diff --git a/src/modules/fw_pos_control/FixedwingPositionControl.cpp b/src/modules/fw_pos_control/FixedwingPositionControl.cpp
index 4b0a391fc5bc..b9dc214f3412 100644
--- a/src/modules/fw_pos_control/FixedwingPositionControl.cpp
+++ b/src/modules/fw_pos_control/FixedwingPositionControl.cpp
@@ -129,8 +129,8 @@ FixedwingPositionControl::parameters_update()
 	_tecs.set_speed_weight(_param_fw_t_spdweight.get());
 	_tecs.set_equivalent_airspeed_trim(_performance_model.getCalibratedTrimAirspeed());
 	_tecs.set_equivalent_airspeed_min(_performance_model.getMinimumCalibratedAirspeed());
-	_tecs.set_throttle_damp(_param_fw_t_thr_damp.get());
-	_tecs.set_integrator_gain_throttle(_param_fw_t_I_gain_thr.get());
+	_tecs.set_throttle_damp(_param_fw_t_thr_damping.get());
+	_tecs.set_integrator_gain_throttle(_param_fw_t_thr_integ.get());
 	_tecs.set_integrator_gain_pitch(_param_fw_t_I_gain_pit.get());
 	_tecs.set_throttle_slewrate(_param_fw_thr_slew_max.get());
 	_tecs.set_vertical_accel_limit(_param_fw_t_vert_acc.get());
diff --git a/src/modules/fw_pos_control/FixedwingPositionControl.hpp b/src/modules/fw_pos_control/FixedwingPositionControl.hpp
index 9f672ef2eeec..751904590b53 100644
--- a/src/modules/fw_pos_control/FixedwingPositionControl.hpp
+++ b/src/modules/fw_pos_control/FixedwingPositionControl.hpp
@@ -934,14 +934,14 @@ class FixedwingPositionControl final : public ModuleBase<FixedwingPositionContro
 
 		(ParamFloat<px4::params::FW_T_HRATE_FF>) _param_fw_t_hrate_ff,
 		(ParamFloat<px4::params::FW_T_ALT_TC>) _param_fw_t_h_error_tc,
-		(ParamFloat<px4::params::FW_T_I_GAIN_THR>) _param_fw_t_I_gain_thr,
+		(ParamFloat<px4::params::FW_T_THR_INTEG>) _param_fw_t_thr_integ,
 		(ParamFloat<px4::params::FW_T_I_GAIN_PIT>) _param_fw_t_I_gain_pit,
 		(ParamFloat<px4::params::FW_T_PTCH_DAMP>) _param_fw_t_ptch_damp,
 		(ParamFloat<px4::params::FW_T_RLL2THR>) _param_fw_t_rll2thr,
 		(ParamFloat<px4::params::FW_T_SINK_MAX>) _param_fw_t_sink_max,
 		(ParamFloat<px4::params::FW_T_SPDWEIGHT>) _param_fw_t_spdweight,
 		(ParamFloat<px4::params::FW_T_TAS_TC>) _param_fw_t_tas_error_tc,
-		(ParamFloat<px4::params::FW_T_THR_DAMP>) _param_fw_t_thr_damp,
+		(ParamFloat<px4::params::FW_T_THR_DAMPING>) _param_fw_t_thr_damping,
 		(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_SEB_R_FF>) _param_seb_rate_ff,
diff --git a/src/modules/fw_pos_control/fw_path_navigation_params.c b/src/modules/fw_pos_control/fw_path_navigation_params.c
index 07518de71087..a636d8d75768 100644
--- a/src/modules/fw_pos_control/fw_path_navigation_params.c
+++ b/src/modules/fw_pos_control/fw_path_navigation_params.c
@@ -465,38 +465,34 @@ PARAM_DEFINE_FLOAT(FW_T_SINK_MAX, 5.0f);
  * Increase to add damping to correct for oscillations in speed and height.
  *
  * @min 0.0
- * @max 2.0
- * @decimal 2
- * @increment 0.1
+ * @max 1.0
+ * @decimal 3
+ * @increment 0.01
  * @group FW TECS
  */
-PARAM_DEFINE_FLOAT(FW_T_THR_DAMP, 0.1f);
+PARAM_DEFINE_FLOAT(FW_T_THR_DAMPING, 0.05f);
 
 /**
  * Integrator gain throttle
  *
- * This is the integrator gain on the throttle part of the control loop.
- * Increasing this gain increases the speed at which speed
- * and height offsets are trimmed out, but reduces damping and
- * increases overshoot. Set this value to zero to completely
- * disable all integrator action.
+ * Integrator gain on the throttle part of the control loop.
+ * Increase it to trim out speed and height offsets faster,
+ * with the downside of possible overshoots and oscillations.
  *
  * @min 0.0
- * @max 2.0
- * @decimal 2
- * @increment 0.05
+ * @max 1.0
+ * @decimal 3
+ * @increment 0.005
  * @group FW TECS
  */
-PARAM_DEFINE_FLOAT(FW_T_I_GAIN_THR, 0.05f);
+PARAM_DEFINE_FLOAT(FW_T_THR_INTEG, 0.02f);
 
 /**
  * Integrator gain pitch
  *
- * This is the integrator gain on the pitch part of the control loop.
- * Increasing this gain increases the speed at which speed
- * and height offsets are trimmed out, but reduces damping and
- * increases overshoot. Set this value to zero to completely
- * disable all integrator action.
+ * Integrator gain on the pitch part of the control loop.
+ * Increase it to trim out speed and height offsets faster,
+ * with the downside of possible overshoots and oscillations.
  *
  * @min 0.0
  * @max 2.0