mirror of
https://github.com/PX4/PX4-Autopilot.git
synced 2026-05-28 02:36:37 +08:00
New Crowdin translations - zh-CN (#25813)
Co-authored-by: Crowdin Bot <support+bot@crowdin.com>
This commit is contained in:
@@ -187,6 +187,7 @@
|
|||||||
- [Radiolink PIX6](flight_controller/radiolink_pix6.md)
|
- [Radiolink PIX6](flight_controller/radiolink_pix6.md)
|
||||||
- [Sky-Drones AIRLink](flight_controller/airlink.md)
|
- [Sky-Drones AIRLink](flight_controller/airlink.md)
|
||||||
- [SPRacing SPRacingH7EXTREME](flight_controller/spracingh7extreme.md)
|
- [SPRacing SPRacingH7EXTREME](flight_controller/spracingh7extreme.md)
|
||||||
|
- [SVehicle E2](flight_controller/svehicle_e2.md)
|
||||||
- [ThePeach FCC-K1](flight_controller/thepeach_k1.md)
|
- [ThePeach FCC-K1](flight_controller/thepeach_k1.md)
|
||||||
- [ThePeach FCC-R1](flight_controller/thepeach_r1.md)
|
- [ThePeach FCC-R1](flight_controller/thepeach_r1.md)
|
||||||
- [Experimental Autopilots](flight_controller/autopilot_experimental.md)
|
- [Experimental Autopilots](flight_controller/autopilot_experimental.md)
|
||||||
|
|||||||
@@ -102,8 +102,7 @@ The test steps are:
|
|||||||
|
|
||||||
</div><div v-else-if="$frontmatter.frame === 'Plane'">
|
</div><div v-else-if="$frontmatter.frame === 'Plane'">
|
||||||
|
|
||||||
4. The drone will first start to perform quick roll motions followed by pitch and yaw motions. When [`FW_AT_SYSID_TYPE`](../advanced_config/parameter_reference.md#FW_AT_SYSID_TYPE) is set to linear/logarithmic sine sweep (recommended), the max rates are approximately 45 deg/s for roll and 30 deg/s for pitch and yaw.
|
4. The drone will first start to perform quick roll motions followed by pitch and yaw motions. When [`FW_AT_SYSID_TYPE`](../advanced_config/parameter_reference.md#FW_AT_SYSID_TYPE) is set to linear/logarithmic sine sweep (recommended), the max rates reached during the maneuvers are 75% of the maximum configured roll (`FW_R_RMAX`), pitch (`FW_P_RMAX_NEG`, `FW_P_RMAX_POS`) and yaw (`FW_Y_RMAX`) rates. The progress is shown in the progress bar, next to the _Autotune_ button.
|
||||||
The progress is shown in the progress bar, next to the _Autotune_ button.
|
|
||||||
|
|
||||||
</div>
|
</div>
|
||||||
<div style="display: inline;" v-if="$frontmatter.frame === 'Multicopter'">
|
<div style="display: inline;" v-if="$frontmatter.frame === 'Multicopter'">
|
||||||
@@ -198,7 +197,7 @@ Increase the [MC_AT_SYSID_AMP](../advanced_config/parameter_reference.md#MC_AT_S
|
|||||||
</div>
|
</div>
|
||||||
<div v-else-if="$frontmatter.frame === 'Plane'">
|
<div v-else-if="$frontmatter.frame === 'Plane'">
|
||||||
|
|
||||||
By default, the autotune maneuvers ensure that a sufficient angular rate is reached for system identification. The target rates are approximately 45 deg/s for roll and 30 deg/s for pitch and yaw.
|
By default, the autotune maneuvers ensure that a sufficient angular rate is reached for system identification, corresponding to 75% of the configured maximum roll (`FW_R_RMAX`), pitch (`FW_P_RMAX_NEG`, `FW_P_RMAX_POS`) and yaw (`FW_Y_RMAX`) rates.
|
||||||
|
|
||||||
If the signal-to-noise ratio of the vehicle is low, the system identification algorithm might have issues finding the correct coefficients. Ensure that there is no excessive noise and/or platform vibration.
|
If the signal-to-noise ratio of the vehicle is low, the system identification algorithm might have issues finding the correct coefficients. Ensure that there is no excessive noise and/or platform vibration.
|
||||||
|
|
||||||
|
|||||||
@@ -35,5 +35,6 @@ The boards in this category are:
|
|||||||
- [Radiolink PIX6](../flight_controller/radiolink_pix6.md)
|
- [Radiolink PIX6](../flight_controller/radiolink_pix6.md)
|
||||||
- [Sky-Drones AIRLink](../flight_controller/airlink.md)
|
- [Sky-Drones AIRLink](../flight_controller/airlink.md)
|
||||||
- [SPRacing SPRacingH7EXTREME](../flight_controller/spracingh7extreme.md)
|
- [SPRacing SPRacingH7EXTREME](../flight_controller/spracingh7extreme.md)
|
||||||
|
- [Svehicle E2](../flight_controller/svehicle_e2.md)
|
||||||
- [ThePeach FCC-K1](../flight_controller/thepeach_k1.md)
|
- [ThePeach FCC-K1](../flight_controller/thepeach_k1.md)
|
||||||
- [ThePeach FCC-R1](../flight_controller/thepeach_r1.md)
|
- [ThePeach FCC-R1](../flight_controller/thepeach_r1.md)
|
||||||
|
|||||||
@@ -0,0 +1,176 @@
|
|||||||
|
# S-Vehicle E2
|
||||||
|
|
||||||
|
:::warning
|
||||||
|
PX4 does not manufacture this (or any) autopilot.
|
||||||
|
:::
|
||||||
|
|
||||||
|
The _E2_ is an advanced autopilot manufactured by S-Vehicle<sup>®</sup>.
|
||||||
|
|
||||||
|
The autopilot is recommended for commercial system integration, but is also suitable for academic research and any other applications.
|
||||||
|
It brings you ultimate performance, stability, and reliability in every aspect.
|
||||||
|
|
||||||
|

|
||||||
|
|
||||||
|
:::info
|
||||||
|
These flight controllers are [manufacturer supported](../flight_controller/autopilot_manufacturer_supported.md).
|
||||||
|
:::
|
||||||
|
|
||||||
|
### Processors & Sensors
|
||||||
|
|
||||||
|
- FMU Processor: STM32H753IIK6
|
||||||
|
- 32 Bit Arm® Cortex®-M7, 480MHz, 2MB flash memory, 1MB RAM
|
||||||
|
- IO Processor: STM32F103
|
||||||
|
- 32 Bit Arm® Cortex®-M3, 72MHz, 20KB SRAM
|
||||||
|
- On-board sensors
|
||||||
|
- Accel/Gyro: BMI088
|
||||||
|
- Accel/Gyro: ICM-42688-P
|
||||||
|
- Accel/Gyro: ICM-20649
|
||||||
|
- Mag: RM3100
|
||||||
|
- Barometer: 2x ICP-20100
|
||||||
|
|
||||||
|
### 接口
|
||||||
|
|
||||||
|
- 14x PWM Servo Outputs
|
||||||
|
- 1x Dedicated R/C Input 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
|
||||||
|
- 2x CAN Ports
|
||||||
|
- 3x Power Input Ports
|
||||||
|
- ADC Power Input
|
||||||
|
- I2C Power Input
|
||||||
|
- 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
|
||||||
|
|
||||||
|
## Purchase Channels
|
||||||
|
|
||||||
|
Order from [S-Vehicle](https://svehicle.cn/).
|
||||||
|
|
||||||
|
## 遥控器
|
||||||
|
|
||||||
|
A Radio Control (RC) system is required if you want to manually control your vehicle (PX4 does not require a radio system for autonomous flight modes).
|
||||||
|
|
||||||
|
将 <em>HW\\u PM</em> 模块的6针连接器连接到飞控的<code>电源</code>接口。
|
||||||
|
|
||||||
|
Spektrum/DSM receivers connect to the DSM/SBUS RC input.
|
||||||
|
PPM or SBUS receivers connect to the RC IN input port.
|
||||||
|
CRSF receiver must be wired to a spare port (UART) on the Flight Controller. Then you can bind the transmitter and receiver together.
|
||||||
|
|
||||||
|
## 串口映射
|
||||||
|
|
||||||
|
| UART | 设备 | Port |
|
||||||
|
| ------ | ---------- | ------------- |
|
||||||
|
| USART1 | /dev/ttyS0 | GPS |
|
||||||
|
| USART2 | /dev/ttyS1 | TELEM3 |
|
||||||
|
| USART3 | /dev/ttyS2 | Debug Console |
|
||||||
|
| UART4 | /dev/ttyS3 | UART4 |
|
||||||
|
| UART5 | /dev/ttyS4 | TELEM2 |
|
||||||
|
| USART6 | /dev/ttyS5 | PX4IO/RC |
|
||||||
|
| UART7 | /dev/ttyS6 | TELEM1 |
|
||||||
|
| UART8 | /dev/ttyS7 | GPS2 |
|
||||||
|
|
||||||
|
## PWM Output
|
||||||
|
|
||||||
|
The E2-Plus flight controller supports up to 14 PWM outputs.
|
||||||
|
The first 8 outputs (labelled M1 to M8) are controlled by a dedicated STM32F103 IOMCU controller.
|
||||||
|
The remaining 6 outputs (labelled 9 to 14) are the "auxiliary" outputs.
|
||||||
|
These are directly attached to the STM32H753 FMU controller .
|
||||||
|
|
||||||
|
The 14 PWM outputs are:
|
||||||
|
|
||||||
|
M1 - M8 are connected to the IOMCU
|
||||||
|
A1 - A6 are connected to the FMU
|
||||||
|
|
||||||
|
M1 - M8 support DShot and are in 3 groups:
|
||||||
|
|
||||||
|
- M1, M2 in group 1
|
||||||
|
- M3, M4 in group 2
|
||||||
|
- M5, M6, M7, M8 in group 3
|
||||||
|
|
||||||
|
The 6 FMU PWM outputs are in 2 groups:
|
||||||
|
|
||||||
|
A1 - A4 are in one group.
|
||||||
|
A5, A6 are in a 2nd group.
|
||||||
|
|
||||||
|
Channels within the same group need to use the same output rate.
|
||||||
|
If any channel in a group uses DShot then all channels in the group need to use DShot.
|
||||||
|
|
||||||
|
### Electrical data
|
||||||
|
|
||||||
|
- Voltage Ratings:
|
||||||
|
- Max input voltage: 5.7V
|
||||||
|
- USB Power Input: 4.75\~5.25V
|
||||||
|
- Servo Rail Input: 0\~9.9V
|
||||||
|
- Current Ratings:
|
||||||
|
- TELEM1 and GPS2 combined output current limiter: 1.5A
|
||||||
|
- All other port combined output current limiter: 1.5A
|
||||||
|
|
||||||
|
## Battery Monitoring
|
||||||
|
|
||||||
|
The board has connectors for 3 power monitors.
|
||||||
|
|
||||||
|
- POWER1 -- ADC
|
||||||
|
- POWER2 -- DroneCAN
|
||||||
|
- POWER3 -- I2C
|
||||||
|
|
||||||
|
The board is configure by default for a analog power monitor, and also has DroneCAN power monitor and I2C defaults configured which is enabled.
|
||||||
|
|
||||||
|
The default PDB included with the E2+ is analog and must be connected to `POWER1`.
|
||||||
|
|
||||||
|
## 编译固件
|
||||||
|
|
||||||
|
To [build PX4](../dev_setup/building_px4.md) for this target, execute:
|
||||||
|
|
||||||
|
```sh
|
||||||
|
make svehicle_e2_default
|
||||||
|
```
|
||||||
|
|
||||||
|
## 调试接口
|
||||||
|
|
||||||
|
The [PX4 System Console](../debug/system_console.md) and [SWD Interface](../debug/swd_debug.md) operate on the **FMU Debug** port.
|
||||||
|
|
||||||
|
| 针脚 | 信号 | 电压 |
|
||||||
|
| ---- | --------------------------------- | --------------------- |
|
||||||
|
| 1(红) | 5V+ | +5V |
|
||||||
|
| 2 | DEBUG TX (OUT) | +3.3V |
|
||||||
|
| 3 | DEBUG RX (IN) | +3.3V |
|
||||||
|
| 4(黑) | FMU_SWDIO | +3.3V |
|
||||||
|
| 6 | FMU_SWCLK | +3.3V |
|
||||||
|
| 6 | GND | GND |
|
||||||
|
|
||||||
|
For information about using this port see:
|
||||||
|
|
||||||
|
- [SWD Debug Port](../debug/swd_debug.md)
|
||||||
|
- [PX4 System Console](../debug/system_console.md) (Note, the FMU console maps to USART3).
|
||||||
|
- All ports use GH1.25 ,power ports use ports on E2 uses the 6 circuit [2.00mm Pitch CLIK-Mate Wire-to-Board PCB Receptacle](https://www.molex.com/en-us/products/part-detail/5024430670).
|
||||||
|
|
||||||
|
## 针脚定义
|
||||||
|
|
||||||
|

|
||||||
|
|
||||||
|

|
||||||
|
|
||||||
|

|
||||||
|
|
||||||
|

|
||||||
|
|
||||||
|
## 支持的平台/机身
|
||||||
|
|
||||||
|
Any multirotor/airplane/rover or boat that can be controlled using normal RC servos or Futaba S-Bus servos.
|
||||||
|
The complete set of supported configurations can be found in the [Airframe Reference](../airframes/airframe_reference.md).
|
||||||
Reference in New Issue
Block a user