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A system for automated testing of Ethernet signals of a unit under test (UUT) in a simulated Avionics Full Duplex (AFDX) network environment. The UUT may be any Ethernet device, including a 24 port Ethernet switch. Ethernet signal are received from a UUT by a measurement module that is adapted to mo

A system for automated testing of Ethernet signals of a unit under test (UUT) in a simulated Avionics Full Duplex (AFDX) network environment. The UUT may be any Ethernet device, including a 24 port Ethernet switch. Ethernet signal are received from a UUT by a measurement module that is adapted to modify the Ethernet signals according to a condition indicative of an AFDX network environment. Such modification includes attenuating the Ethernet signals with an RF attenuator or terminating the Ethernet signals with a 10 Base-T Ethernet simulation circuit. Modified signals are then monitored or evaluated to determine functionality of the UUT.

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1. A system for automated testing of Ethernet signals of a physical unit under test (UUT) in a simulated Avionics Full Duplex (AFDX) network environment, the system comprising: a measurement module adapted for connecting to the physical UUT and receiving Ethernet signals originating from the physica

1. A system for automated testing of Ethernet signals of a physical unit under test (UUT) in a simulated Avionics Full Duplex (AFDX) network environment, the system comprising: a measurement module adapted for connecting to the physical UUT and receiving Ethernet signals originating from the physical UUT and modifying the Ethernet signals according to a condition indicative of an AFDX network environment;a switching module coupled to the measurement module defining a path of communication of the modified Ethernet signals; anda data storage module receiving and storing data derived from the Ethernet signals, wherein the path is between the switching module and one of a plurality of channels of the data storage module. 2. The system of claim 1, wherein the measurement module further comprises an RF attenuator to attenuate the Ethernet signals. 3. The system of claim 2, wherein the measurement module further comprises a 10 Base-T Ethernet simulation circuit that attenuates a transmit signal of the Ethernet signals from the UUT. 4. The system of claim 1, further comprising a display module coupled to the plurality of channels of the data storage module. 5. The system of claim 4, wherein the display module is an oscilloscope. 6. The system of claim 1, further comprising the UUT. 7. The system of claim 6, wherein the UUT is a 24 port Ethernet switch. 8. The system of claim 1, wherein the switching module comprises RF switches to define the path of the modified Ethernet signals. 9. The system of claim 1, wherein the data storage module stores data representative of the characteristics of the modified Ethernet signals, such characteristics include at least one of a differential signal, amplitude symmetry, rise time, fall time, duty cycle distortion, transmit jitter, and overshoot. 10. A method for automated testing of Ethernet signals of a physical unit under test (UUT) in a simulated Avionics Full DupleX (AFDX) network environment, the method comprising: connecting a measurement module to the physical UUT;receiving Ethernet signals originating from the physical UUT;modifying the Ethernet signals according to a condition indicative of an AFDX network environment;defining a path of communication for the modified Ethernet signals to a data storage module; andtransmitting the modified Ethernet signals on the defined path to a channel of the data storage module. 11. The method of claim 10, and further comprising attenuating the Ethernet signals. 12. The method of claim 11, and further comprising attenuating the Ethernet signals to a level indicative of a 10 Base-T Ethernet signal. 13. The method of claim 10, and further comprising displaying the modified Ethernet signals. 14. The method of claim 10, wherein defining the path of communication to the data storage module includes switching an RF relay to define the path for transmitting the Ethernet signals. 15. The method of claim 10, and further comprising measuring the modified Ethernet signals to determine characteristics of the Ethernet signals, which characteristics include at least one of a differential signal, amplitude symmetry, rise time, fall time, duty cycle distortion, transmit jitter, and overshoot. 16. A device for receiving Ethernet signals from a physical unit under test (UUT) and modifying the Ethernet signals in order to simulate an Avionics Full DupleX (AFDX) network environment, the device comprising: a measurement module adapted for connecting to the physical UUT and receiving the Ethernet signals originating from the physical UUT and modifying the Ethernet signals according to a condition indicative of an AFDX network environment;a measurement probe measuring the modified Ethernet signals; anda switching module receiving the measured Ethernet signals and defining a path of communication from the switching module. 17. The device of claim 16, wherein the measurement module further comprises an RF attenuator to attenuate the Ethernet signals. 18. The device of claim 16, wherein the measurement module further comprises a 10 Base-T Ethernet simulation circuit that attenuates the Ethernet signals from the UUT. 19. The device of claim 16, wherein the switching module receives directions from a controller for defining the path of communication from the switching module to one of a plurality of channels on an oscilloscope for displaying the measured Ethernet signal. 20. The system of claim 1, wherein the Ethernet signals received by the measurement module are Full-Duplex Ethernet signals. 21. The method of claim 10, wherein the Ethernet signals received from the UUT are Full-Duplex Ethernet signals. 22. The device of claim 16, wherein the Ethernet signals received by the measurement module are Full-Duplex Ethernet signals.