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docs(i18n): PX4 guide translations (Crowdin) - zh-CN (#27479)

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2026-05-28 07:44:55 +10:00
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docs/zh/msg_docs/FixedWingRunwayControl.md
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@@ -10,12 +10,12 @@ Auxiliary control fields for fixed-wing runway takeoff/landing.
## Fields
| 参数名 | 类型 | Unit [Frame] | Range/Enum | 描述 |
| ------------------------------------------------------------------------------------------ | --------- | ---------------------------------------------------------------- | ---------------------------------------------------------------------------- | ---------------------------------------------------------------------------------------------------------- |
| timestamp | `uint64` | us | | time since system start |
| runway_takeoff_state | `uint8` | | | Current state of runway takeoff state machine |
| wheel_steering_enabled | `bool` | | | Flag that enables the wheel steering. |
| wheel_steering_nudging_rate | `float32` | FRD | [-1 : 1] | Manual wheel nudging, added to controller output. NAN is interpreted as 0. |
| 参数名 | 类型 | Unit [Frame] | Range/Enum | 描述 |
| -------------------------------------------------------------------------------------------------------------------------------------- | --------- | ---------------------------------------------------------------- | ---------------------------------------------------------------------------- | ---------------------------------------------------------------------------------------------------------- |
| <a id="fld_timestamp"></a>timestamp | `uint64` | us | | time since system start |
| <a id="fld_runway_takeoff_state"></a>runway_takeoff_state | `uint8` | | | Current state of runway takeoff state machine |
| <a id="fld_wheel_steering_enabled"></a>wheel_steering_enabled | `bool` | | | Flag that enables the wheel steering. |
| <a id="fld_wheel_steering_nudging_rate"></a>wheel_steering_nudging_rate | `float32` | FRD | [-1 : 1] | Manual wheel nudging, added to controller output. NAN is interpreted as 0. |
## Constants