CN106325259A - Multi-LRU parallel safety testing method - Google Patents

Multi-LRU parallel safety testing method Download PDF

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Publication number
CN106325259A
CN106325259A CN201610681650.6A CN201610681650A CN106325259A CN 106325259 A CN106325259 A CN 106325259A CN 201610681650 A CN201610681650 A CN 201610681650A CN 106325259 A CN106325259 A CN 106325259A
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CN
China
Prior art keywords
lru
test
safety
parts
testing
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Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Pending
Application number
CN201610681650.6A
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Chinese (zh)
Inventor
常华
曹睿婷
刘赛遥
张航
刘宏明
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Xian Flight Automatic Control Research Institute of AVIC
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Xian Flight Automatic Control Research Institute of AVIC
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
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Publication date
Application filed by Xian Flight Automatic Control Research Institute of AVIC filed Critical Xian Flight Automatic Control Research Institute of AVIC
Priority to CN201610681650.6A priority Critical patent/CN106325259A/en
Publication of CN106325259A publication Critical patent/CN106325259A/en
Pending legal-status Critical Current

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Classifications

    • GPHYSICS
    • G05CONTROLLING; REGULATING
    • G05BCONTROL OR REGULATING SYSTEMS IN GENERAL; FUNCTIONAL ELEMENTS OF SUCH SYSTEMS; MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS OR ELEMENTS
    • G05B23/00Testing or monitoring of control systems or parts thereof
    • G05B23/02Electric testing or monitoring

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  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Engineering & Computer Science (AREA)
  • Automation & Control Theory (AREA)
  • Test And Diagnosis Of Digital Computers (AREA)

Abstract

The invention belongs to the civil aviation flight control system safety testing technology, relating to the parallel safety testing method for testing multiple identical-model LRU components on a plane. The LRU is a locale replaceable unit, an important component of a flight control system of a plane; because the safety test directly affects safety of the flight control system and the test result directly affects a dispatching rate of the plane. A sequence test method is adopted for safety test on multiple identical parts on the plane. The invention provides a multi-LRU parallel safety testing method. The multi-LRU parallel safety testing method uses coding, decoding and a bit logic operation method to realize parallel testing of multiple identical components, reduces system resource consumption, improves safety testing efficiency and supports improving the dispatching rate of the plane.

Description

A kind of many LRU parallel safety method of testing
Technical field
The invention belongs to the security test technology of civil aircraft flight control system, relate to multiple same types LRU on aircraft The method of component in parallel test.
Background technology
LRU is Field Replaceable Unit, aboard the important component part of flight control system.At present, civil aircraft parts Security test be boat after BIT test a part, belong to the important component part of flight control system maintenance function module.Due to Security test directly affects the safety of flight control system, and what its test result directly affected aircraft sends rate, therefore, how to carry The efficiency of high security test, is an important research direction of civil aircraft flight control system maintenance function.At present, on aircraft The security test of multiple same parts, the main method using sequential testing, the testing time is long, wastes system resource, is fall One of low aircraft many factors sending rate.
Summary of the invention
The technical problem to be solved is: propose a kind of many LRU parallel safety method of testing, to reduce system Resource consumption, improves the efficiency of security test, sends rate to provide support for improving aircraft.
One many LRU parallel safety method of testing of the present invention, for carrying out parallel peace to multiple identical LRU parts Full property test, the method comprises the following steps:
Step 1, the N road binary data signal of M LRU parts of Real-time Collection, after receiving test initiation command, according to Quantity M of LRU parts, encodes described data signal, generates the integer variable of N number of M figure place, and is stored in variable list In;
Step 2, according to the security test requirement of LRU parts, is utilized respectively a logical operations same road to M LRU Signal condition judges, generates the test result integer variable of N number of M figure place according to judged result;
Step 3, is decoded computing to each test result integer variable, exports the N drive test examination of each LRU parts respectively Result data signal.
The invention has the beneficial effects as follows: propose a kind of many LRU parallel safety method of testing, utilize coding, decoding and position Logical calculation method, it is achieved that the concurrent testing of multiple same parts, reduces system resources consumption, improves the effect of security test Rate, sends rate to provide support for improving aircraft.
Detailed description of the invention
Below the present invention is described in further details.A kind of security test software design approach based on model, profit With coding, decoding and position logical operations, it is achieved the concurrent testing of multiple identical LRU, the step performing security test is as follows:
Step 1, gathers the multichannel data signal of multiple LRU parts, after receiving test initiation command, according to input data letter All data signals are encoded by the quantity of number type, generate multiple integer variables according to signal type, this integer variable Binary coding figure place is identical with LRU quantity, and number is identical with the quantity of input data signal type.All integer variables are deposited Storage is in software variable list.
Step 2, according to the step of this LRU piece safety test request, is utilized respectively a logical operations to multiple LRU's Multiple signals state judges, provides testing procedure according to judged result and is fully completed the multiple integers needed for the output of rear system Variable, the binary coding figure place of this integer variable is identical with LRU number, the outputting data signals needed for quantity and test result The number of type is identical.
Step 3, according to the step of this LRU piece safety test, order performs the universal safety for single LRU parts Property test program, output multi-channel data signal.
Step 4, is decoded computing according to the multiple integer variables in step 2, exports the multichannel of multiple LRU parts respectively Data signal, indicates the different test results of multiple LRU parts.
The operation principle of the present invention is:
Utilize the concordance of multiple identical LRU parts, use coded method the input signal of multiple same parts to be carried out Packing processes, and after reducing data volume, utilizes position logical operations to complete the universal test program of single parts, utilizes position logic simultaneously Computing, according to the different conditions of different parts, is decoded output signal processing, it is achieved multiple same parts concurrent testings, Draw the different test results of multiple parts.
Embodiment 1
19 identical LRU parts of certain civil aircraft flight control system are performed security test.
1, gather 8 kinds of data messages of 19 LRU parts, according to the type of data message, after receiving test initiation command, Its all data messages are encoded, forms the signal variable of 8 19, be stored in software variable list.
2, according to 3 testing procedures defined in maintenance function framework, utilize position logical operations 8 to 19 LRU parts Plant signal condition to judge, provide 3 testing procedures according to judged result and be fully completed 6 19 needed for the output of rear system Signal variable.
3, according to 3 testing procedures defined in maintenance function framework, order performs general security test program, defeated Go out 6 kinds of data messages.
4, it is decoded computing according to 6 19 signal variables in step 2, exports 6 kinds of numbers of 19 LRU parts respectively It is believed that breath, the different test results of 19 LRU parts of instruction.

Claims (1)

1. the parallel safety method of testing of LRU more than, for multiple identical LRU parts are carried out parallel security test, It is characterized in that, the method comprises the following steps:
Step 1, the N road binary data signal of M LRU parts of Real-time Collection, after receiving test initiation command, according to LRU portion Quantity M of part, encodes described data signal, generates the integer variable of N number of M figure place, and is stored in variable list;
Step 2, according to the security test requirement of LRU parts, is utilized respectively a logical operations same road signal to M LRU State judges, generates the test result integer variable of N number of M figure place according to judged result;
Step 3, is decoded computing to each test result integer variable, exports the N drive test test result of each LRU parts respectively Data signal.
CN201610681650.6A 2016-08-17 2016-08-17 Multi-LRU parallel safety testing method Pending CN106325259A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201610681650.6A CN106325259A (en) 2016-08-17 2016-08-17 Multi-LRU parallel safety testing method

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201610681650.6A CN106325259A (en) 2016-08-17 2016-08-17 Multi-LRU parallel safety testing method

Publications (1)

Publication Number Publication Date
CN106325259A true CN106325259A (en) 2017-01-11

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CN (1) CN106325259A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110174584A (en) * 2019-06-03 2019-08-27 西安飞机工业(集团)有限责任公司 A kind of big airplane complete machine cable automatic detection distributed arrangement method
CN115483987A (en) * 2022-08-23 2022-12-16 中国电子科技集团公司第十研究所 CNI system function distributed detection equipment and method
CN116203393A (en) * 2023-02-27 2023-06-02 杭州朗迅科技股份有限公司 Integrated circuit testing method and system

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CN103543980A (en) * 2013-11-07 2014-01-29 吴胜远 Digital data processing method and device
CN103577155A (en) * 2012-07-26 2014-02-12 中国航空工业集团公司第六三一研究所 ARINC 659 protocol based instruction decoding circuit implementation method
CN103625647A (en) * 2013-11-29 2014-03-12 中国航空无线电电子研究所 Onboard novel comprehensive data loading and transmitting device
CN103744416A (en) * 2013-12-23 2014-04-23 中国人民解放军63908部队 Detection device for unmanned aerial vehicle-mounted electronic system
CN105446847A (en) * 2014-09-26 2016-03-30 中国航空工业第六一八研究所 Automatic testing system and method for ARINC659 buses

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103577155A (en) * 2012-07-26 2014-02-12 中国航空工业集团公司第六三一研究所 ARINC 659 protocol based instruction decoding circuit implementation method
CN103543980A (en) * 2013-11-07 2014-01-29 吴胜远 Digital data processing method and device
CN103625647A (en) * 2013-11-29 2014-03-12 中国航空无线电电子研究所 Onboard novel comprehensive data loading and transmitting device
CN103744416A (en) * 2013-12-23 2014-04-23 中国人民解放军63908部队 Detection device for unmanned aerial vehicle-mounted electronic system
CN105446847A (en) * 2014-09-26 2016-03-30 中国航空工业第六一八研究所 Automatic testing system and method for ARINC659 buses

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* Cited by examiner, † Cited by third party
Title
徐文辉: "ARINC659总线简介", 《航空电子技术》 *

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110174584A (en) * 2019-06-03 2019-08-27 西安飞机工业(集团)有限责任公司 A kind of big airplane complete machine cable automatic detection distributed arrangement method
CN115483987A (en) * 2022-08-23 2022-12-16 中国电子科技集团公司第十研究所 CNI system function distributed detection equipment and method
CN116203393A (en) * 2023-02-27 2023-06-02 杭州朗迅科技股份有限公司 Integrated circuit testing method and system
CN116203393B (en) * 2023-02-27 2023-09-26 杭州朗迅科技股份有限公司 Integrated circuit testing method and system

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