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docs(i18n): PX4 guide translations (Crowdin) - ko (#26976)

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docs/ko/flight_controller/cuav_x25-evo.md
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@@ -19,12 +19,17 @@ The X25-EVO brings you ultimate performance, stability, and reliability in every
### 특징
- 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.
@@ -33,7 +38,7 @@ The X25-EVO brings you ultimate performance, stability, and reliability in every
- Main Processor: STM32H743XI
- 32-bit Arm® Cortex®-M7, 480MHz, 2MB Flash, 1MB RAM
- Onboard Sensors:
- Accel/Gyro: IIM42652\*2
- Accel/Gyro: IIM42652 (x2)
- Accel/Gyro: IIM42653
- 자력계 : RM3100
- Barometer: BMP581
@@ -47,14 +52,14 @@ The X25-EVO brings you ultimate performance, stability, and reliability in every
- 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
### 인터페이스
- 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
@@ -83,7 +88,12 @@ The X25-EVO brings you ultimate performance, stability, and reliability in every
### 기계식 부품
- Not provided.
- 중량
- Flight Controller Module: 110g
- Operating & storage temperature: -20 ~ 85°C
- Dimensions:
![CUAV X25 EVO](../../assets/flight_controller/cuav_x25-evo/x25_evo_size.png)
## Purchase Channels {#store}
@@ -91,11 +101,11 @@ Order from [CUAV](https://store.cuav.net/).
## 조립 및 설정
- Not provided.
The [X25 EVO Wiring Quick Start](../assembly/quick_start_cuav_x25_evo.md) provides instructions on how to assemble required/important peripherals including GPS, Power Module etc.
## Pin Definitions
## 핀배열
- Not provided.
![CUAV X25 EVO Pinout](../../assets/flight_controller/cuav_x25-evo/x25_evo_pinouts.jpg)
## 시리얼 포트 매핑
@@ -106,12 +116,34 @@ Order from [CUAV](https://store.cuav.net/).
| USART3 | /dev/ttyS2 | 디버그 콘솔 |
| UART4 | /dev/ttyS3 | UART4 |
| UART5 | /dev/ttyS4 | TELEM2 |
| USART6 | /dev/ttyS5 | RC |
| USART6 | /dev/ttyS5 | RC IN |
| UART7 | /dev/ttyS6 | TELEM1 |
## PWM Outputs {#pwm_outputs}
This flight controller supports up to 16 FMU PWM outputs (MAIN).
Outputs:
- Outputs 1-8 support [DShot](../peripherals/dshot.md).
- Outputs 9-16 do not support DShot.
- Outputs 1-7 support [Bidirectional DShot](../peripherals/dshot.md#bidirectional-dshot-telemetry).
- Output 8 supports Bidirectional DShot output only (no eRPM capture).
The 16 outputs are in 5 groups:
- Outputs 1-4 in group1 (Timer5)
- Outputs 5-8 in group2 (Timer4)
- Outputs 9-11 in group3 (Timer1)
- Outputs 12-14 in group4 (Timer8)
- Outputs 15-16 in group5 (Timer12)
All outputs within the same group must use the same output protocol and rate.
## 정격 전압
The _X25-EVO_ achieves triple redundancy on power supplies if three power sources are provided. The three power rails are POWERC1, POWERC2, and USB.
The _X25-EVO_ 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.
@@ -154,7 +186,8 @@ The [PX4 System Console](../debug/system_console.md) and [SWD Interface](../debu
## 지원 플랫폼 및 기체
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).
일반 RC 서보 또는 Futaba S-Bus 서보로 제어 가능한 모든 멀티콥터/비행기/로버 또는 보트.
The complete set of supported configurations can be seen in the [Airframes Reference](../airframes/airframe_reference.md).
## 추가 정보