CN105866578A - Airplane standard hanger management system detection method - Google Patents
Airplane standard hanger management system detection method Download PDFInfo
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- CN105866578A CN105866578A CN201610207014.XA CN201610207014A CN105866578A CN 105866578 A CN105866578 A CN 105866578A CN 201610207014 A CN201610207014 A CN 201610207014A CN 105866578 A CN105866578 A CN 105866578A
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- management system
- test
- bus
- storage management
- aircraft
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- G—PHYSICS
- G01—MEASURING; TESTING
- G01R—MEASURING ELECTRIC VARIABLES; MEASURING MAGNETIC VARIABLES
- G01R31/00—Arrangements for testing electric properties; Arrangements for locating electric faults; Arrangements for electrical testing characterised by what is being tested not provided for elsewhere
Abstract
Disclosed is an airplane standard hanger management system detection method. There is a detection device. The detection device comprises an industrial control computer and a display, the industrial control computer is internally provided with a GJB289A bus communication module, a 28.5V DC switching quantity input output module and a 115V AC 400Hz acquisition module, detection software runs on a mainboard of the industrial control computer, the GJB289A bus communication module can be taken as an RT end for communication with a standard hanger management system, and the industrial control computer is in single connection with the standard hanger management system through a GJB1188A bus; a group of special-purpose test signals are designed according to test content of the airplane standard hanger management system; the test signals are sent to the airplane standard hanger management system through the industrial control computer; and the airplane standard hanger management system feeds corresponding response signals to the industrial control computer through the GJB1188A bus.
Description
Technical field
The present invention relates to aircraft manufacturing detection technique, the detection side of a kind of Aircraft Standard Storage Management System
Method.
Background technology
Aircraft Standard hanger refer to be predefined in interior of aircraft or outside hang and deliver and install on delivery device appoint
Whether what device, separate with aircraft during flying regardless of this device, in general can directly support that aircraft is concrete
Completing of task.Storage Management System is one of aviation electronics subsystem, for controlling and monitor install aboard outstanding
Hang the duty of thing, and the communication between management Airborne Stores and other subsystem of aircraft is provided.If not to outstanding
Hang property management reason system and carry out comprehensive, careful detection, completing of aircraft flight task, serious situation must be likely to affect
It is also possible to directly result in the failure of task.
Test currently for Aircraft Standard Storage Management System is all by the testing process of a whole set of standard, i.e.
The most according to condition serial carries out flow process inspection.For the testing process step that some of them are important, it it is the most all basis
In Aircraft Standard hanger real work, the working time of process step determines that it controls the test response of equipment corresponding steps
Time, such as guided missile send out the step for that the guided missile inertial navigation in flow control journey is directed at, and machine is actually needed 8 minutes, current survey
Examination is also required to wait 8 minutes and could enter next step, cause whole testing process to generally require cost three, 40 minutes.
Along with the development of missilery, the newer versions of these missiles that far firing range, function are many continues to bring out, it means that flow control journey and the survey of guided missile
What try can become suddenly becomes increasingly complex, and the time of consuming can be more and more longer, and once certain step breaks down in flow process, whole
Whether individual testing process can not continue executing with, have problems and also cannot be verified in follow-up process step.
Summary of the invention
For problems of the prior art, it is an object of the invention to provide a kind of Aircraft Standard store management system
System detection method, this detection method, it is not only able to shorten proof cycle, and a flow process inspection just can determine that all existence are asked
The interface of topic, significantly facilitates detection.
A kind of Aircraft Standard Storage Management System detection method, it is known that the test content of Aircraft Standard hanger, it is special
Levy and be, 1) there is a detection equipment, this detection equipment contains an industrial computer and a display, installs one in industrial computer
GJB289A bus communication module, 28.5V dc switch amount input/output module, a 115V exchange 400Hz gather mould
Block, inspection software operates on industrial control computer mainboard, and wherein GJB289A bus communication module can be as RT end, with standard suspension
Property management reason system communicates, and this industrial computer is connected by GJB1188A bus with standard suspension property management reason system signal；2)
The test signal that test content design according to Aircraft Standard Storage Management System one group is special；3) this test signal is passed through
Above-mentioned industrial computer is sent to Aircraft Standard Storage Management System；4) Aircraft Standard Storage Management System will pass through
GJB1188A bus feedback is to one corresponding answer signal of industrial computer.If standard suspension property management reason system is normal, will pass through
GJB1188A bus feedback is to one corresponding answer signal of industrial computer；If standard suspension property management reason system is abnormal, industry control
Machine just can not receive the answer signal of correspondence or receives a wrong answer signal.
The beneficial effects of the present invention is: 1) the application present invention is when detecting Aircraft Standard Storage Management System,
The test signal of each interface contains this interface and be there is a need to the content of test in testing process, it is possible to detect this interface
All hardware problem that may be present, it is possible to effectively promote testing efficiency, shorten test period；2) can fundamentally solve to fly
Machine standard suspension property management reason system testing process must carry out a difficult problem for software development according to its different model, significantly saves development
Funds.3) as a example by the Storage Management System test equipment of certain emphasis model aircraft, single system examination is carried out according to existing method
Test and need hanging point simulator management a set of, plug-in subsystem special test equipment a set of, more than 500 ten thousand yuan altogether, and use this Shen
Please method, the test apparatus value of needs is estimated at about 1,000,000 yuan, can be with effectively save more than 400 ten thousand yuan；Use original method
Complete test and need 40 minutes, and use novel test method to complete test and have only to about two minutes；4) survey of the present invention is used
It is simple that method for testing has exploitation, feature easy to use, reliable, it is possible to meet the Aircraft Standard hanger of different model, kind
The test request of management system.Meanwhile, also can promote the use of in other the measuring technology of computer equipment.
Below in conjunction with embodiment accompanying drawing, the application is described in further detail:
Accompanying drawing explanation
Fig. 1 is the theory diagram of the Aircraft Standard Storage Management System detection method of the application.
Detailed description of the invention
Embodiment is managed as a example by the detection of system by the standard suspension property management of certain emphasis model aircraft domestic, further describes this
The summary of the invention of application.
The standard suspension property management reason system of emphasis model aircraft is operated in two GJB289A buses, a wherein bus
Upper standard Storage Management System is RT equipment, receives input signal；It is BC equipment in another bus, is GJB1188A bus
In GJB289A bus.
First having a detection equipment, this detection equipment contains an industrial computer, installs a GJB289A total in industrial computer
Line communication module, 28.5V dc switch amount input/output module, a 115V exchange 400Hz acquisition module, inspection software
Operating on industrial control computer mainboard, wherein GJB289A bus communication module can be entered with standard suspension property management reason system as RT end
Row communication, this industrial computer is connected by GJB1188A bus with standard suspension property management reason system signal；Above-mentioned 28.5V direct current is opened
Pass amount input/output module has eight road 28.5V ground effectively inputs, eight road 28.5V effectively input, eight road 28.5V ground effectively outputs
Ability, described 115V exchange 400Hz acquisition module has the ability gathering three road 115V AC signals inputs.
According to new detection method program detection software, all signals GJB1188A bus specified are by different tests
Order is defined numbering, sets up test command storehouse by this standard, realizes calling and any group of arbitrary test command with software
That closes test command calls (this function uses programming software to realize very easily).
All test commands of regulation in GJB1188A bus are defined numbering, are specifically defined numbering and see attached list one.
Subordinate list one
By in inspection software above-mentioned for the definition numbering write of this test command, according in standard suspension property management reason system
Test content, selects the definition numbering of its corresponding test command, forms one group of special test signal.
The detection content of standard suspension property management reason system of this aircraft, the corresponding test command of GJB1188A bus, phase
The corresponding relation closed between the definition numbering of test command and the test signal being made up of definition numbering sees attached list two.
Subordinate list two
The main working process of plug-in test is as follows:
First determine that Aircraft Standard Storage Management System needs the test content that carries out: include address bit A0, A1,
A2, A3, A4, main interface interlocking signal, satellite interface interlocking signal, throw in and allow signal, auxiliary 115V exchanges A phase, B phase, C
Phase, main 115V exchanges A phase, B phase, C phase, main 28.5V DC source 1, main 28.5V DC source 2 and auxiliary 28.5V direct current.
2., according to subordinate list two, this Aircraft Standard Storage Management System needs the GJB1188A that the test content that carries out is corresponding
The test command of bus includes: connects, cut off auxiliary 115V exchange A phase, B phase, C phase, connects, cuts off 28.5V DC source 1,
Arrange, remove address bit A0, A1, A2, A3, A4, arrange, cancel main interface interlocking signal, arrange, cancel satellite interface interlocking letter
Number, connect, cut off 28.5V DC source 2, arrange, cancel input permission signal, connect, cut off 115V exchange A phase, B phase, C
Phase, connects, cuts off auxiliary 28.5V direct current, and the definition numbering of these test commands is: 37,38,39,40,41,42,23,24,
21,22,19,20,17,18,15,16,13,14,11,12,45,46,25,26,9,10,27,28,31,32,29,30,35,36,
The definition of these test commands is numbered permutation and combination sequentially becomes one group to be exclusively used in this kind of plug-in test signal: 9,
10、11、12、13、14、15、16、17、18、19、20、21、22、23、24、25、26、27、28、29、30、31、32、35、36、
37、38、39、40、41、42、45、46。
3. the industrial computer of detection equipment is attached with this Aircraft Standard Storage Management System.(this detection equipment is every
Secondary can detect multichannel 1188A interface) simultaneously
4. start Aircraft Standard Storage Management System, it is set and is operated in checking mode.
5. run inspection software, activate above-mentioned one group of test being exclusively used in this kind of Aircraft Standard Storage Management System and believe
Number, to plug-in transmission test command 9,10,11,12,13,14,15,16,17,18,19,20,21,22,23,24,25,26,27,
28、29、30、31、32、35、36、37、38、39、40、41、42、45、46.Standard suspension property management reason system must be responsive to these lives
Order, feeds back corresponding answer signal in GJB1188A bus, if can not receive corresponding answering after sending some test command
Answer signal or receive the answer signal of mistake, then in judging the detection that tested Aircraft Standard Storage Management System is corresponding
Hold and there is fault.
6. all detection work completes.
Claims (4)
1. an Aircraft Standard Storage Management System detection method, it is known that the test content of Aircraft Standard hanger, its feature
It is, 1) there is a detection equipment, this detection equipment contains an industrial computer and display, installs one in industrial computer
GJB289A bus communication module, 28.5V dc switch amount input/output module, a 115V exchange 400Hz gather mould
Block, inspection software operates on industrial control computer mainboard, and wherein GJB289A bus communication module can be as RT end, with standard suspension
Property management reason system communicates, and this industrial computer is connected by GJB1188A bus with standard suspension property management reason system signal；2)
The test signal that test content design according to Aircraft Standard Storage Management System one group is special；3) this test signal is passed through
Above-mentioned industrial computer is sent to Aircraft Standard Storage Management System；4) Aircraft Standard Storage Management System will pass through
GJB1188A bus feedback is to one corresponding answer signal of industrial computer.
2. Aircraft Standard Storage Management System detection method as claimed in claim 1, it is characterised in that by GJB1188A
In bus, all test commands of regulation are defined numbering, by inspection software above-mentioned for the definition numbering write of this test command
In, according to the test content in Aircraft Standard Storage Management System, select the definition of GJB1188A bus correspondence test command
Numbering, forms one group of special test signal.
3. Aircraft Standard Storage Management System detection method as claimed in claim 1, it is characterised in that described 28.5V is straight
Flow with the having eight road 28.5V effectively input of On-off signal output module, eight road 28.5V effectively input, eight road 28.5V ground are effective
The ability of output, described 115V exchange 400Hz acquisition module has the ability gathering three road 115V AC signal inputs.
4. Aircraft Standard Storage Management System detection method as claimed in claim 2, it is characterised in that by GJB1188A
In bus, all test commands of regulation are defined numbering, and concrete numbering see table:
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
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| CN201610207014.XA CN105866578A (en) | 2016-04-01 | 2016-04-01 | Airplane standard hanger management system detection method |
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| CN201610207014.XA CN105866578A (en) | 2016-04-01 | 2016-04-01 | Airplane standard hanger management system detection method |
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Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108563596A (en) * | 2018-04-18 | 2018-09-21 | 天津津航计算技术研究所 | A kind of acquisition of Portable aircraft 1188A interface signals and detection device |
| CN110727625A (en) * | 2019-09-23 | 2020-01-24 | 江西洪都航空工业集团有限责任公司 | Data loading equipment and data interaction method after loading of missile-borne integrated guide machine |
| CN111637802A (en) * | 2020-05-29 | 2020-09-08 | 西安现代控制技术研究所 | Missile simulator with small pendant electrical interface |
| CN112416836A (en) * | 2020-10-15 | 2021-02-26 | 中国航空工业集团公司洛阳电光设备研究所 | Method for controlling RT address allocation of hanging point nodes in distributed hanging object management system |
| CN113721090A (en) * | 2021-08-07 | 2021-11-30 | 中国航空工业集团公司沈阳飞机设计研究所 | Universal weapon system input and output line checking method |
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Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108563596A (en) * | 2018-04-18 | 2018-09-21 | 天津津航计算技术研究所 | A kind of acquisition of Portable aircraft 1188A interface signals and detection device |
| CN108563596B (en) * | 2018-04-18 | 2021-06-08 | 天津津航计算技术研究所 | Portable airplane 1188A interface signal acquisition and detection device |
| CN110727625A (en) * | 2019-09-23 | 2020-01-24 | 江西洪都航空工业集团有限责任公司 | Data loading equipment and data interaction method after loading of missile-borne integrated guide machine |
| CN111637802A (en) * | 2020-05-29 | 2020-09-08 | 西安现代控制技术研究所 | Missile simulator with small pendant electrical interface |
| CN112416836A (en) * | 2020-10-15 | 2021-02-26 | 中国航空工业集团公司洛阳电光设备研究所 | Method for controlling RT address allocation of hanging point nodes in distributed hanging object management system |
| CN112416836B (en) * | 2020-10-15 | 2022-11-01 | 中国航空工业集团公司洛阳电光设备研究所 | Method for controlling RT address allocation of hanging point nodes in distributed hanging object management system |
| CN113721090A (en) * | 2021-08-07 | 2021-11-30 | 中国航空工业集团公司沈阳飞机设计研究所 | Universal weapon system input and output line checking method |
| CN113721090B (en) * | 2021-08-07 | 2023-10-20 | 中国航空工业集团公司沈阳飞机设计研究所 | Input/output circuit inspection method for universal weapon system |
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Application publication date: 20160817 |
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