diff --git a/src/lib/ecl/attitude_fw/ecl_controller.h b/src/lib/ecl/attitude_fw/ecl_controller.h
index 9880d1c174..254052964a 100644
--- a/src/lib/ecl/attitude_fw/ecl_controller.h
+++ b/src/lib/ecl/attitude_fw/ecl_controller.h
@@ -62,6 +62,9 @@ struct ECL_ControlData {
 	float speed_body_u;
 	float speed_body_v;
 	float speed_body_w;
+	float acc_body_x;
+	float acc_body_y;
+	float acc_body_z;
 	float roll_setpoint;
 	float pitch_setpoint;
 	float yaw_setpoint;
diff --git a/src/modules/fw_att_control/fw_att_control_main.cpp b/src/modules/fw_att_control/fw_att_control_main.cpp
index 5dfc827479..6e49bd1d15 100644
--- a/src/modules/fw_att_control/fw_att_control_main.cpp
+++ b/src/modules/fw_att_control/fw_att_control_main.cpp
@@ -954,6 +954,9 @@ FixedwingAttitudeControl::task_main()
 				control_input.speed_body_u = speed_body_u;
 				control_input.speed_body_v = speed_body_v;
 				control_input.speed_body_w = speed_body_w;
+				control_input.acc_body_x = _accel.x;
+				control_input.acc_body_y = _accel.y;
+				control_input.acc_body_z = _accel.z;
 				control_input.roll_setpoint = roll_sp;
 				control_input.pitch_setpoint = pitch_sp;
 				control_input.airspeed_min = _parameters.airspeed_min;