIM42652
- Accel/Gyro: IIM42653
- Magnetometer: RM3100
- Barometer: BMP581
- Barometer: ICP-20100
### Electrical Data
- Rated Voltage:
- Input Voltage: 10~18V
- USB Power Input: 4.75~5.25V
- Servo Rail Input: 0~9.9V
- Rated Current:
- Total Output Max Current: 10A
- `TELEM1` and `TELEM2` Output Current limiter: 4A
- `CAN1` and `CAN2` Output Current limiter: 2.4A
- Other Ports Output Current limiter: 1.5A
### Interfaces
- 16x PWM Servo Outputs
- 1x Dedicated R/C Input(`RC IN`) for Spektrum / DSM and S.Bus
- 1x Analog/PWM RSSI Input
- 2x TELEM Ports (with full flow control)
- 1x UART4 Port
- 2x GPS Ports
- 1x Full GPS plus Safety Switch Port (GPS1)
- 1x Basic GPS Port (with I2C, GPS2)
- 1x USB Port (TYPE-C)
- 1x Ethernet Port
- Transformerless application
- 100Mbps
- 3x I2C Bus Ports
- 1x SPI Bus
- 1x Chip Select Line
- 1x Data Ready Line
- 1x SPI Reset Line
- 5x CAN Ports for CAN Peripherals
- 3x CAN1 Bus Multiplexed Ports
- 2x CAN2 Bus Multiplexed Ports
- 2x Power Input Ports
- DroneCAN/UAVCAN Power Input
- 2x AD Ports
- Analog Input (3.3V)
- Analog Input (6.6V - not supported by PX4)
- 1x Dedicated Debug Port
- FMU Debug
### Mechanical Data
- Dimensions:
## Purchase Channels {#store}
Order from [CUAV](https://store.cuav.net/).
## Assembly/Setup
The [X25 SUPER Wiring Quick Start](../assembly/quick_start_cuav_x25_evo.md) provides instructions on how to assemble required/important peripherals including GPS, Power Module etc.
## Pinouts
## Serial Port Mapping
| UART | Device | Port |
| ------ | ---------- | ------------- |
| USART1 | /dev/ttyS0 | GPS1 |
| USART2 | /dev/ttyS1 | GPS2 |
| USART3 | /dev/ttyS2 | Debug Console |
| UART4 | /dev/ttyS3 | UART4 |
| UART5 | /dev/ttyS4 | TELEM2 |
| USART6 | /dev/ttyS5 | RC IN |
| UART7 | /dev/ttyS6 | TELEM1 |
## RC Input
The RC input pin is directly connected to the FMU UART6 TX.
## Voltage Ratings
The _X25-SUPER_ achieves triple redundancy on power supplies if three power sources are provided.
The three power rails are `POWERC1`, `POWERC2`, and `USB`.
- **POWER C1** and **POWER C2** are DroneCAN/UAVCAN battery interfaces.
**Normal Operation Maximum Ratings**
Under these conditions, all power sources will be used to power the system in the following order:
1. **POWER C1** and **POWER C2** Inputs (10V to 18V)
2. USB Input (4.75V to 5.25V)
**Voltage monitoring**
Digital DroneCAN/UAVCAN battery monitoring is enabled by default.
## Building Firmware
::: tip
Most users will not need to build this firmware (from PX4 v1.18).
It is pre-built and automatically installed by _QGroundControl_ when appropriate hardware is connected.
:::
To [build PX4](../dev_setup/building_px4.md) for this target, execute:
```sh
make cuav_x25-super_default
```
## Debug Port {#debug_port}
The [PX4 System Console](../debug/system_console.md) and [SWD Interface](../debug/swd_debug.md) operate on the **FMU Debug** port.
| Pin | Signal | Volt |
| ------- | -------------- | ----- |
| 1 (red) | 5V+ | +5V |
| 2 (blk) | DEBUG TX (OUT) | +3.3V |
| 3 (blk) | DEBUG RX (IN) | +3.3V |
| 4 (blk) | FMU_SWDIO | +3.3V |
| 5 (blk) | FMU_SWCLK | +3.3V |
| 6 (blk) | GND | GND |
## 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](../airframes/airframe_reference.md).
## Further info
- [CUAV Docs](https://doc.cuav.net/)