System interface fault isolator test set

• US 5,479,610 A
• Filed: 11/01/1993
• Issued: 12/26/1995
• Est. Priority Date: 11/01/1993
• Status: Expired due to Term

• Current Assignee: Northrop Grumman Systems Corporation (Northrop Grumman Corporation)
• Original Assignee: Northrop Grumman Corporation
• Inventors: Roll-Mecak, Doru T., Teich, Stanley
• Primary Examiner(s): Beausoliel, Jr., Robert W.
• Assistant Examiner(s): Decady, Albert
• Application Number:
  US08/144,318
• Time in Patent Office: 785 Days
• Field of Search: 371/15.1, 371/22.4, 371/25.1, 371/27, 364/267.7, 324/527, 324/528, 324/533, 324/500, 324/512, 324/534, 395/575
• US Class Current: 714/25
• CPC Class Codes: G01R 31/11 using pulse reflection methods
• CPC Class Codes: G01R 31/2822 of microwave or radiofrequency circuits of attenuation, gain, e.g. using network analyzers G01R27/28
• CPC Class Codes: G06F 11/221 to test buses, lines or interfaces, e.g. stuck-at or open line faults

Abstract

A system interface fault isolator uses time domain reflectometry test techniques to isolate faults from only one end of a cable, a cable string or component without requiring removal of the cable or component from the system interface. A separate maintenance control unit includes a mass storage means for storing TDR or VSWR signatures of a variety of systems and comparing the signatures with data obtained by the TDR measurement board connected to the cable or component to be tested. VSWR data is obtained by processing the TDR data using software built-in the maintenance control unit. The control unit is programmable to accommodate a variety of different system interfaces, and bit status data can be downloaded directly to the control unit. Two adaptors are also provided, one of which is connected to the control unit to analyze a multi-line digital bus, and the other of which allows differential TDR measurements to be taken by the SI-FI on a MIL-STD-1553 bus.

Claims

1. A system interface fault isolator apparatus, comprising:

TDR/oscilloscope measurement circuitry housed in a measurement unit, said TDR/oscilloscope measurement circuitry including

means including a time domain reflectometer for performing time domain reflectometry tests on a signal cable, signal cable string, component in a system, or system interface in order to detect faults and determine their location; and

means for measuring at least one parameter of a signal in said signal cable, signal cable string, component in a system, or system interface;

means for connecting the TDR/oscilloscope measurement circuitry to an input switch means which selects an appropriate input channel of the measurement unit;

means for connecting the measurement unit to said signal cable, signal cable string, component in a system, or system interface under test;

means for protecting the measurement unit from accidental ESD by discharging any capacitively stored energy present in said connection means before measurements are made;

means for detecting a live circuit condition at the input of the measurement unit;

a separate maintenance control unit which includes mass storage means for storing reference data, test limits data and test results data for a plurality of different components, systems or system interfaces under test;

means for connecting the maintenance control unit to the TDR/oscilloscope measurement circuitry to cause the reflectometer to perform a measurement and upload test results data to the control unit, and processor means for comparing the test results data with reference and test limits data stored in the mass storage means of said control unit.

2. Apparatus as claimed in claim 1, wherein said measurement unit further comprises means for disconnecting the maintenance control unit from said measurement unit to allow stand alone use of said maintenance control unit.

3. Apparatus as claimed in claim 1, wherein said maintenance control unit further comprises means for disconnecting the maintenance control unit from the measurement unit to allow stand alone use of said maintenance control unit.

4. Apparatus as claimed in claim 1, wherein said measurement means includes means for performing measurements including impedance, frequency, voltage, rise time, pulse width and RF path loss in a unit under test, and wherein a bus architecture of the apparatus permits still further measurement performing means to be added as needed.

5. Apparatus as claimed in claim 1, wherein the maintenance control unit comprises means for performing a Fast Fourier Transform on the TDR data in order to obtain a voltage standing wave ratio (VSWR) profile of a component path.

6. Apparatus as claimed in claim 1, wherein the maintenance control unit includes means for downloading aircraft bit status data from an aircraft for post-flight analysis.

7. Apparatus as claimed in claim 1, wherein the TDR measurement unit and maintenance control unit each comprises its own power supply.

8. Apparatus as claimed in claim 1, further comprising a thru-line bus test adaptor for a parallel data bus, comprising means including a bus isolator placed between a bus controller and remote terminal for providing a signal path while DC isolating the bus controller from the remote terminal, a driver/receiver pair for each data and control line, and a reconfigurable test interface connected between the driver/receiver pairs and the maintenance control unit.

9. Apparatus as claimed in claim 1, further comprising a MIL-STD-1553 bus test adaptor which includes two identical impedance converter/delay normalization circuits connected between the time domain reflectometer and a MIL-STD-1553 bus, in order to perform differential TDR measurements on said MIL-STD-1553 bus.

10. Apparatus as claimed in claim 1, wherein said maintenance control unit and measurement unit are portable.

11. A system interface fault isolator apparatus, comprising:

a portable measurement unit containing a plurality of test instruments connected by means including a bus to which additional instrument modules can be connected for performing different types of measurements on different types of interfaces; and

a separate maintenance control unit which includes mass storage means for storing system interface data for a plurality of different system interfaces and processor means for comparing the system interface data with data obtained from said test instruments under control of a program in said maintenance control unit.

wherein said plurality of test instruments includes means for measuring at least one parameter of a signal in a signal cable, signal cable string, component in a system, or system interface, said at least one parameter including at least one parameter selected from the group consisting of;

frequency, voltage, rise time, and pulse width;

means for protecting the measurement unit from accidental ESD by discharging any capacitively stored energy present in a connection means before measurements are made;

means for detecting a live circuit condition at the input of the measurement unit; and

means for connecting the measurement unit to said signal cable, signal cable string, component in a system, or system interface under test and for connecting the maintenance control unit to the measurement unit to cause the measurement performing means to perform a measurement of said at least one parameter and upload test results data to the control unit.

12. Apparatus as claimed in claim 11, wherein said plurality of test instruments contained in said measurement unit includes an RF signal source.

13. Apparatus as claimed in claim 11, wherein said plurality of test instruments contained in said measurement unit includes an optical TDR.

14. Apparatus as claimed in claim 11, wherein said maintenance control unit further comprises means for disconnecting the maintenance control unit from the measurement unit to allow stand alone use.

15. Apparatus as claimed in claim 11, wherein said measurement unit includes instrument means for measuring impedance, frequencies, voltage, rise time, and RF path loss in a unit under test.

16. Apparatus as claimed in claim 11, wherein the maintenance control unit includes means for downloading aircraft bit status data from an aircraft for post-flight analysis.

17. Apparatus as claimed in claim 11, wherein said maintenance control unit includes means for directly connecting to a MIL-STD-1553 data bus, and means for allowing said maintenance control unit to operate either as a bus controller, a remote terminal or a bus analyzer on said MIL-STD-1553 bus.

18. Apparatus as claimed in claim 11, wherein said maintenance control unit includes means for directly connecting to an IEEE-488 data bus, and means for allowing said maintenance control unit to operate either as a controller-in-charge, a device or a bus analyzer on said IEEE-488 bus.

19. Apparatus as claimed in claim 11, wherein said mass storage means of said maintenance control unit is removable.

20. Apparatus as claimed in claim 11, further comprising a thru-line bus test adaptor for a parallel data bus, comprising means including a bus isolator, a driver/receiver pair for each data and control line and a reconfigurable test interface, wherein said reconfigurable test interface can be reconfigured by means of software uploaded from said maintenance control unit.

21. Apparatus as claimed in claim 11, further comprising a thru-line bus test adaptor for a parallel data bus, comprising means including a bus isolator, a driver/receiver pair for each data and control line and a reconfigurable test interface, wherein said driver/receiver pair can accomodate either unipolar or differential inputs and outputs.