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Co-Authored-By: PX4 BuildBot <bot@px4.io>
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@@ -14,14 +14,14 @@ If both altitude and height_rate are NAN, the controller maintains the current a
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## Fields
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| Name | Type | Unit [Frame] | Range/Enum | Description |
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| ------------------- | --------- | ------------ | ---------- | ---------------------------------------------------------------------------------- |
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| timestamp | `uint64` | us | | Time since system start |
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| altitude | `float32` | m | | Altitude setpoint AMSL, not controlled directly if NAN or if height_rate is finite |
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| height_rate | `float32` | m/s [ENU] | | Scalar height rate setpoint. NAN if not controlled directly |
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| equivalent_airspeed | `float32` | m/s | [0 : inf] | Scalar equivalent airspeed setpoint. NAN if system default should be used |
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| pitch_direct | `float32` | rad [FRD] | [-pi : pi] | NAN if not controlled, overrides total energy controller |
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| throttle_direct | `float32` | norm | [0 : 1] | NAN if not controlled, overrides total energy controller |
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| Name | Type | Unit [Frame] | Range/Enum | Description |
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| ------------------------------------------------------- | --------- | ------------ | ---------- | ---------------------------------------------------------------------------------- |
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| <a id="fld_timestamp"></a>timestamp | `uint64` | us | | Time since system start |
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| <a id="fld_altitude"></a>altitude | `float32` | m | | Altitude setpoint AMSL, not controlled directly if NAN or if height_rate is finite |
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| <a id="fld_height_rate"></a>height_rate | `float32` | m/s [ENU] | | Scalar height rate setpoint. NAN if not controlled directly |
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| <a id="fld_equivalent_airspeed"></a>equivalent_airspeed | `float32` | m/s | [0 : inf] | Scalar equivalent airspeed setpoint. NAN if system default should be used |
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| <a id="fld_pitch_direct"></a>pitch_direct | `float32` | rad [FRD] | [-pi : pi] | NAN if not controlled, overrides total energy controller |
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| <a id="fld_throttle_direct"></a>throttle_direct | `float32` | norm | [0 : 1] | NAN if not controlled, overrides total energy controller |
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## Constants
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