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

<airframe>
  <section name="IMU" prefix="IMU_">
    <!-- Magneto calibration -->
    <define name="MAG_X_NEUTRAL" value="-16"/>
    <define name="MAG_Y_NEUTRAL" value="55"/>
    <define name="MAG_Z_NEUTRAL" value="204"/>
    <define name="MAG_X_SENS" value="7.28514789391" integer="16"/>
    <define name="MAG_Y_SENS" value="7.33022132691" integer="16"/>
    <define name="MAG_Z_SENS" value="7.57102035692" integer="16"/>

    <!-- Magneto current calibration -->
    <!--define name= "MAG_X_CURRENT_COEF" value="0.00129333644507"/>
    <define name= "MAG_Y_CURRENT_COEF" value="-0.00180224741034"/>
    <define name= "MAG_Z_CURRENT_COEF" value="0.00514030157101"/-->
  </section>
</airframe>
