Abstract: In a triplex redundant digital control system, one of three computer units is selected for controlling a digital flight control system by using fault scoring and selection logic circuitry that responds to discrete signals produced by the computer units that represent both self-test and cross-test information on the health of the three available units. The self-test and cross-test discrete information signals are received and processed by the selection logic circuit in accordance with a fault-scoring scheme in which the self-test scores are accorded different and, in particular, greater weight than the cross-test scores and a computer unit exhibiting the lowest combined self- and cross-test fault score is selected as the computer in control. The circuitry also includes memory devices for storing the fault scores associated with previous fault conditions so that a previously unfailed computer unit is selected over a previously failed but currently healthy computer.