<!DOCTYPE airframe SYSTEM "../../airframe.dtd">

<airframe>
  <section name="IMU" prefix="IMU_">
    <!-- Magneto calibration -->

    <!-- MAGNETO CALIBRATION ANTWERP -->
<define name="MAG_X_NEUTRAL" value="-518"/>
<define name="MAG_Y_NEUTRAL" value="-282"/>
<define name="MAG_Z_NEUTRAL" value="-305"/>
<define name="MAG_X_SENS" value="3.77332912301" integer="16"/>
<define name="MAG_Y_SENS" value="4.27226640255" integer="16"/>
<define name="MAG_Z_SENS" value="3.64337128259" integer="16"/>


    <!-- MAGNETO CURRENT CALIBRATION -->
    <define name= "MAG_X_CURRENT_COEF" value="-0.0176704713698"/>
    <define name= "MAG_Y_CURRENT_COEF" value="0.0174222594634"/>
    <define name= "MAG_Z_CURRENT_COEF" value="0.0187570316492"/>
  </section>
</airframe>
