AIR FORCE - MIL-STD-001591A
COMMAND, CONTROL AND COMMUNICATIONS(C3) SYSTEM 7 COMPONENT FAULT DIAGNOSIS, SUB-SYSTEMS, ANALYSIS/SYNTHESIS OF
| Organization: | AIR FORCE |
| Publication Date: | 8 December 1978 |
| Status: | inactive |
| Page Count: | 21 |
scope:
This standard establishes uniform criteria for conducting trade studies to determine the optimal design for command, control and communication system and component fault diagnosis/isolation subsystems, hereafter referred to as Fault Identification & Test Subsystems (FITS). FITS include the hardware and/or software necessary for the detection and isolation of failures.
This standard is applicable to Electronics Systems Division procurements which include the development of fault/detection isolation/diagnosis and test subsystems where:
a. Selections can be made among such alternatives as centrally controlled system built-in-test, individual system component (equipment) built-in-test, equipment subunit built-in-test, special purpose external test subsystems and testers or combinations of the preceding.
b. Different design and/or architectures exist for each alternative. Such subsystems are inclusive of system/equipment operational level fault detection coupled with built-in-test, and external test subsystems, as well as shop and depot level applicable built-in-test and testers.
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