mirror of
https://github.com/PX4/PX4-Autopilot.git
synced 2026-05-27 10:17:45 +08:00
docs(docs): Update CUAV X25 Series Doc (#26882)
This commit is contained in:
@@ -1,6 +1,6 @@
|
||||
# CUAV X25-SUPER
|
||||
|
||||
<Badge type="tip" text="PX4 v1.18)" />
|
||||
<Badge type="tip" text="PX4 v1.18" />
|
||||
|
||||
::: warning
|
||||
PX4 does not manufacture this (or any) autopilot.
|
||||
@@ -21,12 +21,17 @@ These flight controllers are [manufacturer supported](../flight_controller/autop
|
||||
|
||||
### 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.
|
||||
- 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.
|
||||
- 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.
|
||||
|
||||
@@ -50,14 +55,14 @@ These flight controllers are [manufacturer supported](../flight_controller/autop
|
||||
- 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
|
||||
- `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 for Spektrum / DSM and S.Bus
|
||||
- 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
|
||||
@@ -80,16 +85,15 @@ These flight controllers are [manufacturer supported](../flight_controller/autop
|
||||
- DroneCAN/UAVCAN Power Input
|
||||
- 2x AD Ports
|
||||
- Analog Input (3.3V)
|
||||
- Analog Input (6.6V - not supported)
|
||||
- Analog Input (6.6V - not supported by PX4)
|
||||
- 1x Dedicated Debug Port
|
||||
- FMU Debug
|
||||
|
||||
### Mechanical Data
|
||||
|
||||
- Size
|
||||
- Flight controller
|
||||
- Dimensions:
|
||||
|
||||

|
||||

|
||||
|
||||
## Purchase Channels {#store}
|
||||
|
||||
@@ -97,7 +101,7 @@ Order from [CUAV](https://store.cuav.net/).
|
||||
|
||||
## Assembly/Setup
|
||||
|
||||
- Not provided.
|
||||
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
|
||||
|
||||
@@ -113,7 +117,7 @@ Order from [CUAV](https://store.cuav.net/).
|
||||
| USART3 | /dev/ttyS2 | Debug Console |
|
||||
| UART4 | /dev/ttyS3 | UART4 |
|
||||
| UART5 | /dev/ttyS4 | TELEM2 |
|
||||
| USART6 | /dev/ttyS5 | RC |
|
||||
| USART6 | /dev/ttyS5 | RC IN |
|
||||
| UART7 | /dev/ttyS6 | TELEM1 |
|
||||
|
||||
## RC Input
|
||||
@@ -122,7 +126,8 @@ 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.
|
||||
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.
|
||||
|
||||
@@ -140,13 +145,13 @@ 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.
|
||||
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
|
||||
```
|
||||
|
||||
|
||||
Reference in New Issue
Block a user