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New Crowdin translations - ko (#25811)
Co-authored-by: Crowdin Bot <support+bot@crowdin.com>
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@@ -187,6 +187,7 @@
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- [Radiolink PIX6](flight_controller/radiolink_pix6.md)
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- [Sky-Drones AIRLink](flight_controller/airlink.md)
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- [SPRacing SPRacingH7EXTREME](flight_controller/spracingh7extreme.md)
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- [SVehicle E2](flight_controller/svehicle_e2.md)
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- [ThePeach FCC-K1](flight_controller/thepeach_k1.md)
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- [ThePeach FCC-R1](flight_controller/thepeach_r1.md)
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- [Experimental Autopilots](flight_controller/autopilot_experimental.md)
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@@ -102,8 +102,7 @@ The test steps are:
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</div><div v-else-if="$frontmatter.frame === 'Plane'">
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4. The drone will first start to perform quick roll motions followed by pitch and yaw motions. When [`FW_AT_SYSID_TYPE`](../advanced_config/parameter_reference.md#FW_AT_SYSID_TYPE) is set to linear/logarithmic sine sweep (recommended), the max rates are approximately 45 deg/s for roll and 30 deg/s for pitch and yaw.
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The progress is shown in the progress bar, next to the _Autotune_ button.
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4. The drone will first start to perform quick roll motions followed by pitch and yaw motions. When [`FW_AT_SYSID_TYPE`](../advanced_config/parameter_reference.md#FW_AT_SYSID_TYPE) is set to linear/logarithmic sine sweep (recommended), the max rates reached during the maneuvers are 75% of the maximum configured roll (`FW_R_RMAX`), pitch (`FW_P_RMAX_NEG`, `FW_P_RMAX_POS`) and yaw (`FW_Y_RMAX`) rates. The progress is shown in the progress bar, next to the _Autotune_ button.
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</div>
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<div style="display: inline;" v-if="$frontmatter.frame === 'Multicopter'">
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@@ -198,7 +197,7 @@ Increase the [MC_AT_SYSID_AMP](../advanced_config/parameter_reference.md#MC_AT_S
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</div>
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<div v-else-if="$frontmatter.frame === 'Plane'">
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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.
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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.
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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.
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@@ -35,5 +35,6 @@ This category includes boards that are not fully compliant with the pixhawk stan
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- [Radiolink PIX6](../flight_controller/radiolink_pix6.md)
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- [Sky-Drones AIRLink](../flight_controller/airlink.md)
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- [SPRacing SPRacingH7EXTREME](../flight_controller/spracingh7extreme.md)
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- [Svehicle E2](../flight_controller/svehicle_e2.md)
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- [ThePeach FCC-K1](../flight_controller/thepeach_k1.md)
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- [ThePeach FCC-R1](../flight_controller/thepeach_r1.md)
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177
docs/ko/flight_controller/svehicle_e2.md
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177
docs/ko/flight_controller/svehicle_e2.md
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@@ -0,0 +1,177 @@
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# S-Vehicle E2
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:::warning
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PX4 does not manufacture this (or any) autopilot.
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:::
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The _E2_ is an advanced autopilot manufactured by S-Vehicle<sup>®</sup>.
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The autopilot is recommended for commercial system integration, but is also suitable for academic research and any other applications.
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It brings you ultimate performance, stability, and reliability in every aspect.
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:::info
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이 비행 컨트롤러는 [제조업체에서 지원](../flight_controller/autopilot_manufacturer_supported.md)합니다.
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:::
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### Processors & Sensors
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- FMU Processor: STM32H753IIK6
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- 32 Bit Arm® Cortex®-M7, 480MHz, 2MB flash memory, 1MB RAM
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- IO Processor: STM32F103
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- 32 Bit Arm® Cortex®-M3, 72MHz, 20KB SRAM
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- 내장 센서 :
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- Accel/Gyro: BMI088
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- Accel/Gyro: ICM-42688-P
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- Accel/Gyro: ICM-20649
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- Mag: RM3100
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- Barometer: 2x ICP-20100
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### 인터페이스
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- 14x PWM Servo Outputs
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- 1x Dedicated R/C Input for Spektrum / DSM and S.Bus
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- 1x Analog/PWM RSSI Input
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- 2x TELEM Ports (with full flow control)
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- 1x UART4 Port
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- 2x GPS Ports
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- 1x Full GPS plus Safety Switch Port (GPS1)
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- 1x Basic GPS Port (with I2C, GPS2)
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- 1x USB Port (TYPE-C)
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- 1x Ethernet Port
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- Transformerless application
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- 100Mbps
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- 3x I2C Bus Ports
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- 1x SPI Bus
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- 1x Chip Select Line
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- 1x Data Ready Line
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- 1x SPI Reset Line
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- 2x CAN Ports
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- 3x Power Input Ports
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- ADC Power Input
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- I2C Power Input
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- DroneCAN/UAVCAN Power Input
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- 2x AD Ports
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- Analog Input (3.3V)
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- Analog Input (6.6V - not supported by PX4)
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- 1x Dedicated Debug Port
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- FMU Debug
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## Purchase Channels
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Order from [S-Vehicle](https://svehicle.cn/).
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## 무선 조종
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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).
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기체와 조종자가 통신하기 위하여 송신기와 수신기를 바인딩하여야 합니다.
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송신기와 수신기의 매뉴얼을 참고하십시오.
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Spektrum/DSM receivers connect to the DSM/SBUS RC input.
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PPM or SBUS receivers connect to the RC IN input port.
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CRSF receiver must be wired to a spare port (UART) on the Flight Controller. Then you can bind the transmitter and receiver together.
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## 시리얼 포트 매핑
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| UART | 장치 | 포트 |
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| ------ | ---------- | -------- |
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| USART1 | /dev/ttyS0 | GPS |
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| USART2 | /dev/ttyS1 | TELEM3 |
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| USART3 | /dev/ttyS2 | 디버그 콘솔 |
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| UART4 | /dev/ttyS3 | UART4 |
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| UART5 | /dev/ttyS4 | TELEM2 |
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| USART6 | /dev/ttyS5 | PX4IO/RC |
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| UART7 | /dev/ttyS6 | TELEM1 |
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| UART8 | /dev/ttyS7 | GPS2 |
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## PWM Output
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The E2-Plus flight controller supports up to 14 PWM outputs.
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The first 8 outputs (labelled M1 to M8) are controlled by a dedicated STM32F103 IOMCU controller.
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The remaining 6 outputs (labelled 9 to 14) are the "auxiliary" outputs.
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These are directly attached to the STM32H753 FMU controller .
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The 14 PWM outputs are:
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M1 - M8 are connected to the IOMCU
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A1 - A6 are connected to the FMU
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M1 - M8 support DShot and are in 3 groups:
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- M1, M2 in group 1
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- M3, M4 in group 2
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- M5, M6, M7, M8 in group 3
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The 6 FMU PWM outputs are in 2 groups:
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A1 - A4 are in one group.
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A5, A6 are in a 2nd group.
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Channels within the same group need to use the same output rate.
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If any channel in a group uses DShot then all channels in the group need to use DShot.
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### Electrical data
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- Voltage Ratings:
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- Max input voltage: 5.7V
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- USB Power Input: 4.75\~5.25V
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- Servo Rail Input: 0\~9.9V
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- Current Ratings:
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- TELEM1 and GPS2 combined output current limiter: 1.5A
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- All other port combined output current limiter: 1.5A
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## Battery Monitoring
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The board has connectors for 3 power monitors.
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- POWER1 -- ADC
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- POWER2 -- DroneCAN
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- POWER3 -- I2C
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The board is configure by default for a analog power monitor, and also has DroneCAN power monitor and I2C defaults configured which is enabled.
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The default PDB included with the E2+ is analog and must be connected to `POWER1`.
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## 펌웨어 빌드
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To [build PX4](../dev_setup/building_px4.md) for this target, execute:
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```sh
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make svehicle_e2_default
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```
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## 디버그 포트
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The [PX4 System Console](../debug/system_console.md) and [SWD Interface](../debug/swd_debug.md) operate on the **FMU Debug** port.
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| 핀 | 신호 | 전압 |
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| ------------------------- | ------------------------------- | --------------------- |
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| 1(red) | 5V+ | +5V |
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| 2 (흑) | DEBUG TX(출력) | +3.3V |
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| 3 (흑) | DEBUG TX(입력) | +3.3V |
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| 4 (흑) | FMU_SWDIO | +3.3V |
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| 5 (흑) | FMU_SWCLK | +3.3V |
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| 6 (흑) | GND | GND |
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For information about using this port see:
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- [SWD Debug Port](../debug/swd_debug.md)
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- [PX4 System Console](../debug/system_console.md) (Note, the FMU console maps to USART3).
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- 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).
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## 핀배열
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## 지원 플랫폼 및 기체
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Any multirotor/airplane/rover or boat that can be controlled using normal RC servos or Futaba S-Bus servos.
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The complete set of supported configurations can be found in the [Airframe Reference](../airframes/airframe_reference.md).
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