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

<airframe>
  <section name="IMU" prefix="IMU_">
    <!-- Magneto calibration -->
<define name="MAG_X_NEUTRAL" value="25"/>
<define name="MAG_Y_NEUTRAL" value="15"/>
<define name="MAG_Z_NEUTRAL" value="-55"/>
<define name="MAG_X_SENS" value="7.41844640022" integer="16"/>
<define name="MAG_Y_SENS" value="7.37548054866" integer="16"/>
<define name="MAG_Z_SENS" value="7.76207768102" integer="16"/>



    <!-- Magneto current calibration -->
<define name= "MAG_X_CURRENT_COEF" value="0.00194778573768"/>
<define name= "MAG_Y_CURRENT_COEF" value="-0.00279087354538"/>
<define name= "MAG_Z_CURRENT_COEF" value="0.00591470539289"/>

  </section>
</airframe>
