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New Crowdin translations - ko (#26487)

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docs/ko/msg_docs/AirspeedValidated.md
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---
pageClass: is-wide-page
---
# AirspeedValidated (UORB message)
Validated airspeed
Validated airspeed.
Provides information about airspeed (indicated, true, calibrated) and the source of the data.
Used by controllers, estimators and for airspeed reporting to operator.
[source file](https://github.com/PX4/PX4-Autopilot/blob/main/msg/versioned/AirspeedValidated.msg)
**TOPICS:** airspeed_validated
## Fields
| 명칭 | 형식 | Unit [Frame] | Range/Enum | 설명 |
| ----------------------------------------------------------------------------------------------------------------------------------------- | --------- | ---------------------------------------------------------------- | ----------------- | --------------------------------------------------------------------------------------------------------------------------------------------------------------- |
| timestamp | `uint64` | us | | Time since system start |
| indicated_airspeed_m_s | `float32` | m/s | | Indicated airspeed (IAS) (Invalid: NaN) |
| calibrated_airspeed_m_s | `float32` | m/s | | Calibrated airspeed (CAS) (Invalid: NaN) |
| true_airspeed_m_s | `float32` | m/s | | True airspeed (TAS) (Invalid: NaN) |
| airspeed_source | `int8` | | [SOURCE](#SOURCE) | Source of currently published airspeed values |
| calibrated_ground_minus_wind_m_s | `float32` | m/s | | CAS calculated from groundspeed - windspeed, where windspeed is estimated based on a zero-sideslip assumption (Invalid: NaN) |
| calibraded_airspeed_synth_m_s | `float32` | m/s | | Synthetic airspeed (Invalid: NaN) |
| airspeed_derivative_filtered | `float32` | m/s^2 | | Filtered indicated airspeed derivative |
| throttle_filtered | `float32` | | | Filtered fixed-wing throttle |
| pitch_filtered | `float32` | rad | | Filtered pitch |
## Enums
### SOURCE {#SOURCE}
| 명칭 | 형식 | Value | 설명 |
| -------------------------------------------------------------------------------------------------------------------------------- | ------ | ----- | ----------------------- |
| <a href="#SOURCE_DISABLED"></a> SOURCE_DISABLED | `int8` | -1 | Disabled |
| <a href="#SOURCE_GROUND_MINUS_WIND"></a> SOURCE_GROUND_MINUS_WIND | `int8` | 0 | Ground speed minus wind |
| <a href="#SOURCE_SENSOR_1"></a> SOURCE_SENSOR_1 | `int8` | 1 | Sensor 1 |
| <a href="#SOURCE_SENSOR_2"></a> SOURCE_SENSOR_2 | `int8` | 2 | Sensor 2 |
| <a href="#SOURCE_SENSOR_3"></a> SOURCE_SENSOR_3 | `int8` | 3 | Sensor 3 |
| <a href="#SOURCE_SYNTHETIC"></a> SOURCE_SYNTHETIC | `int8` | 4 | Synthetic airspeed |
## Constants
| 명칭 | 형식 | Value | 설명 |
| -------------------------------------------------------------------- | -------- | ----- | -- |
| <a href="#MESSAGE_VERSION"></a> MESSAGE_VERSION | `uint32` | 1 | |
## Source Message
[Source file (GitHub)](https://github.com/PX4/PX4-Autopilot/blob/main/msg/versioned/AirspeedValidated.msg)
:::details
Click here to see original file
```c
# Validated airspeed
@@ -35,5 +80,6 @@ float32 calibraded_airspeed_synth_m_s # [m/s] [@invalid NaN] Synthetic airsp
float32 airspeed_derivative_filtered # [m/s^2] Filtered indicated airspeed derivative
float32 throttle_filtered # [-] Filtered fixed-wing throttle
float32 pitch_filtered # [rad] Filtered pitch
```
:::