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

<airframe>
  <section name="IMU" prefix="IMU_">
    <!-- Magneto calibration -->
<define name="MAG_X_NEUTRAL" value="-120"/>
<define name="MAG_Y_NEUTRAL" value="54"/>
<define name="MAG_Z_NEUTRAL" value="49"/>
<define name="MAG_X_SENS" value="6.3026110969" integer="16"/>
<define name="MAG_Y_SENS" value="6.75366277396" integer="16"/>
<define name="MAG_Z_SENS" value="5.77699238143" integer="16"/>


    <!-- Magneto current calibration -->
<define name= "MAG_X_CURRENT_COEF" value="-0.00363854777985"/>
<define name= "MAG_Y_CURRENT_COEF" value="-0.000238563933841"/>
<define name= "MAG_Z_CURRENT_COEF" value="-0.00142141412685"/>

  </section>
</airframe>
