<airframe>

  <section name="IMU" prefix="IMU_">

    <!-- Accelerometer calibration -->
    <define name="ACCEL_X_NEUTRAL" value="-39"/>
    <define name="ACCEL_Y_NEUTRAL" value="-22"/>
    <define name="ACCEL_Z_NEUTRAL" value="-26"/>
    <define name="ACCEL_X_SENS" value="2.44700925154" integer="16"/>
    <define name="ACCEL_Y_SENS" value="2.45054927516" integer="16"/>
    <define name="ACCEL_Z_SENS" value="2.43828948519" integer="16"/>

    <!-- Magnetometer calibration -->
    <define name="MAG_X_NEUTRAL" value="-71"/>
    <define name="MAG_Y_NEUTRAL" value="-176"/>
    <define name="MAG_Z_NEUTRAL" value="84"/>
    <define name="MAG_X_SENS" value="9.8165895067" integer="16"/>
    <define name="MAG_Y_SENS" value="8.68135381265" integer="16"/>
    <define name="MAG_Z_SENS" value="6.74384859593" integer="16"/>

    <!-- Magnetometer current calibration -->
    <define name= "MAG_X_CURRENT_COEF" value="0.00351822710955"/>
    <define name= "MAG_Y_CURRENT_COEF" value="0.00208165834374"/>
    <define name= "MAG_Z_CURRENT_COEF" value="-0.00525676641302"/>

    <define name="BODY_TO_IMU_PHI"   value="0." unit="deg"/>
    <define name="BODY_TO_IMU_THETA" value="0." unit="deg"/>
    <define name="BODY_TO_IMU_PSI"   value="0." unit="deg"/>

  </section>

</airframe>
