diff --git a/sw/airborne/firmwares/rotorcraft/autopilot.c b/sw/airborne/firmwares/rotorcraft/autopilot.c
index e9685f32c5..d33e24eaa9 100644
--- a/sw/airborne/firmwares/rotorcraft/autopilot.c
+++ b/sw/airborne/firmwares/rotorcraft/autopilot.c
@@ -102,7 +102,7 @@ void autopilot_set_mode(uint8_t new_autopilot_mode) {
     /* horizontal mode */
     switch (new_autopilot_mode) {
     case AP_MODE_FAILSAFE:
-#ifndef BOOZ_KILL_AS_FAILSAFE
+#ifndef KILL_AS_FAILSAFE
       booz_stab_att_sp_euler.phi = 0;
       booz_stab_att_sp_euler.theta = 0;
       booz2_guidance_h_mode_changed(BOOZ2_GUIDANCE_H_MODE_ATTITUDE);
@@ -135,7 +135,7 @@ void autopilot_set_mode(uint8_t new_autopilot_mode) {
     /* vertical mode */
     switch (new_autopilot_mode) {
     case AP_MODE_FAILSAFE:
-#ifndef BOOZ_KILL_AS_FAILSAFE
+#ifndef KILL_AS_FAILSAFE
       booz2_guidance_v_zd_sp = SPEED_BFP_OF_REAL(0.5);
       booz2_guidance_v_mode_changed(BOOZ2_GUIDANCE_V_MODE_CLIMB);
       break;