A test apparatus comprises a computer-implemented core test unit including a plurality of software modules, each being associated with a driver 14a, and being configured to perform a specified test by simulating a predetermined condition, generating at least one stimulus signal and receiving response data. The apparatus comprises adaptor units or looms 16, each loom being connected between the core test unit 12 and a unit under test (UUT) 18, so as to facilitate data transfer. Each loom 16 is associated with a software module of the core test unit 12 and includes a data storage module having operational data configured to activate a specified software module when it is connected; the operational data is transferred to the core test unit 12 in use, and each loom 16 is configured to effect data transfer between said respective specified software module and said unit under test 18 by transmitting the stimulus signal received from the specified software module to the UUT 18 and transmitting the response data received from the UUT to the specified software module. The apparatus also comprises a user interface module 10 to output test data generated using the response data.
Avionics ground test rig system
2021-12-15
Patent
Elektronische Ressource
Englisch
IPC: | B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen / G06F ELECTRIC DIGITAL DATA PROCESSING , Elektrische digitale Datenverarbeitung / G01M TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES , Prüfen der statischen oder dynamischen Massenverteilung rotierender Teile von Maschinen oder Konstruktionen / G01R Messen elektrischer Größen , MEASURING ELECTRIC VARIABLES / H01R Elektrisch leitende Verbindungen , ELECTRICALLY-CONDUCTIVE CONNECTIONS |
Reconfigurable avionics test platform - Avionics Test Bench and Avionics Test Studio
Emerald Group Publishing | 2008
Online Contents | 1996
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