diff --git a/src/modules/fw_dyn_soar_control/fw_dyn_soar_control_params.c b/src/modules/fw_dyn_soar_control/fw_dyn_soar_control_params.c
index 4bd3846bea..9203089210 100644
--- a/src/modules/fw_dyn_soar_control/fw_dyn_soar_control_params.c
+++ b/src/modules/fw_dyn_soar_control/fw_dyn_soar_control_params.c
@@ -179,7 +179,7 @@ PARAM_DEFINE_FLOAT(C_D2, 1.984f);
  * @increment 0.0001
  * @group FW DYN SOAR Control
  */
-PARAM_DEFINE_FLOAT(FILTER_A1, 0.53010968f);
+PARAM_DEFINE_FLOAT(FILTER_A1, 1.16826067f);
 
 /**
  * coefficients of the butterworth filter used for smoothing the IMU
@@ -191,7 +191,7 @@ PARAM_DEFINE_FLOAT(FILTER_A1, 0.53010968f);
  * @increment 0.0001
  * @group FW DYN SOAR Control
  */
-PARAM_DEFINE_FLOAT(FILTER_A2, -0.22169409f);
+PARAM_DEFINE_FLOAT(FILTER_A2, -0.42411821f);
 
 /**
  * coefficients of the butterworth filter used for smoothing the IMU
@@ -203,7 +203,7 @@ PARAM_DEFINE_FLOAT(FILTER_A2, -0.22169409f);
  * @increment 0.0001
  * @group FW DYN SOAR Control
  */
-PARAM_DEFINE_FLOAT(FILTER_B1, 0.1728961f);
+PARAM_DEFINE_FLOAT(FILTER_B1, 0.06396438f);
 
 /**
  * coefficients of the butterworth filter used for smoothing the IMU
@@ -215,7 +215,7 @@ PARAM_DEFINE_FLOAT(FILTER_B1, 0.1728961f);
  * @increment 0.0001
  * @group FW DYN SOAR Control
  */
-PARAM_DEFINE_FLOAT(FILTER_B2, 0.3457922f);
+PARAM_DEFINE_FLOAT(FILTER_B2, 0.12792877f);
 
 /**
  * coefficients of the butterworth filter used for smoothing the IMU
@@ -227,7 +227,7 @@ PARAM_DEFINE_FLOAT(FILTER_B2, 0.3457922f);
  * @increment 0.0001
  * @group FW DYN SOAR Control
  */
-PARAM_DEFINE_FLOAT(FILTER_B3, 0.1728961f);
+PARAM_DEFINE_FLOAT(FILTER_B3, 0.06396438f);
 
 // ========================================================
 // =================== CONTROL GAINS ======================