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New Crowdin translations - zh-CN (#26488)

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docs/zh/msg_docs/TecsStatus.md
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@@ -1,6 +1,47 @@
---
pageClass: is-wide-page
---
# TecsStatus (UORB message)
[source file](https://github.com/PX4/PX4-Autopilot/blob/main/msg/TecsStatus.msg)
**TOPICS:** tecs_status
## Fields
| 参数名 | 类型 | Unit [Frame] | Range/Enum | 描述 |
| ---------------------------------------------------------------------------------------------------------------- | --------- | ---------------------------------------------------------------- | ---------- | ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ |
| timestamp | `uint64` | | | time since system start (microseconds) |
| altitude_sp | `float32` | | | Altitude setpoint AMSL [m] |
| altitude_reference | `float32` | | | Altitude setpoint reference AMSL [m] |
| altitude_time_constant | `float32` | | | Time constant of the altitude tracker [s] |
| height_rate_reference | `float32` | | | Height rate setpoint reference [m/s] |
| height_rate_direct | `float32` | | | Direct height rate setpoint from velocity reference generator [m/s] |
| height_rate_setpoint | `float32` | | | Height rate setpoint [m/s] |
| height_rate | `float32` | | | Height rate [m/s] |
| equivalent_airspeed_sp | `float32` | | | Equivalent airspeed setpoint [m/s] |
| true_airspeed_sp | `float32` | | | True airspeed setpoint [m/s] |
| true_airspeed_filtered | `float32` | | | True airspeed filtered [m/s] |
| true_airspeed_derivative_sp | `float32` | | | True airspeed derivative setpoint [m/s^2] |
| true_airspeed_derivative | `float32` | | | True airspeed derivative [m/s^2] |
| true_airspeed_derivative_raw | `float32` | | | True airspeed derivative raw [m/s^2] |
| total_energy_rate_sp | `float32` | | | Total energy rate setpoint [m^2/s^3] |
| total_energy_rate | `float32` | | | Total energy rate estimate [m^2/s^3] |
| total_energy_balance_rate_sp | `float32` | | | Energy balance rate setpoint [m^2/s^3] |
| total_energy_balance_rate | `float32` | | | Energy balance rate estimate [m^2/s^3] |
| throttle_integ | `float32` | | | Throttle integrator value [-] |
| pitch_integ | `float32` | | | Pitch integrator value [rad] |
| throttle_sp | `float32` | | | Current throttle setpoint [-] |
| pitch_sp_rad | `float32` | | | Current pitch setpoint [rad] |
| throttle_trim | `float32` | | | estimated throttle value [0,1] required to fly level at equivalent_airspeed_sp in the current atmospheric conditions |
| underspeed_ratio | `float32` | | | 0: no underspeed, 1: maximal underspeed. Controller takes measures to avoid stall proportional to ratio if >0. |
| fast_descend_ratio | `float32` | | | value indicating if fast descend mode is enabled with ramp up and ramp down [0-1] |
## Source Message
[Source file (GitHub)](https://github.com/PX4/PX4-Autopilot/blob/main/msg/TecsStatus.msg)
:::details
Click here to see original file
```c
uint64 timestamp # time since system start (microseconds)
@@ -34,5 +75,6 @@ float32 throttle_trim # estimated throttle value [0,1] required to fly level a
float32 underspeed_ratio # 0: no underspeed, 1: maximal underspeed. Controller takes measures to avoid stall proportional to ratio if >0.
float32 fast_descend_ratio # value indicating if fast descend mode is enabled with ramp up and ramp down [0-1]
```
:::