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VehicleAttitudeSetpoint.msg: remove reset_integral and fw_control_yaw_wheel

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Signed-off-by: Silvan <silvan@auterion.com>
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Silvan
2025-05-26 14:47:38 +02:00
committed by Silvan Fuhrer
parent 0276f66b18
commit 3e3f10f5bc
11 changed files with 90 additions and 136 deletions
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msg/versioned/VehicleAttitudeSetpoint.msg
+1 -5
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@@ -1,4 +1,4 @@
uint32 MESSAGE_VERSION = 0
uint32 MESSAGE_VERSION = 1
uint64 timestamp # time since system start (microseconds)
@@ -11,8 +11,4 @@ float32[4] q_d # Desired quaternion for quaternion control
# 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 FRD frame [-1,1]
bool reset_integral # Reset roll/pitch/yaw integrals (navigation logic change)
bool fw_control_yaw_wheel # control heading with steering wheel (used for auto takeoff on runway)
# TOPICS vehicle_attitude_setpoint mc_virtual_attitude_setpoint fw_virtual_attitude_setpoint