diff --git a/src/modules/fw_att_control/FixedwingAttitudeControl.cpp b/src/modules/fw_att_control/FixedwingAttitudeControl.cpp
index f7651c759a..72b5ce9f00 100644
--- a/src/modules/fw_att_control/FixedwingAttitudeControl.cpp
+++ b/src/modules/fw_att_control/FixedwingAttitudeControl.cpp
@@ -488,13 +488,13 @@ void FixedwingAttitudeControl::Run()
 			float trim_yaw = _param_trim_yaw.get();
 
 			if (airspeed < _param_fw_airspd_trim.get()) {
-				trim_roll += interpolate(airspeed, _param_fw_airspd_stall.get(), _param_fw_airspd_trim.get(),
+				trim_roll += interpolate(airspeed, _param_fw_airspd_min.get(), _param_fw_airspd_trim.get(),
 							 _param_fw_dtrim_r_vmin.get(),
 							 0.0f);
-				trim_pitch += interpolate(airspeed, _param_fw_airspd_stall.get(), _param_fw_airspd_trim.get(),
+				trim_pitch += interpolate(airspeed, _param_fw_airspd_min.get(), _param_fw_airspd_trim.get(),
 							  _param_fw_dtrim_p_vmin.get(),
 							  0.0f);
-				trim_yaw += interpolate(airspeed, _param_fw_airspd_stall.get(), _param_fw_airspd_trim.get(),
+				trim_yaw += interpolate(airspeed, _param_fw_airspd_min.get(), _param_fw_airspd_trim.get(),
 							_param_fw_dtrim_y_vmin.get(),
 							0.0f);
 
diff --git a/src/modules/fw_att_control/FixedwingAttitudeControl.hpp b/src/modules/fw_att_control/FixedwingAttitudeControl.hpp
index 25dabed2f0..07e3590ba7 100644
--- a/src/modules/fw_att_control/FixedwingAttitudeControl.hpp
+++ b/src/modules/fw_att_control/FixedwingAttitudeControl.hpp
@@ -174,6 +174,7 @@ private:
 		(ParamFloat<px4::params::FW_ACRO_Z_MAX>) _param_fw_acro_z_max,
 
 		(ParamFloat<px4::params::FW_AIRSPD_MAX>) _param_fw_airspd_max,
+		(ParamFloat<px4::params::FW_AIRSPD_MIN>) _param_fw_airspd_min,
 		(ParamFloat<px4::params::FW_AIRSPD_STALL>) _param_fw_airspd_stall,
 		(ParamFloat<px4::params::FW_AIRSPD_TRIM>) _param_fw_airspd_trim,
 		(ParamInt<px4::params::FW_ARSP_MODE>) _param_fw_arsp_mode,