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# LongitudinalControlConfiguration (UORB message)

Fixed Wing Longitudinal Control Configuration message.

Used by the fw_lateral_longitudinal_control module and TECS to constrain FixedWingLongitudinalSetpoint messages
and configure the resultant setpoints.

**TOPICS:** longitudinal_control_configuration

## Fields

| Name                          | Type      | Unit [Frame] | Range/Enum | Description                                                                                                                                       |
| ----------------------------- | --------- | ------------ | ---------- | ------------------------------------------------------------------------------------------------------------------------------------------------- |
| timestamp                     | `uint64`  | us           |            | Time since system start                                                                                                                           |
| pitch_min                     | `float32` | rad          | [-pi : pi] | Defaults to FW_P_LIM_MIN if NAN.                                                                                                                  |
| pitch_max                     | `float32` | rad          | [-pi : pi] | Defaults to FW_P_LIM_MAX if NAN.                                                                                                                  |
| throttle_min                  | `float32` | norm         | [0 : 1]    | Defaults to FW_THR_MIN if NAN.                                                                                                                    |
| throttle_max                  | `float32` | norm         | [0 : 1]    | Defaults to FW_THR_MAX if NAN.                                                                                                                    |
| climb_rate_target             | `float32` | m/s          |            | Target climbrate to change altitude. Defaults to FW_T_CLIMB_MAX if NAN. Not used if height_rate is directly set in FixedWingLongitudinalSetpoint. |
| sink_rate_target              | `float32` | m/s          |            | Target sinkrate to change altitude. Defaults to FW_T_SINK_MAX if NAN. Not used if height_rate is directly set in FixedWingLongitudinalSetpoint.   |
| speed_weight                  | `float32` |              | [0 : 2]    | 0=pitch controls altitude only, 2=pitch controls airspeed only                                                                                    |
| enforce_low_height_condition  | `bool`    |              |            | If true, the altitude controller is configured with an alternative timeconstant for tighter altitude tracking                                     |
| disable_underspeed_protection | `bool`    |              |            | If true, underspeed handling is disabled in the altitude controller                                                                               |

## Constants

| Name                                          | Type     | Value | Description |
| --------------------------------------------- | -------- | ----- | ----------- |
| <a id="#MESSAGE_VERSION"></a> MESSAGE_VERSION | `uint32` | 0     |

## Source Message

[Source file (GitHub)](https://github.com/PX4/PX4-Autopilot/blob/main/msg/versioned/LongitudinalControlConfiguration.msg)

::: details Click here to see original file

```c
# Fixed Wing Longitudinal Control Configuration message
#
# Used by the fw_lateral_longitudinal_control module and TECS to constrain FixedWingLongitudinalSetpoint messages
# and configure the resultant setpoints.

uint32 MESSAGE_VERSION = 0

uint64 timestamp # [us] Time since system start

float32 pitch_min # [rad] [@range -pi, pi] Defaults to FW_P_LIM_MIN if NAN.
float32 pitch_max # [rad] [@range -pi, pi] Defaults to FW_P_LIM_MAX if NAN.
float32 throttle_min # [norm] [@range 0,1] Defaults to FW_THR_MIN if NAN.
float32 throttle_max # [norm] [@range 0,1] Defaults to FW_THR_MAX if NAN.
float32 climb_rate_target # [m/s] Target climbrate to change altitude. Defaults to FW_T_CLIMB_MAX if NAN. Not used if height_rate is directly set in FixedWingLongitudinalSetpoint.
float32 sink_rate_target # [m/s] Target sinkrate to change altitude. Defaults to FW_T_SINK_MAX if NAN. Not used if height_rate is directly set in FixedWingLongitudinalSetpoint.
float32 speed_weight # [-] [@range 0,2] 0=pitch controls altitude only, 2=pitch controls airspeed only
bool enforce_low_height_condition # If true, the altitude controller is configured with an alternative timeconstant for tighter altitude tracking
bool disable_underspeed_protection # If true, underspeed handling is disabled in the altitude controller
```

:::