diff --git a/sw/airborne/booz/stabilization/booz_stabilization_attitude.h b/sw/airborne/booz/stabilization/booz_stabilization_attitude.h
index 6841e75c4d..c5989aa974 100644
--- a/sw/airborne/booz/stabilization/booz_stabilization_attitude.h
+++ b/sw/airborne/booz/stabilization/booz_stabilization_attitude.h
@@ -38,6 +38,9 @@ extern void booz_stabilization_attitude_run(bool_t  in_flight);
 extern void booz_stabilization_attitude_ref_init(void);
 extern void booz_stabilization_attitude_ref_update(void);
 
+extern float booz_stabilization_attitude_beta_vane_gain;
+extern float booz_stabilization_attitude_alpha_vane_gain;
+
 
 #define booz_stabilization_attitude_SetKiPhi(_val) {	\
     booz_stabilization_igain.x = _val;			\
diff --git a/sw/airborne/booz/stabilization/booz_stabilization_attitude_quat_float.c b/sw/airborne/booz/stabilization/booz_stabilization_attitude_quat_float.c
index 1c933a8915..c6de1e7539 100644
--- a/sw/airborne/booz/stabilization/booz_stabilization_attitude_quat_float.c
+++ b/sw/airborne/booz/stabilization/booz_stabilization_attitude_quat_float.c
@@ -41,6 +41,9 @@ struct FloatEulers booz_stabilization_att_sum_err;
 float booz_stabilization_att_fb_cmd[COMMANDS_NB];
 float booz_stabilization_att_ff_cmd[COMMANDS_NB];
 
+float booz_stabilization_attitude_beta_vane_gain;
+float booz_stabilization_attitude_alpha_vane_gain;
+
 
 void booz_stabilization_attitude_init(void) {
 
@@ -69,6 +72,11 @@ void booz_stabilization_attitude_init(void) {
   FLOAT_QUAT_ZERO( booz_stabilization_sum_err );
   FLOAT_EULERS_ZERO( booz_stabilization_att_sum_err );
 
+#ifdef USE_VANE
+  booz_stabilization_attitude_alpha_vane_gain = BOOZ_STABILIZATION_ATTITUDE_ALPHA_VANE_T;
+  booz_stabilization_attitude_beta_vane_gain = BOOZ_STABILIZATION_ATTITUDE_BETA_VANE_T;
+#endif
+
 }
 
 static void reset_psi_ref_from_body(void) {
@@ -149,7 +157,8 @@ void booz_stabilization_attitude_read_beta_vane(float beta)
   struct FloatEulers sticks_eulers;
   struct FloatQuat sticks_quat, prev_sp_quat;
 
-  sticks_eulers.phi = BOOZ_STABILIZATION_ATTITUDE_BETA_VANE_T * beta / RC_UPDATE_FREQ;
+
+  sticks_eulers.phi = booz_stabilization_attitude_beta_vane_gain * beta / RC_UPDATE_FREQ;
   sticks_eulers.theta = 0;
   sticks_eulers.psi = 0;
 
@@ -166,7 +175,7 @@ void booz_stabilization_attitude_read_alpha_vane(float alpha)
   struct FloatEulers sticks_eulers;
   struct FloatQuat sticks_quat, prev_sp_quat;
   sticks_eulers.phi = 0;
-  sticks_eulers.theta = BOOZ_STABILIZATION_ATTITUDE_ALPHA_VANE_T * alpha / RC_UPDATE_FREQ;
+  sticks_eulers.theta = booz_stabilization_attitude_alpha_vane_gain * alpha / RC_UPDATE_FREQ;
   sticks_eulers.psi = 0;
 
   // convert eulers to quaternion