diff --git a/src/modules/fw_pos_control_l1/FixedwingPositionControl.cpp b/src/modules/fw_pos_control_l1/FixedwingPositionControl.cpp
index 60fe50f696..bba68307c4 100644
--- a/src/modules/fw_pos_control_l1/FixedwingPositionControl.cpp
+++ b/src/modules/fw_pos_control_l1/FixedwingPositionControl.cpp
@@ -438,6 +438,12 @@ FixedwingPositionControl::get_auto_airspeed_setpoint(const float control_interva
 					       MAX_WEIGHT_RATIO);
 	}
 
+	// Adapt min airspeed setpoint based on wind estimate for more stability in higher winds.
+	if (_airspeed_valid && _wind_valid && _param_fw_wind_arsp_sc.get() > FLT_EPSILON) {
+		calibrated_min_airspeed = math::min(calibrated_min_airspeed + _param_fw_wind_arsp_sc.get() * _wind_vel.length(),
+						    _param_fw_airspd_max.get());
+	}
+
 	// Stall speed increases with the square root of the load factor times the weight ratio
 	// Vs ~ sqrt(load_factor * weight_ratio)
 	calibrated_min_airspeed = constrain(_param_fw_airspd_stall.get() * sqrtf(load_factor * weight_ratio),
diff --git a/src/modules/fw_pos_control_l1/FixedwingPositionControl.hpp b/src/modules/fw_pos_control_l1/FixedwingPositionControl.hpp
index 6ec4a9e990..7e54b0cb3b 100644
--- a/src/modules/fw_pos_control_l1/FixedwingPositionControl.hpp
+++ b/src/modules/fw_pos_control_l1/FixedwingPositionControl.hpp
@@ -860,7 +860,9 @@ private:
 		(ParamFloat<px4::params::FW_LND_FL_SINK>) _param_fw_lnd_fl_sink,
 		(ParamFloat<px4::params::FW_LND_TD_OFF>) _param_fw_lnd_td_off,
 		(ParamInt<px4::params::FW_LND_NUDGE>) _param_fw_lnd_nudge,
-		(ParamInt<px4::params::FW_LND_ABORT>) _param_fw_lnd_abort
+		(ParamInt<px4::params::FW_LND_ABORT>) _param_fw_lnd_abort,
+
+		(ParamFloat<px4::params::FW_WIND_ARSP_SC>) _param_fw_wind_arsp_sc
 	)
 
 };
diff --git a/src/modules/fw_pos_control_l1/fw_pos_control_l1_params.c b/src/modules/fw_pos_control_l1/fw_pos_control_l1_params.c
index c66b7d8c09..29e0975e53 100644
--- a/src/modules/fw_pos_control_l1/fw_pos_control_l1_params.c
+++ b/src/modules/fw_pos_control_l1/fw_pos_control_l1_params.c
@@ -1076,3 +1076,20 @@ PARAM_DEFINE_INT32(FW_LND_NUDGE, 2);
  * @group FW Auto Landing
  */
 PARAM_DEFINE_INT32(FW_LND_ABORT, 3);
+
+/**
+ * Wind-based airspeed scaling factor
+ *
+ * Multiplying this factor with the current absolute wind estimate gives the airspeed offset
+ * added to the minimum airspeed setpoint limit. This helps to make the
+ * system more robust against disturbances (turbulence) in high wind.
+ * Only applies to AUTO flight mode.
+ *
+ * airspeed_min_adjusted = FW_AIRSPD_MIN + FW_WIND_ARSP_SC * wind.length()
+ *
+ * @min 0
+ * @decimal 2
+ * @increment 0.01
+ * @group FW TECS
+ */
+PARAM_DEFINE_FLOAT(FW_WIND_ARSP_SC, 0.f);