PX4-Autopilot/docs/en/msg_docs/VehicleRatesSetpoint.md
Hamish Willee 88d623bedb
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Signed-off-by: Ramon Roche <mrpollo@gmail.com>
Co-authored-by: Ramon Roche <mrpollo@gmail.com>
2025-03-13 16:08:27 +11:00

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# VehicleRatesSetpoint (UORB message)
[source file](https://github.com/PX4/PX4-Autopilot/blob/main/msg/versioned/VehicleRatesSetpoint.msg)
```c
uint32 MESSAGE_VERSION = 0
uint64 timestamp # time since system start (microseconds)
# body angular rates in FRD frame
float32 roll # [rad/s] roll rate setpoint
float32 pitch # [rad/s] pitch rate setpoint
float32 yaw # [rad/s] yaw rate setpoint
# For clarification: For multicopters thrust_body[0] and thrust[1] are usually 0 and thrust[2] is the negative throttle demand.
# For fixed wings thrust_x is the throttle demand and thrust_y, thrust_z will usually be zero.
float32[3] thrust_body # Normalized thrust command in body NED frame [-1,1]
bool reset_integral # Reset roll/pitch/yaw integrals (navigation logic change)
```