Built-in test for satellite digital payload verification

• US 9,720,042 B2
• Filed: 05/21/2014
• Issued: 08/01/2017
• Est. Priority Date: 05/21/2014
• Status: Active Grant

• Current Assignee: The Boeing Co.
• Original Assignee: The Boeing Co.
• Inventors: Chiu, Robert Conder, Bolton, Robert Emerson, Behboudikha, Payman, Jaque, Philip Stewart
• Primary Examiner(s): Blair, April Y
• Assistant Examiner(s): NGUYEN, THIEN DANG
• Application Number:
  US14/283,950
• Publication Number:
  US 20150339205A1
• Time in Patent Office: 1,168 Days
• CPC Class Codes: B64G 1/00 Cosmonautic vehicles
• CPC Class Codes: B64G 1/428 Power distribution and management
• CPC Class Codes: B64G 1/66 Arrangements or adaptations of apparatus or instruments, not otherwise provided for
• CPC Class Codes: G01R 31/3187 Built-in tests
• CPC Class Codes: G06F 11/263 Generation of test inputs, e.g. test vectors, patterns or sequences ; with adaptation of the tested hardware for testability with external testers
• CPC Class Codes: G06F 11/27 Built-in tests

Abstract

According to an embodiment, a testing system for a satellite payload includes a built-in testing component configured at a satellite, the built-in testing component comprising a built-in testing component input and a built-in testing component output, and a payload component configured at the satellite, the payload component comprising a payload component input communicatively connected to the built-in testing component output and a payload component output communicatively connected to the built-in testing component input, wherein the built-in testing component is configured to transmit a digital test signal from the built-in testing component output to the payload component input and receive a digital output signal at the built-in testing component input from the payload component output.

Claims

1. A testing system for a satellite payload, the testing system comprising:

a built-in testing component installed in a satellite, the built-in testing component comprising a built-in testing component input and a built-in testing component output; and

a payload component installed in the satellite, the payload component comprising a payload component input communicatively connected to the built-in testing component output and a payload component output communicatively connected to the built-in testing component input,

wherein the built-in testing component is configured to transmit a digital test signal from the built-in testing component output to the payload component input and receive a digital output signal at the built-in testing component input from the payload component output;

wherein the built-in testing component is configured to transmit the digital output signal from the payload component output to the payload component input to create a loop for loopback testing; and

wherein the digital test signal is generated so that any added distortion is a result of tested components.

2. The testing system of claim 1, wherein the built-in testing component is further configured to generate the digital test signal.

3. The testing system of claim 2, wherein the built-in testing component is further configured to generate the digital test signal in response to receiving a test signal from an external stimulus device.

4. The testing system of claim 2, wherein the built-in testing component is further configured to generate the digital test signal in response to receiving an instruction to generate the digital test signal.

5. The testing system of claim 1, wherein the built-in testing component is further configured to evaluate the digital output signal received from the payload component output.

6. The testing system of claim 5, wherein the built-in testing component is further configured to transmit results of evaluating the digital output signal received from the payload component output to an external device.

7. The testing system of claim 1, wherein the satellite is configured in an environmental chamber.

8. A testing system for a satellite payload, the testing system comprising:

a plurality of built-in testing components installed in a satellite, each of the plurality of built-in testing components comprising a built-in testing component input and a built-in testing component output; and

a payload component installed in the satellite, the payload component comprising a plurality of payload component inputs each communicatively connected to a respective one of the built-in testing component outputs and a plurality of payload component outputs each communicatively connected to a respective one of the built-in testing component inputs,

wherein each of the plurality of built-in testing components is configured to transmit a digital test signal from its built-in testing component output to a respective payload component input and receive a digital output signal at its built-in testing component input from a respective payload component output;

wherein the built-in testing components are configured to transmit the digital output signal from the payload component outputs to the payload component inputs to create a loop for loopback testing; and

wherein the digital test signal is generated so that any added distortion is a result of tested components.

9. The testing system of claim 8, wherein each of the plurality of built-in testing components is further configured to generate the digital test signal.

10. The testing system of claim 9, wherein each of the plurality of built-in testing components is further configured to generate the digital test signal in response to receiving a test signal from an external stimulus device.

11. The testing system of claim 9, wherein each of the plurality of built-in testing components is further configured to generate the digital test signal in response to receiving an instruction to generate the digital test signal.

12. The testing system of claim 8, wherein each of the plurality of built-in testing components is further configured to evaluate the digital output signal received from the respective payload component output.

13. The testing system of claim 12, wherein each of the plurality of built-in testing components is further configured to transmit results of evaluating the digital output signal received from the respective payload component output to an external device.

14. The testing system of claim 8, wherein the satellite is configured in an environmental chamber.

15. A method of testing a payload component configured at a satellite, the method comprising:

transmitting, from a built-in testing component comprising a built-in testing component input and a built-in testing component output, a digital test signal from the built-in testing component output to a payload component input; and

receiving, at the built-in testing component input from a payload component output, a digital output signal,

wherein the built-in testing component and the payload component are configured at the satellite

wherein the payload component input is communicatively connected to the built-in testing component output and the payload component output is communicatively connected to the built-in testing component input and the payload component input to create a loop for loopback testing; and

wherein the digital test signal is generated so that any added distortion is a result of tested components.

16. The method of claim 15, further comprising generating the digital test signal at the built-in testing component.

17. The method of claim 16, wherein generating the digital test signal at the built-in testing component comprises generating the digital test signal in response to receiving a test signal from an external stimulus device.

18. The method of claim 16, wherein generating the digital test signal at the built-in testing component comprises generating the digital test signal in response to receiving an instruction to generate the digital test signal.

19. The method of claim 15, further comprising evaluating the digital output signal received from the payload component output at the built-in testing component.

20. The method of claim 19, further comprising transmitting, by the built-in testing component to an external device, results of evaluating the digital output signal received from the payload component output.