diff --git a/src/lib/tecs/TECS.cpp b/src/lib/tecs/TECS.cpp
index 6306618573..3579fe42b8 100644
--- a/src/lib/tecs/TECS.cpp
+++ b/src/lib/tecs/TECS.cpp
@@ -436,7 +436,8 @@ void TECS::_update_pitch_setpoint()
 	}
 
 	// Calculate a specific energy correction that doesn't include the integrator contribution
-	float SEB_rate_correction = _SEB_rate_error * _pitch_damping_gain + _pitch_integ_state + SEB_rate_setpoint;
+	float SEB_rate_correction = _SEB_rate_error * _pitch_damping_gain + _pitch_integ_state + _SEB_rate_ff *
+				    SEB_rate_setpoint;
 
 	// During climbout, bias the demanded pitch angle so that a zero speed error produces a pitch angle
 	// demand equal to the minimum pitch angle set by the mission plan. This prevents the integrator
diff --git a/src/lib/tecs/TECS.hpp b/src/lib/tecs/TECS.hpp
index 2c39d931ce..f3ced9bfa3 100644
--- a/src/lib/tecs/TECS.hpp
+++ b/src/lib/tecs/TECS.hpp
@@ -131,6 +131,8 @@ public:
 	void set_ste_rate_time_const(float time_const) { _STE_rate_time_const = time_const; }
 	void set_speed_derivative_time_constant(float time_const) { _speed_derivative_time_const = time_const; }
 
+	void set_seb_rate_ff_gain(float ff_gain) { _SEB_rate_ff = ff_gain; }
+
 
 	// TECS status
 	uint64_t timestamp() { return _pitch_update_timestamp; }
@@ -224,6 +226,7 @@ private:
 	float _throttle_slewrate{0.0f};					///< throttle demand slew rate limit (1/sec)
 	float _STE_rate_time_const{0.1f};				///< filter time constant for specific total energy rate (damping path) (s)
 	float _speed_derivative_time_const{0.01f};			///< speed derivative filter time constant (s)
+	float _SEB_rate_ff{1.0f};
 
 	// complimentary filter states
 	float _vert_vel_state{0.0f};					///< complimentary filter state - height rate (m/sec)
diff --git a/src/modules/fw_pos_control_l1/FixedwingPositionControl.cpp b/src/modules/fw_pos_control_l1/FixedwingPositionControl.cpp
index 54a4c0f718..7efea241ec 100644
--- a/src/modules/fw_pos_control_l1/FixedwingPositionControl.cpp
+++ b/src/modules/fw_pos_control_l1/FixedwingPositionControl.cpp
@@ -125,6 +125,7 @@ FixedwingPositionControl::parameters_update()
 	_tecs.set_airspeed_error_time_constant(_param_fw_t_tas_error_tc.get());
 	_tecs.set_ste_rate_time_const(_param_ste_rate_time_const.get());
 	_tecs.set_speed_derivative_time_constant(_param_tas_rate_time_const.get());
+	_tecs.set_seb_rate_ff_gain(_param_seb_rate_ff.get());
 
 
 	// Landing slope
diff --git a/src/modules/fw_pos_control_l1/FixedwingPositionControl.hpp b/src/modules/fw_pos_control_l1/FixedwingPositionControl.hpp
index e376015dde..d6080394cd 100644
--- a/src/modules/fw_pos_control_l1/FixedwingPositionControl.hpp
+++ b/src/modules/fw_pos_control_l1/FixedwingPositionControl.hpp
@@ -394,6 +394,7 @@ private:
 		(ParamFloat<px4::params::FW_T_VERT_ACC>) _param_fw_t_vert_acc,
 		(ParamFloat<px4::params::FW_T_STE_R_TC>) _param_ste_rate_time_const,
 		(ParamFloat<px4::params::FW_T_TAS_R_TC>) _param_tas_rate_time_const,
+		(ParamFloat<px4::params::FW_T_SEB_R_FF>) _param_seb_rate_ff,
 
 		(ParamFloat<px4::params::FW_THR_ALT_SCL>) _param_fw_thr_alt_scl,
 		(ParamFloat<px4::params::FW_THR_CRUISE>) _param_fw_thr_cruise,
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 75475a76f6..26856cb788 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
@@ -761,3 +761,16 @@ PARAM_DEFINE_FLOAT(FW_T_STE_R_TC, 0.4f);
  * @group FW TECS
  */
 PARAM_DEFINE_FLOAT(FW_T_TAS_R_TC, 0.2f);
+
+
+/**
+ * Specific total energy balance rate feedforward gain.
+ *
+ *
+ * @min 0.5
+ * @max 3
+ * @decimal 2
+ * @increment 0.01
+ * @group FW TECS
+ */
+PARAM_DEFINE_FLOAT(FW_T_SEB_R_FF, 1.0f);