The CADC receives pressures from the aircraft's pitot tube. One problem is that the airflow over the aircraft distorts the static pressure reading. The fix is to apply a Pressure Error Correction factor. This factor is determined by the Compensator, an external unit. 6/12
The Compensator uses a 3-D cam to generate the correction factor, sent to the CADC as a synchro signal. The CADC uses a servo loop to generate a rotation corresponding to this factor, then multiplies it with a differential. 7/12