New Crowdin translations - zh-CN (#26488)

Co-authored-by: Crowdin Bot <support+bot@crowdin.com>
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PX4 Build Bot
2026-02-18 16:44:34 +11:00
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commit 47d5971f42
314 changed files with 11960 additions and 1374 deletions
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@@ -1,6 +1,39 @@
---
pageClass: is-wide-page
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# AirspeedValidatedV0 (UORB message)
[source file](https://github.com/PX4/PX4-Autopilot/blob/main/msg/px4_msgs_old/msg/AirspeedValidatedV0.msg)
**TOPICS:** airspeed_validatedv0
## Fields
| 参数名 | 类型 | Unit [Frame] | Range/Enum | 描述 |
| ----------------------------------------------------------------------------------------------------------------------------------------- | --------- | ---------------------------------------------------------------- | ---------- | ------------------------------------------------------------------------------------------------------------------------------------ |
| timestamp | `uint64` | | | time since system start (microseconds) |
| indicated_airspeed_m_s | `float32` | | | indicated airspeed in m/s (IAS), set to NAN if invalid |
| calibrated_airspeed_m_s | `float32` | | | calibrated airspeed in m/s (CAS, accounts for instrumentation errors), set to NAN if invalid |
| true_airspeed_m_s | `float32` | | | true filtered airspeed in m/s (TAS), set to NAN if invalid |
| calibrated_ground_minus_wind_m_s | `float32` | | | CAS calculated from groundspeed - windspeed, where windspeed is estimated based on a zero-sideslip assumption, set to NAN if invalid |
| true_ground_minus_wind_m_s | `float32` | | | TAS calculated from groundspeed - windspeed, where windspeed is estimated based on a zero-sideslip assumption, set to NAN if invalid |
| airspeed_sensor_measurement_valid | `bool` | | | True if data from at least one airspeed sensor is declared valid. |
| selected_airspeed_index | `int8` | | | 1-3: airspeed sensor index, 0: groundspeed-windspeed, -1: airspeed invalid |
| airspeed_derivative_filtered | `float32` | | | filtered indicated airspeed derivative [m/s/s] |
| throttle_filtered | `float32` | | | filtered fixed-wing throttle [-] |
| pitch_filtered | `float32` | | | filtered pitch [rad] |
## Constants
| 参数名 | 类型 | 值 | 描述 |
| -------------------------------------------------------------------- | -------- | - | -- |
| <a href="#MESSAGE_VERSION"></a> MESSAGE_VERSION | `uint32` | 0 | |
## Source Message
[Source file (GitHub)](https://github.com/PX4/PX4-Autopilot/blob/main/msg/px4_msgs_old/msg/AirspeedValidatedV0.msg)
:::details
Click here to see original file
```c
uint32 MESSAGE_VERSION = 0
@@ -21,5 +54,6 @@ int8 selected_airspeed_index # 1-3: airspeed sensor index, 0: groundspeed-win
float32 airspeed_derivative_filtered # filtered indicated airspeed derivative [m/s/s]
float32 throttle_filtered # filtered fixed-wing throttle [-]
float32 pitch_filtered # filtered pitch [rad]
```
:::