diff --git a/msg/VehicleAttitudeSetpoint.msg b/msg/VehicleAttitudeSetpoint.msg
index e4f66c446a..f52025d2bb 100644
--- a/msg/VehicleAttitudeSetpoint.msg
+++ b/msg/VehicleAttitudeSetpoint.msg
@@ -11,7 +11,7 @@ float32[4] q_d			# Desired quaternion for quaternion control
 
 # 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]
+float32[3] thrust_body		# Normalized thrust command in body FRD frame [-1,1]
 
 bool reset_integral	# Reset roll/pitch/yaw integrals (navigation logic change)