diff --git a/ArduPlane/tiltrotor.cpp b/ArduPlane/tiltrotor.cpp
index 05df5cdf88..4a2d04c580 100644
--- a/ArduPlane/tiltrotor.cpp
+++ b/ArduPlane/tiltrotor.cpp
@@ -144,8 +144,8 @@ void QuadPlane::tiltrotor_continuous_update(void)
         // Q_TILT_MAX. Anything above 50% throttle gets
         // Q_TILT_MAX. Below 50% throttle we decrease linearly. This
         // relies heavily on Q_VFWD_GAIN being set appropriately.
-        float settilt = constrain_float(SRV_Channels::get_output_scaled(SRV_Channel::k_throttle) / 50.0f, 0, 1);
-        tiltrotor_slew(settilt * tilt.max_angle_deg / 90.0f);
+       float settilt = constrain_float((SRV_Channels::get_output_scaled(SRV_Channel::k_throttle)-MAX(plane.aparm.throttle_min.get(),0)) / 50.0f, 0, 1);
+       tiltrotor_slew(settilt * tilt.max_angle_deg / 90.0f);
     }
 }
 
@@ -346,7 +346,6 @@ void QuadPlane::tiltrotor_vectoring(void)
 
     // calculate the basic tilt amount from current_tilt
     float base_output = zero_out + (tilt.current_tilt * (level_out - zero_out));
-
     // for testing when disarmed, apply vectored yaw in proportion to rudder stick
     // Wait TILT_DELAY_MS after disarming to allow props to spin down first.
     constexpr uint32_t TILT_DELAY_MS = 3000;