CN109270918A - A kind of aircraft avionics floor synthetic debugging system based on performance test - Google Patents
A kind of aircraft avionics floor synthetic debugging system based on performance test Download PDFInfo
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- CN109270918A CN109270918A CN201810940994.3A CN201810940994A CN109270918A CN 109270918 A CN109270918 A CN 109270918A CN 201810940994 A CN201810940994 A CN 201810940994A CN 109270918 A CN109270918 A CN 109270918A
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- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05B—CONTROL OR REGULATING SYSTEMS IN GENERAL; FUNCTIONAL ELEMENTS OF SUCH SYSTEMS; MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS OR ELEMENTS
- G05B23/00—Testing or monitoring of control systems or parts thereof
- G05B23/02—Electric testing or monitoring
- G05B23/0205—Electric testing or monitoring by means of a monitoring system capable of detecting and responding to faults
- G05B23/0208—Electric testing or monitoring by means of a monitoring system capable of detecting and responding to faults characterized by the configuration of the monitoring system
- G05B23/0213—Modular or universal configuration of the monitoring system, e.g. monitoring system having modules that may be combined to build monitoring program; monitoring system that can be applied to legacy systems; adaptable monitoring system; using different communication protocols
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- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05B—CONTROL OR REGULATING SYSTEMS IN GENERAL; FUNCTIONAL ELEMENTS OF SUCH SYSTEMS; MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS OR ELEMENTS
- G05B2219/00—Program-control systems
- G05B2219/20—Pc systems
- G05B2219/24—Pc safety
- G05B2219/24065—Real time diagnostics
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Abstract
The aircraft avionics floor synthetic debugging system based on performance test that the present invention relates to a kind of, including basic integrated-type test macro, extend simulation type test macro and properties of product type test macro, the debugging enironment is connected with measurand, the test item of the measurand includes system-wide functions component, subsystem functional unit and component-level performance component, the allomeric function that the basic integrated-type test macro is connected to the entire avionics system of system-wide functions module testing by testing cable, the extension emulation test system is connected to the subsystem function of the subsystem functional unit test avionics system, the properties of product type test macro is connected to the component-level performance component test component performance by testing cable.The present invention realizes the performance test and accident analysis of avionics system ground combined test test, crucial subsystem or equipment, improves the comprehensive utilization and performance test ability of environment.
Description
Technical field
The present invention relates to aviation airborne equipment the field of test technology, specifically a kind of Aircraft based on performance test
Electric floor synthetic debugging system.
Background technique
Type aircraft airborne system is usually made of structure, avionics, winged control and weapon system.Avionics system is as aircraft
" brain " and " nerve center ", it is main to complete function relevant to aerial mission, it is occupied an important position in airborne system.Ground
Comprehensive debugging be airborne avionics system entirely test with the important link of debugging process, with New Equipments designing technique send out
Exhibition, floor synthetic debugging technique also change therewith, how preferably to make full use of the software and hardware resources of floor synthetic debugging enironment,
While the integrative test of the systematization integration of development and debugging efforts, the performance test to subsystem or equipment is unfolded,
Comprehensive verification and confirmation are carried out to airborne subsystem performance, system overall system performance and function.Air force's aeronautical maintenance system is just
Supportability construction is repaired carrying out new machine, lacks the avionics system comprehensive debugging ring based on subsystem or equipment performance test
It realizes while system before realizing avionics system installation is reviewed with floor synthetic debugging capability to crucial important subsystem in border
Or performance test and the debugging capability of equipment, while guaranteeing the repairing quality of avionics system, improve the utilization rate and property of environment
Valence ratio.
Chinese invention patent CN201320841988.5 (publication date is on July 9th, 2014) discloses avionics system ground
Joint-trial system, the system are built by master control system, emulator, simulator and driver, are filled to ready system products
Checking feature before machine, the disadvantage is that the system is the ground joint-trial of avionics system, without reference to the performance to subsystem or equipment
Test.
Chinese invention patent CN201410007750.1 (publication date is on April 30th, 2014) discloses a kind of avionics system
Auto-Test System, the system is by by store Combinations simulator, each target simulator, admittance driver, carrier aircraft flight simulation
The test accessories such as device carry out the connection of Real-time Network, under the control of test master control platform, can be referred to as by one kind and be retrieved
The method that formula judges automatically, to complete automatic test, by the invention, effectively improves to complete the judgement of data correctness
The efficiency of avionics system test, and largely improve test automatically it is comprehensive, the disadvantage is that the system is only navigated
The automatic test of electric system, without reference to the performance test to subsystem or equipment.
Chinese invention patent CN201410072725.1 (publication date is on June 4th, 2014) discloses a kind of for flying control
The ground test device and control method of system, The present invention gives test device and its three kinds of test methods, can be more
On ground test unmanned vehicle flight control system performance, flight control system design experimental stage can effectively checking system join
Number, the reasonability and validity of access control circuit, navigation algorithm etc..The disadvantage is that the system is unmanned vehicle flight control system
Ground test device and control method, without reference to the performance test to subsystem or equipment.
It is real that the 54-56 pages of the phase of " aeronautical maintenance and the engineering " the 4th published in April, 2015 discloses a kind of comprehensive avionics fire control
When network dynamic joint-trial system, which carries out the equipment such as fight environment simulation equipment, test equipment, avionics system simulator mutual
Even, the control of system dynamic and performance evaluation are realized, it being capable of fast failure positioning and investigation.Disadvantage only realizes and builds certain type machine
Synthesis avionics fire control ground dynamic joint-trial platform, without reference to the performance test to subsystem or equipment.
O. 11th page 209,212 of " dual-use technology and the product " published in November, 2015 discloses a kind of comprehensive boat
The research of electrical fire control system detection method, this researchs and proposes the use of bus test equipment, reduces survey equipment, simplifies test
Environment substantially reduces so that the test environment of comprehensive avionics fire control system really develops to general direction and surveys equipment
Lead time improves the reliability of test, is a kind of development trend of system detection method.Disadvantage only proposes a kind of total
The comprehensive avionics fire control system test method of the use of line testing device, without reference to the performance test to subsystem or equipment.
It is winged that the 903-907 pages of the phase of " the war industry's automation " the 6th published in June, 2017 discloses certain a kind of type unmanned helicopter
It is real to provide half using certain type " single rotor fan is coaxial " formula unmanned helicopter as object for row control system HWIL simulation, the research
Object emulation platform real-time working process gains knowledge according to power and carries out mathematical modeling, discusses the contents such as design scheme, by outstanding
Stop state simulation to platform feature demonstrate platform can approximate simulation flight control system running environment, can effectively verify winged control
The logic function and quality of system.Disadvantage only proposes a kind of unmanned helicopter flight control system HWIL simulation research,
Without reference to the performance test to subsystem or equipment.
Therefore, for the test of airborne system and ground joint-trial technical research, mainly different model avionics system is surveyed
Test system research, joint-trial research and technique study.But it is based on the avionics system ground tune of subsystem or equipment performance test
Test system or Environmental Studies are less.It is necessary to develop the avionics system floor synthetic debugging enironment for properties of product test.
Summary of the invention
Technical problem to be solved by the present invention lies in propose a kind of aircraft avionics floor synthetic based on performance test
Debugging system is realized the performance test and accident analysis of avionics system ground combined test test, crucial subsystem or equipment, is used
In test and verification avionics system, avionics system subsystem or maintenance of equipment after system function inspection and performance checking, to reach
To the repairing quality for preferably ensureing airborne system.
The technical problems to be solved by the invention are realized using following technical scheme:
A kind of aircraft avionics floor synthetic debugging system based on performance test, including basic integrated-type test macro, expansion
Exhibition simulation type test macro and properties of product type test macro, the debugging enironment are connected with measurand, the measurand
Test item include system-wide functions component, subsystem functional unit and component-level performance component, the basic integrated-type is surveyed
The allomeric function that test system is connected to the entire avionics system of system-wide functions module testing by testing cable, the extension
Emulation test system is connected to the subsystem function of the subsystem functional unit test avionics system, and the properties of product type is surveyed
Test system is connected to the component-level performance component test component performance by testing cable.
The basic integrated-type test macro includes centralized management equipment, and the centralized management equipment is connected with integration test
Equipment, flight simulation module, driver and simulator, general and ancillary equipment, real-time network, basic integrated-type test script collection
It is middle to manage equipment corresponding with control；
The integral test system is by the basic integrated-type test script test item, it can be achieved that various to avionics system
Bus data, non-bus signal are tested；
The flight simulation module realizes the state of flight of simulation the machine and multiple target aircrafts, exports flight parameter number
According to providing dynamic exciting data for the driver and simulator；
The driver and simulator provide avionics system external dynamic under the data-driven of the flight simulation module
The simulation and excitation of signal, signal needed for guaranteeing avionics system various kinds of sensors or terminal proper testing, the signal include
RS-422, HB6096 signal；Type, control logic characteristic, function and the time characteristic signals of weapon；The feature of radar target is believed
Number；The navigation signals such as speech, data communication and orientation, distance, height；The various voices and light signal alerted on machine；
The general and ancillary equipment controllable power power supply and liquid cooling pressure supply support tested airborne products and described basic
The electrical crosslinking of integrated-type test macro, provides product and equipment working environment resource, the resource include power supply power supply distribution,
Cold air and liquid cooling, analog capsule cabin, joint-trial rack, test cable, attenuator and absorbing load Support Resource；
The real-time network is used cooperatively by Reflective memory network and gigabit Ethernet, is needing real-time transmission data
In device resource, realizes to include emulation data, test data, the network real-time Transmission of control command information, form the extension
Simulation type test macro and properties of product type test macro manage network to the control of basic integrated-type test macro related resource
Channel；
The basic integrated-type test script is used to edit, save, execute the test code of the system-wide functions component
Set.
The extension emulation test system includes task management machine testpieces, avionics system emulator, extension simulation type survey
Training sheet, mounting rack and exemplar；
Core calculations platform of the task management machine testpieces as avionics system has data, FC network exchange, figure
The comprehensive treatment capability and system storage capacity of shape/image and video, when lacking airborne task management machine equipment, it is ensured that institute
The debugging enironment for stating extension simulation type test macro can operate normally, and be that the subsystem functional unit of the measurand is tested
Task provides management control and supports；
The avionics system emulator according to the difference of test object, complete in addition to task management machine other avionics systems or
The functional simulation of equipment；Emulation data include inertial navigation, communication and navigation identification, atmosphere data, weapon management, fly control and electromechanics
Control, electronic countermeasure, photoelectricity/radar, data management, the bus interface work that can be realized corresponding airborne products and subsystem are patrolled
Collect simulation；
The extension simulation type test script is used to edit, save, execute the test code of the subsystem functional unit
Set；
The mounting rack and exemplar include test product mounting rack and control and display exemplar, for substituting airborne equipment
Participate in the spare part of system integration test.
The properties of product type test macro includes task management machine examination measurement equipment, product special inspecting equipment, product
It can type test script；
The task management machine examination measurement equipment is matched when equipment of participating in the experiment is detached from the joint-trial environment more detailed interface testing of progress
The commissioning device being tested for the property to task management machine is set, task management machine in the component-level performance component may be implemented
Optical signal test, video switching and superposition test, network interface communication test, 1553B communication test, serial port data interactive are logical
Letter, Time Service functional test and DC power supply ripple, RS422 signal level baud rate and electrical characteristics test；
The product special inspecting equipment is special for realizing providing each product in the component-level performance component
Excitation or analog signal；
The properties of product type test script is used to edit, save, execute the test code of the component-level performance component
Set.
The beneficial effects of the present invention are:
(1) a kind of aircraft avionics floor synthetic debugging system based on performance test is provided, realizes avionics system ground connection
The performance test and accident analysis for adjusting joint-trial test, crucial subsystem or equipment, are used for test and verification avionics system, avionics system
System function inspection and performance checking after the subsystem or maintenance of equipment of system, to reach the repairing matter for preferably ensureing airborne system
Amount, promotes total system, subsystem functional test, component-level performance test and the accident analysis ability of airborne system；
(2) properties of product type test macro is used, realizes the performance test to the subsystem or equipment of avionics system, it is comprehensive
Using basic integrated-type test macro and extension simulation type test macro, the comprehensive utilization and performance test ability of environment are promoted；
(3) real-time network is used, realizes extension simulation type test macro and properties of product type test macro to substantially integrated
The calling of type test macro related resource controls, the network real-time Transmission of the information such as emulation data, test data, control command,
Improve test bridging property, the response real-time of environmental level；
(4) test script is used, realizes in test item editor, save, system-wide functions, subsystem function can be executed respectively
The system software module and structuring of environment can be improved with component-level performance test.
Detailed description of the invention
Present invention will be further explained below with reference to the attached drawings and examples.
Fig. 1 is system construction drawing of the invention.
Specific embodiment
In order to be easy to understand the technical means, the creative features, the aims and the efficiencies achieved by the present invention, below it is right
The present invention is further described.
System construction drawing as shown in Figure 1:
A kind of aircraft avionics floor synthetic debugging system based on performance test, including basic integrated-type test macro 2, expansion
Open up simulation type test macro 3 and properties of product type test macro 4；
The basic integrated-type test macro 2 includes centralized management equipment 21, integral test system 22, flight simulation module
23, driver and simulator 24, general and ancillary equipment 25, real-time network 26, basic integrated-type test script 27 etc.；
The centralized management equipment 21 connects as the comprehensive centralized management equipment of basic integrated-type test macro 2, control operation
Jaws equipment, it can be achieved that pilot project arrangement, test primary condition setting, Process flowchart, process control, test procedure and check in
Hold the functions such as prompt；The display picture of display can be acquired in real time, and is captured, stored video pictures and display management；It being capable of hand
It moves or obtains test data automatically, automatically generate inspection result；The man-machine boundary of good system testing can be provided for inspection personnel
Face；It can be crosslinked, be realized with extension simulation type test macro 3 and properties of product type test macro 4 by real-time network 27
In the test of non-system-wide functions, the management of extension simulation type test macro 3 and properties of product type test macro 4 is controlled, it is complete
The test of the subsystem functional unit 12 and component-level performance component 13 of pairs of measurand 1；
Integration test function list of the integral test system 22 as the basic 2 various signals in inside of integrated-type test macro
Member, under the control of centralized management equipment 21, by basic 27 test item of integrated-type test script, it can be achieved that each to avionics system
Kind bus data, non-bus signal are tested；
The flight simulation module 23 is started by centralized management equipment 21 and is controlled, it can be achieved that simulating the machine and multiple targets
The state of flight of aircraft, export flight parameter data, for basic integrated-type test macro 2 driver provided with simulator 24 it is dynamic
State excited data；
The driver is started and is controlled by centralized management equipment 21 with simulator 24, in the data of flight simulation module 23
Under driving, completes to provide the simulation and excitation of avionics system external dynamic signal, guarantee avionics system various kinds of sensors or terminal
Signal needed for proper testing；Specifically have: RS-422, HB6096 signal are provided；There is provided the type of weapon, control logic characteristic,
The signals such as function and time response；The characteristic signal of radar target is provided；Communications and orientation, distance, the height such as speech, data are provided
The navigation signals such as degree；Various voices and light signal for alerting on machine are provided；
Described general and ancillary equipment 25 is in the case where centralized management equipment 21 starts and controls, controllable power power supply and liquid cooling
Pressure supply is used to support electrical crosslinking and product and the equipment working environment of tested airborne products and basic integrated-type test macro 2
Condition guarantee；Mainly there are power supply power supply distribution, cold air and liquid cooling, analog capsule cabin, joint-trial rack, test cable, attenuator and suction
Receive the Support Resources such as load；
Real-time network of the real-time network 26 as basic integrated-type test macro 2, passes through Reflective memory network and gigabit
Ethernet is used cooperatively, and completes network real-time Transmission, while being responsible for the basic integrated-type test macro 2 of connection, extension emulation
The device resource of real-time transmission data is needed in type test macro 3 and properties of product type test macro 4, is realized emulation data, is surveyed
The network real-time Transmission of the information such as data, control command is tried, completes to form extension simulation type test macro 3 and properties of product type is surveyed
Control managing network road of the test system 4 to basic 2 related resource of integrated-type test macro；
The basic integrated-type test script 27 is complete for editing, saving, execute under the control of centralized management equipment 21
System function component 11 tests code collection.
The extension simulation type test macro 3 includes task management machine testpieces 31, avionics system emulator 32, extends and imitate
True type test script 33, mounting rack and exemplar 34；
Core calculations platform of the task management machine testpieces 31 as avionics system, have data, FC network exchange,
The comprehensive treatment capability and system storage capacity of Graphics/Image and video, on the basis of basic integrated-type test macro 2,
After being equipped with task management machine testpieces 31, when lacking airborne task management machine equipment, it is ensured that extension simulation type test macro 3
Debugging enironment can operate normally, and provide management control for 1 subsystem functional unit of measurand, 12 test assignment and support；
Centralized management equipment 21 starting and control of the avionics system emulator 32 in basic integrated-type test macro 2
Under, according to the difference of test object, complete other avionics systems or the functional simulation of equipment in addition to task management machine；Main emulation
Data have: inertial navigation, communication and navigation identification, atmosphere data, weapon management, fly control and Electromechanical Control, electronic countermeasure, photoelectricity/
Radar, data management etc. can be realized the bus interface work-based logic simulation of corresponding airborne products and subsystem.When joint-trial environment
In the avionics product that is tested it is uneven full-time, can use avionics system emulator instead of corresponding product, cooperation is completed test and expanded
Open up the test item in simulation type test script 33；
Centralized management equipment 21 starting and control of the extension simulation type test script 33 in basic integrated-type test macro 2
Under system, code collection is tested for editing, saving, executing subsystem functional unit 12；
The mounting rack and the main mounting rack and control and display exemplar including test product of exemplar 34, for substituting machine
Carry the spare part that equipment participates in system integration test；
The properties of product type test macro 4 includes task management machine examination measurement equipment 41, product special inspecting equipment 42, produces
Moral character energy type test script 43；
The task management machine examination measurement equipment 41 participate in the experiment equipment be detached from joint-trial environment carry out more detailed interface testing when,
The commissioning device being tested for the property to task management machine is configured, may be implemented in 1 component-level performance component 13 of test product
Optical signal test, video switching and the superposition test, network interface communication test, 1553B communication test, serial ports of task management machine
Data interaction communication, Time Service functional test and DC power supply ripple, RS422 signal level baud rate and electrical characteristic are surveyed
Examination；
The product special inspecting equipment 42 is tested after being required by the performance test of analysis product in basic integrated-type
When the resource of system 2 and extension simulation type test macro 3 is unable to satisfy, the dedicated product detection device of configuration is mainly used for
Realization provides special excitation or analog signal to each product in 1 component-level performance component 13 of test product；
Centralized management equipment 21 starting and control of the properties of product type test script 43 in basic integrated-type test macro 2
Under system, for editing, saving, execution unit grade performance component 13 test code collection.
The basic principles, main features and advantages of the present invention have been shown and described above.The technology of the industry
Personnel are it should be appreciated that the present invention is not limited to the above embodiments, and what is described in the above embodiment and the description is only the present invention
Principle, without departing from the spirit and scope of the present invention, various changes and improvements may be made to the invention, these variation and
Improvement all fall within the protetion scope of the claimed invention.The claimed scope of the invention is by appended claims and its equivalent
Object defines.
Claims (4)
1. a kind of aircraft avionics floor synthetic debugging system based on performance test, it is characterised in that: surveyed including basic integrated-type
Test system (2), extension simulation type test macro (3) and properties of product type test macro (4), the debugging enironment are connected with tested
Object (1), the test item of the measurand (1) include system-wide functions component (11), subsystem functional unit (12) and
Component-level performance component (13), the basic integrated-type test macro (2) are connected to the system-wide functions by testing cable
Component (11) tests the allomeric function of entire avionics system, and the extension emulation test system (3) is connected to the subsystem function
Energy component (12) tests the subsystem function of avionics system, and the properties of product type test macro (4) passes through test cable connection
In component-level performance component (13) the test component performance.
2. a kind of aircraft avionics floor synthetic debugging system based on performance test according to claim 1, feature exist
In: the basic integrated-type test macro (2) includes centralized management equipment (21), and the centralized management equipment (21) is connected with comprehensive
Close test equipment (22), flight simulation module (23), driver and simulator (24), general and ancillary equipment (25), Real-time Network
Network (26), basic integrated-type test script (27) manage equipment corresponding with control concentratedly；
The integral test system (22) is by basic integrated-type test script (27) test item, it can be achieved that avionics system
Various bus datas, non-bus signal are tested；
The flight simulation module (23) realizes the state of flight of simulation the machine and multiple target aircrafts, exports flight parameter number
According to for the driver and simulator (24) offer dynamic exciting data；
The driver and simulator (24) provide outside avionics system under the data-driven of the flight simulation module (23)
The simulation and excitation of Dynamic Signal, signal needed for guaranteeing avionics system various kinds of sensors or terminal proper testing, the signal
Including RS-422, HB6096 signal；Type, control logic characteristic, function and the time characteristic signals of weapon；The spy of radar target
Reference number；The navigation signals such as speech, data communication and orientation, distance, height；Various voices and the light letter alerted on machine
Number；
General and ancillary equipment (25) the controllable power power supply and liquid cooling pressure supply support tested airborne products and described basic
The electrical crosslinking of integrated-type test macro (2), provides the resource of product and equipment working environment, and the resource includes power supply power supply
Distribution, cold air and liquid cooling, analog capsule cabin, joint-trial rack, test cable, attenuator and absorbing load Support Resource；
The real-time network (26) is used cooperatively by Reflective memory network and gigabit Ethernet, is needing real-time transmission data
In device resource, realizes to include emulation data, test data, the network real-time Transmission of control command information, form the extension
The control of simulation type test macro (3) and properties of product type test macro (4) to basic integrated-type test macro (2) related resource
Managing network road；
The basic integrated-type test script (27) is used to edit, save, execute the test of the system-wide functions component (11)
Code collection.
3. a kind of aircraft avionics floor synthetic debugging system based on performance test according to claim 1, feature exist
In: the extension emulation test system (3) includes task management machine testpieces (31), avionics system emulator (32), extends and imitate
True type test script (33), mounting rack and exemplar (34)；
Core calculations platform of the task management machine testpieces (31) as avionics system has data, FC network exchange, figure
The comprehensive treatment capability and system storage capacity of shape/image and video, when lacking airborne task management machine equipment, it is ensured that institute
The debugging enironment for stating extension simulation type test macro (3) can operate normally, and be the subsystem functional group of the measurand (1)
Part (12) test assignment provides management control and supports；
The avionics system emulator (32) according to the difference of test object, complete in addition to task management machine other avionics systems or
The functional simulation of equipment；Emulation data include inertial navigation, communication and navigation identification, atmosphere data, weapon management, fly control and electromechanics
Control, electronic countermeasure, photoelectricity/radar, data management, the bus interface work that can be realized corresponding airborne products and subsystem are patrolled
Collect simulation；
Extension simulation type test script (33) is used to edit, save, execute the test of the subsystem functional unit (12)
Code collection；
The mounting rack and exemplar (34) include test product mounting rack and control and display exemplar, for substituting airborne equipment
Participate in the spare part of system integration test.
4. a kind of aircraft avionics floor synthetic debugging system based on performance test according to claim 1, feature exist
In: the properties of product type test macro (4) include task management machine examination measurement equipment (41), product special inspecting equipment (42),
Properties of product type test script (43)；
The task management machine examination measurement equipment (41) is matched when equipment of participating in the experiment is detached from the joint-trial environment more detailed interface testing of progress
The commissioning device being tested for the property to task management machine is set, task management in the component-level performance component (13) may be implemented
Optical signal test, video switching and the superposition test, network interface communication test, 1553B communication test, serial port data interactive of machine
Communication, Time Service functional test and DC power supply ripple, RS422 signal level baud rate and electrical characteristics test；
The product special inspecting equipment (42) is special for realizing providing each product in the component-level performance component (13)
Different excitation or analog signal；
The properties of product type test script (43) is used to edit, save, execute the test of the component-level performance component (13)
Code collection.
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