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 1e5c574bb4e..89ceea71ff3 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
@@ -528,11 +528,11 @@ PARAM_DEFINE_FLOAT(FW_T_SINK_MAX, 5.0f);
  *
  * @min 0.0
  * @max 2.0
- * @decimal 1
+ * @decimal 2
  * @increment 0.1
  * @group FW TECS
  */
-PARAM_DEFINE_FLOAT(FW_T_THR_DAMP, 0.5f);
+PARAM_DEFINE_FLOAT(FW_T_THR_DAMP, 0.1f);
 
 /**
  * Integrator gain
@@ -639,11 +639,11 @@ PARAM_DEFINE_FLOAT(FW_T_SPDWEIGHT, 1.0f);
  *
  * @min 0.0
  * @max 2.0
- * @decimal 1
+ * @decimal 2
  * @increment 0.1
  * @group FW TECS
  */
-PARAM_DEFINE_FLOAT(FW_T_PTCH_DAMP, 0.0f);
+PARAM_DEFINE_FLOAT(FW_T_PTCH_DAMP, 0.1f);
 
 /**
  * Altitude error time constant.
@@ -664,7 +664,7 @@ PARAM_DEFINE_FLOAT(FW_T_ALT_TC, 5.0f);
  * @increment 0.05
  * @group FW TECS
  */
-PARAM_DEFINE_FLOAT(FW_T_HRATE_FF, 0.8f);
+PARAM_DEFINE_FLOAT(FW_T_HRATE_FF, 0.4f);
 
 /**
  * True airspeed error time constant.
@@ -674,7 +674,7 @@ PARAM_DEFINE_FLOAT(FW_T_HRATE_FF, 0.8f);
  * @increment 0.5
  * @group FW TECS
  */
-PARAM_DEFINE_FLOAT(FW_T_TAS_TC, 10.0f);
+PARAM_DEFINE_FLOAT(FW_T_TAS_TC, 5.0f);
 
 /**
  * Minimum groundspeed
@@ -729,4 +729,4 @@ PARAM_DEFINE_FLOAT(FW_T_STE_R_TC, 0.4f);
  * @increment 0.01
  * @group FW TECS
  */
-PARAM_DEFINE_FLOAT(FW_T_TAS_R_TC, 0.4f);
+PARAM_DEFINE_FLOAT(FW_T_TAS_R_TC, 0.05f);