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

<airframe>
  <section name="IMU" prefix="IMU_">
    <!-- Magneto calibration -->
    <define name="MAG_X_NEUTRAL" value="-52"/>
    <define name="MAG_Y_NEUTRAL" value="-58"/>
    <define name="MAG_Z_NEUTRAL" value="187"/>
    <define name="MAG_X_SENS" value="7.31288049757" integer="16"/>
    <define name="MAG_Y_SENS" value="7.25278204203" integer="16"/>
    <define name="MAG_Z_SENS" value="7.79836316136" 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>
