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37 lines
2.4 KiB
Markdown
37 lines
2.4 KiB
Markdown
---
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pageClass: is-wide-page
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---
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# FixedWingLateralStatus (UORB message)
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Fixed Wing Lateral Status message. Published by the fw_lateral_longitudinal_control module to report the resultant lateral setpoint.
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**TOPICS:** fixed_wing_lateral_status
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## Fields
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| 명칭 | 형식 | Unit [Frame] | Range/Enum | 설명 |
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| --------------------------------------------------------------------------------------------------------------------- | --------- | ---------------------------------------------------------------- | --------------------------------------------------------------------------- | ---------------------------------------------------------------------------- |
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| <a id="fld_timestamp"></a>timestamp | `uint64` | | | time since system start (microseconds) |
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| <a id="fld_lateral_acceleration_setpoint"></a>lateral_acceleration_setpoint | `float32` | FRD | | resultant lateral acceleration setpoint |
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| <a id="fld_can_run_factor"></a>can_run_factor | `float32` | norm | [0 : 1] | estimate of certainty of the correct functionality of the npfg roll setpoint |
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## Source Message
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[Source file (GitHub)](https://github.com/PX4/PX4-Autopilot/blob/main/msg/FixedWingLateralStatus.msg)
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:::details
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Click here to see original file
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```c
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# Fixed Wing Lateral Status message
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# Published by the fw_lateral_longitudinal_control module to report the resultant lateral setpoint
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uint64 timestamp # time since system start (microseconds)
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float32 lateral_acceleration_setpoint # [m/s^2] [FRD] resultant lateral acceleration setpoint
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float32 can_run_factor # [norm] [@range 0, 1] estimate of certainty of the correct functionality of the npfg roll setpoint
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```
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:::
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