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

<airframe>
  <section name="IMU" prefix="IMU_">
    <!-- Magneto calibration -->
<define name="MAG_X_NEUTRAL" value="-54"/>
<define name="MAG_Y_NEUTRAL" value="-1"/>
<define name="MAG_Z_NEUTRAL" value="134"/>
<define name="MAG_X_SENS" value="7.55622140532" integer="16"/>
<define name="MAG_Y_SENS" value="7.72221931874" integer="16"/>
<define name="MAG_Z_SENS" value="7.84828034818" integer="16"/>



    <!-- Magneto current calibration -->
    <define name="MAG_X_CURRENT_COEF" value="0.0"/>
    <define name="MAG_Y_CURRENT_COEF" value="0.0"/>
    <define name="MAG_Z_CURRENT_COEF" value="0.0"/>
  </section>
</airframe>
