System and method for performing a test procedure

US11142345B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-11142345-B2
Application numberUS-201916546025-A
CountryUS
Kind codeB2
Filing dateAug 20, 2019
Priority dateJun 22, 2017
Publication dateOct 12, 2021
Grant dateOct 12, 2021

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  1. Title

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  2. Abstract

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  3. Assignees and inventors

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  4. Key dates

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  5. First independent claim

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  6. CPC / IPC classifications

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  7. Citations and related patents

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Abstract

Official abstract text for this publication.

A system and method for performing a test procedure on a system under test are provided. An actuation unit operatively coupled to the system under test is configured to perform at least one operation thereon. A visual recognition unit is configured to capture at least one image of the system under test in real-time. A test unit remotely interfaced with the system under test is configured to perform the test procedure. Using the test unit, the test procedure is retrieved from the memory, at least one control signal is output to the actuation unit for causing the at least one operation to be performed in real-time for testing the system under test in accordance with the one or more test instructions, and the at least one image of the system under test is monitored as the at least one operation is performed for validating the test procedure in real-time.

First claim

Opening claim text (preview).

What is claimed is: 1. A system for performing a test procedure on a system under test, the system comprising: an actuation unit operatively coupled to the system under test and configured to perform at least one operation thereon; a visual recognition unit configured to capture at least one image of the system under test in real-time; and a test unit remotely interfaced with the system under test and configured to perform the test procedure thereon, the test unit comprising a non-transitory memory having stored therein the test procedure comprising one or more test instructions for testing the system under test, at least one processing unit, and at least one application stored in the memory and executable by the at least one processing unit for: retrieving the test procedure from the memory, outputting at least one control signal to the actuation unit for causing the at least one operation to be performed in real-time for testing the system under test in accordance with the one or more test instructions, and monitoring the at least one image of the system under test as the at least one operation is performed for validating the test procedure in real-time. 2. The system of claim 1 , wherein the actuation unit comprises a robotic arm. 3. The system of claim 1 , wherein the visual recognition unit comprises at least one image acquisition device with graphic recognition capability. 4. The system of claim 1 , wherein the at least one application is executable by the at least one processing unit for outputting the at least one control signal for causing the at least one operation comprising at least one of simulating a short to ground, disconnecting a connector, injecting a signal, injecting a voltage, injecting a current, simulating a resistance, simulating an impedance, simulating a capacitance, simulating an inductance, measuring a voltage, measuring a current, measuring a resistance, measuring an impedance, measuring a capacitance, measuring an inductance, pressing a switch, turning a knob, and entering data through an input device associated with the system under test to be performed. 5. The system of claim 1 , wherein the system under test is an aircraft system selected from the group consisting of a hydraulics system, an engine system, a fuel system, a navigation system, a landing gear system, a flap control system, an electricity generating system, and a cabin climate control system. 6. The system of claim 1 , wherein the test unit is electrically interfaced with the system under test through at least one cable connecting each electrical connector of the system under test to the test unit. 7. The system of claim 5 , wherein the visual recognition unit is configured to capture the at least one image of at least one standby aircraft instrument. 8. The system of claim 1 , wherein the at least one application is executable by the at least one processing unit for: monitoring the at least one image in real-time and determining at least one test result therefrom; comparing the at least one test result to at least one test criterion defined by the test procedure; responsive to determining that the at least one test result satisfies the at least one test criterion, concluding to a pass of the test procedure; and responsive to determining that the at least one test result does not satisfy the at least one test criterion, concluding to a failure of the test procedure. 9. The system of claim 8 , further comprising a troubleshooting unit connected to the test unit and configured to automatically troubleshoot the system under test responsive to concluding to the failure of the test procedure. 10. A method for performing a test procedure on a system under test, the method comprising: remotely interfacing a test unit with the system under test; and using the test unit, retrieving from memory the test procedure comprising one or more test instructions for testing the system under test, outputting at least one control signal for causing at least one operation to be performed on the system under test in real-time for testing the system under test in accordance with the one or more test instructions, and monitoring at least one image of the system under test for validating the test procedure in real-time, the at least one image captured in real-time as the at least one operation is performed. 11. The method of claim 10 , wherein the at least one control signal is output for causing the at least one operation comprising at least one of simulating a short to ground, disconnecting a connector, injecting a signal, injecting a voltage, injecting a current, simulating a resistance, simulating an impedance, simulating a capacitance, simulating an inductance, measuring a voltage, measuring a current, measuring a resistance, measuring an impedance, measuring a capacitance, measuring an inductance, pressing a switch, turning a knob, and entering data through an input device associated with the system under test to be performed. 12. The method of claim 10 , wherein remotely interfacing the test unit with the system under test comprises electrically interfacing the test unit with the system under test through at least one cable connecting each electrical connector of the system under test to the test unit. 13. The method of claim 10 , further comprising integrating the test unit and at least one avionic test equipment on a workstation electrically interfaced with the system under test. 14. The method of claim 10 , further comprising: monitoring the at least one image in real-time and determining at least one test result therefrom; comparing the at least one test result to at least one test criterion defined by the test procedure; responsive to determining that the at least one test result satisfies the at least one test criterion, concluding to a pass of the test procedure; and responsive to determining that the at least one test result does not satisfy the at least one test criterion, concluding to a failure of the test procedure. 15. The method of claim 14 , further comprising automatically troubleshooting the system under test responsive to concluding to failure of the test procedure. 16. A non-transitory computer readable medium having stored thereon program code executable by a processor for: retrieving from memory a test procedure comprising one or more test instructions for testing a system under test, outputting at least one control signal for causing at least one operation to be performed on the system under test in real-time for testing the system under test in accordance with the one or more test instructions, and monitoring at least one image of the system under test for validating the test procedure in real-time, the at least one image captured in real-time as the at least one operation is performed.

Assignees

Inventors

Classifications

  • B64F5/60Primary

    Testing or inspecting aircraft components or systems · CPC title

  • characterised by the operator's input device (input arrangements for computing systems in general G06F3/00) · CPC title

  • G07C5/008Primary

    communicating information to a remotely located station (transmission systems for measured values G08C) · CPC title

  • Voltage or current aspects, e.g. driver, receiver · CPC title

  • where the device under test is an electronic circuit · CPC title

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Frequently asked questions

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What does patent US11142345B2 cover?
A system and method for performing a test procedure on a system under test are provided. An actuation unit operatively coupled to the system under test is configured to perform at least one operation thereon. A visual recognition unit is configured to capture at least one image of the system under test in real-time. A test unit remotely interfaced with the system under test is configured to per…
Who is the assignee on this patent?
Bell Helicopter Textron Inc, Textron Innovations Inc
What technology area does this patent fall under?
Primary CPC classification B64F5/60. Mapped technology areas include Operations & Transport.
When was this patent published?
Publication date Tue Oct 12 2021 00:00:00 GMT+0000 (Coordinated Universal Time) (B2). Legal status and post-grant events are not shown on this page.
What related patents are in patentsdb?
We list 12 related publications on this page (citations in our corpus or others sharing the same primary CPC).