the reduced thrust value
@ -334,7 +334,7 @@ MultirotorMixer::mix(float *outputs, unsigned space, uint16_t *status_reg)
} else {
yaw = (1.0f - ((roll * _rotors[i].roll_scale + pitch * _rotors[i].pitch_scale) *
roll_pitch_scale + thrust + boost)) / _rotors[i].yaw_scale;
roll_pitch_scale + (thrust - thrust_reduction) + boost)) / _rotors[i].yaw_scale;
}