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New Crowdin translations - uk (#26552)

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2026-03-05 14:01:38 +11:00
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docs/uk/msg_docs/AutotuneAttitudeControlStatus.md
+20 -20
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@@ -11,7 +11,7 @@ and is subscribed to by the respective attitude controllers to command rate setp
The rate_sp field is consumed by the controllers, while the remaining fields (model coefficients, gains, filters, and autotune state) are used for logging and debugging.
**TOPICS:** autotune_attitudecontrol_status
**TOPICS:** autotune_attitude_control_status
## Fields
@@ -37,25 +37,25 @@ The rate_sp field is consumed by the controllers, while the remaining fields (mo
### STATE {#STATE}
| Назва | Тип | Значення | Опис |
| ---------------------------------------------------------------------------------------------------------------------------------------------- | ------- | -------- | ------------------------------------------------------------------------------------------- |
| <a href="#STATE_IDLE"></a> STATE_IDLE | `uint8` | 0 | Idle (not running) |
| <a href="#STATE_INIT"></a> STATE_INIT | `uint8` | 1 | Initialize filters and setup |
| <a href="#STATE_ROLL_AMPLITUDE_DETECTION"></a> STATE_ROLL_AMPLITUDE_DETECTION | `uint8` | 2 | FW only: determine required excitation amplitude (roll) |
| <a href="#STATE_ROLL"></a> STATE_ROLL | `uint8` | 3 | Roll-axis excitation and model identification |
| <a href="#STATE_ROLL_PAUSE"></a> STATE_ROLL_PAUSE | `uint8` | 4 | Pause to return to level flight |
| <a href="#STATE_PITCH_AMPLITUDE_DETECTION"></a> STATE_PITCH_AMPLITUDE_DETECTION | `uint8` | 5 | FW only: determine required excitation amplitude (pitch) |
| <a href="#STATE_PITCH"></a> STATE_PITCH | `uint8` | 6 | Pitch-axis excitation and model identification |
| <a href="#STATE_PITCH_PAUSE"></a> STATE_PITCH_PAUSE | `uint8` | 7 | Pause to return to level flight |
| <a href="#STATE_YAW_AMPLITUDE_DETECTION"></a> STATE_YAW_AMPLITUDE_DETECTION | `uint8` | 8 | FW only: determine required excitation amplitude (yaw) |
| <a href="#STATE_YAW"></a> STATE_YAW | `uint8` | 9 | Yaw-axis excitation and model identification |
| <a href="#STATE_YAW_PAUSE"></a> STATE_YAW_PAUSE | `uint8` | 10 | Pause to return to level flight |
| <a href="#STATE_VERIFICATION"></a> STATE_VERIFICATION | `uint8` | 11 | Verify model and candidate gains |
| <a href="#STATE_APPLY"></a> STATE_APPLY | `uint8` | 12 | Apply gains |
| <a href="#STATE_TEST"></a> STATE_TEST | `uint8` | 13 | Test gains in closed-loop |
| <a href="#STATE_COMPLETE"></a> STATE_COMPLETE | `uint8` | 14 | Tuning completed successfully |
| <a href="#STATE_FAIL"></a> STATE_FAIL | `uint8` | 15 | Tuning failed (model invalid or controller unstable) |
| <a href="#STATE_WAIT_FOR_DISARM"></a> STATE_WAIT_FOR_DISARM | `uint8` | 16 | Waiting for disarm before finalizing |
| Назва | Тип | Значення | Опис |
| -------------------------------------------------------------------------------------------------------------------------------------------- | ------- | -------- | ------------------------------------------------------------------------------------------- |
| <a id="#STATE_IDLE"></a> STATE_IDLE | `uint8` | 0 | Idle (not running) |
| <a id="#STATE_INIT"></a> STATE_INIT | `uint8` | 1 | Initialize filters and setup |
| <a id="#STATE_ROLL_AMPLITUDE_DETECTION"></a> STATE_ROLL_AMPLITUDE_DETECTION | `uint8` | 2 | FW only: determine required excitation amplitude (roll) |
| <a id="#STATE_ROLL"></a> STATE_ROLL | `uint8` | 3 | Roll-axis excitation and model identification |
| <a id="#STATE_ROLL_PAUSE"></a> STATE_ROLL_PAUSE | `uint8` | 4 | Pause to return to level flight |
| <a id="#STATE_PITCH_AMPLITUDE_DETECTION"></a> STATE_PITCH_AMPLITUDE_DETECTION | `uint8` | 5 | FW only: determine required excitation amplitude (pitch) |
| <a id="#STATE_PITCH"></a> STATE_PITCH | `uint8` | 6 | Pitch-axis excitation and model identification |
| <a id="#STATE_PITCH_PAUSE"></a> STATE_PITCH_PAUSE | `uint8` | 7 | Pause to return to level flight |
| <a id="#STATE_YAW_AMPLITUDE_DETECTION"></a> STATE_YAW_AMPLITUDE_DETECTION | `uint8` | 8 | FW only: determine required excitation amplitude (yaw) |
| <a id="#STATE_YAW"></a> STATE_YAW | `uint8` | 9 | Yaw-axis excitation and model identification |
| <a id="#STATE_YAW_PAUSE"></a> STATE_YAW_PAUSE | `uint8` | 10 | Pause to return to level flight |
| <a id="#STATE_VERIFICATION"></a> STATE_VERIFICATION | `uint8` | 11 | Verify model and candidate gains |
| <a id="#STATE_APPLY"></a> STATE_APPLY | `uint8` | 12 | Apply gains |
| <a id="#STATE_TEST"></a> STATE_TEST | `uint8` | 13 | Test gains in closed-loop |
| <a id="#STATE_COMPLETE"></a> STATE_COMPLETE | `uint8` | 14 | Tuning completed successfully |
| <a id="#STATE_FAIL"></a> STATE_FAIL | `uint8` | 15 | Tuning failed (model invalid or controller unstable) |
| <a id="#STATE_WAIT_FOR_DISARM"></a> STATE_WAIT_FOR_DISARM | `uint8` | 16 | Waiting for disarm before finalizing |
## Source Message