<airframe>

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

    <!-- Accelerometer calibration -->
    <define name="ACCEL_X_NEUTRAL" value="-67"/>
    <define name="ACCEL_Y_NEUTRAL" value="-19"/>
    <define name="ACCEL_Z_NEUTRAL" value="219"/>
    <define name="ACCEL_X_SENS" value="2.44402019869" integer="16"/>
    <define name="ACCEL_Y_SENS" value="2.44875128187" integer="16"/>
    <define name="ACCEL_Z_SENS" value="2.42587369757" integer="16"/>

    <!-- Magnetometer calibration -->
    <define name="MAG_X_NEUTRAL" value="-68"/>
    <define name="MAG_Y_NEUTRAL" value="-333"/>
    <define name="MAG_Z_NEUTRAL" value="-305"/>
    <define name="MAG_X_SENS" value="8.27980230766" integer="16"/>
    <define name="MAG_Y_SENS" value="8.37184374456" integer="16"/>
    <define name="MAG_Z_SENS" value="6.60725149679" integer="16"/>

    <!-- Magnetometer current calibration -->
    <define name= "MAG_X_CURRENT_COEF" value="-0.00284737868011"/>
    <define name= "MAG_Y_CURRENT_COEF" value="0.00240832136469"/>
    <define name= "MAG_Z_CURRENT_COEF" value="-0.000908830770325"/>

    <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>
