Functional avionic core tester

Electricity: measuring and testing – Measuring – testing – or sensing electricity – per se – With rotor

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324 731, 371 151, G01R 3102, G01R 3128

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active

052237885

ABSTRACT:
A testing system, in particular for weapons and avionics applications, includes a bus interface unit capable of operating as a bus controller, a remote terminal, and a monitor. The bus interface unit is compatible with military standard buses and is controlled using an enhanced Atlas test programming language. Test instruments are provided on cards using a two-part architecture in which common test instruments are arranged as part of a core tester unit while application-specific enhanced are controlled by a separate microprocessor in a functional interface unit.

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William A. Bostrom and Henry J. Baluta, "Fast Functional Avionics System Tester," Sep. 17, 1990, Auto Test Con Conference Report, pp. 9-14.
IEEE Standard 716-1989, pp. 13-2 to 13-9.

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