CN106094566A - A kind of method for low cost universal ground experiment simulation carrier aircraft system - Google Patents
A kind of method for low cost universal ground experiment simulation carrier aircraft system Download PDFInfo
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- CN106094566A CN106094566A CN201610420238.9A CN201610420238A CN106094566A CN 106094566 A CN106094566 A CN 106094566A CN 201610420238 A CN201610420238 A CN 201610420238A CN 106094566 A CN106094566 A CN 106094566A
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- carrier aircraft
- air weapon
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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
- G05B17/00—Systems involving the use of models or simulators of said systems
- G05B17/02—Systems involving the use of models or simulators of said systems electric
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Abstract
A kind of method for low cost universal ground experiment simulation carrier aircraft system, high-performance industrial computer is used to test as carrier, gondola is connected with 1553B bus system respectively with air weapon, carrier aircraft information system is installed in high-performance industrial computer simultaneously, the carrier aircraft information system Models computed to ADC, INS, then carrier aircraft information system is connected with the fire control performance element of slave computer by Ethernet, controls carrier aircraft ground simulation test by fire control performance element.In the present invention, carrier aircraft information system truly simulates carrier aircraft, gondola, the triangular crosslinking of air weapon, communication relation, ground test verification condition and technical support is provided for air weapon development, effectively shorten the weapon development cycle, improve development efficiency, reduce checking cost；This system Construction cost is relatively low simultaneously, and composition is simple, easy to use, and takes VC++ to develop, and possesses good human-computer interaction interface, simple to operate, and carrier aircraft information system is portable preferably.
Description
Technical field
The present invention relates to modelling technique field, particularly relate to a kind of for low cost universal ground experiment simulation load
The method of machine system.
Background technology
Along with informationization technology is in the extensive application of military field, air weapon in actual use, generally combines airborne
Gondola auxiliary uses, to improve precise guidance air weapon informationization technology, and then the precision guidance capability of raising air weapon,
Therefore this type of air weapon is in the scientific research stage, substantial amounts of ground test test need to be carried out, to verify carrier aircraft, gondola and air weapon
Relation, the correctness of control logic and communication relation etc. is cross-linked between communication.
Air weapon is in actual on-hook uses, and especially before and after transmitting of disembarking, 1553B information, in interaction, is hung
Cabin is i.e. as the subsystem RT of carrier aircraft, and the BC as air weapon uses simultaneously again, carrier aircraft as higher level's 1553B bus system,
Gondola and air weapon are as subordinate's bus system, and communicate with one another between three；And under the conditions of ground experiment, because of expense, examination
Test the factors such as place, the whole series carrier aircraft system, Towed bird system are set up unrealistic with framework in kind, in traditional application, past
Carry out toward the mode taking simulation carrier aircraft and weapon, simulation gondola to cross-link respectively with weapon, thus during the work of simulated implementation weapon
Information interaction flow, this forming types also can the most effectively verify that between weapon and carrier aircraft, weapon and gondola, communication is closed
The correctness of system, but can not the most truly simulate actual operational state and simulation carrier aircraft, gondola and the weapon three of air weapon
Between communication relation.
Summary of the invention
Technical problem solved by the invention is that providing a kind of simulates carrier aircraft system for the universal ground experiment of low cost
The method of system, to solve the shortcoming in above-mentioned background technology.
Technical problem solved by the invention realizes by the following technical solutions:
A kind of method for low cost universal ground experiment simulation carrier aircraft system, uses high-performance industrial computer to enter as carrier
Row test, gondola is connected with 1553B bus system respectively with air weapon, is provided with carrier aircraft letter in high-performance industrial computer simultaneously
Breath system, the carrier aircraft information system Models computed to ADC, INS, then carrier aircraft information system is by the fire of Ethernet with slave computer
Control performance element connects, and controls carrier aircraft ground simulation test by fire control performance element, specifically comprises the following steps that
1) electric interfaces is formulated
Power supply logics function of supplying power according to air weapon, formulates universal electric interfaces, and electric interfaces meets GJB1188A-
1999 military standard of China, supplied character meets GJB181A-2003 requirement；
2) system cable is set
According to air weapon communication interface characteristic, carry out cable setting in conjunction with actual test environment；
3) carrier aircraft information system
Carrier aircraft information system is the Models computed of ADC, INS, and by the calculation result fire control by Ethernet transmission to slave computer
Performance element, carrier aircraft information system uses VC++ visual development environment to carry out the system integration, and for adapting to ground test, employing is joined
The mode putting file loading is carried out, and when practical operation, according to different air weapon Trajectories examination conditions, sets up different
Carrier aircraft information text file, and carrier aircraft information text carries out respective profiles add according to air weapon emulation examination ballistic conditions
Realizing visualization after load, so that test operation personnel judge loading correctness, this configuration file also can be existing simultaneously
Field is modified at any time；
4) carrier aircraft ground simulation test
Fire control performance element in slave computer, as the functional check part of carrier aircraft information system, is also air weapon control simultaneously
Part, it is as follows that its carrier aircraft ground simulation test realizes step:
A) reception and the task of carrier aircraft information loads
Fire control performance element completes to receive the carrier aircraft real-time resolving information that carrier aircraft information system passes down, and will by 1553B bus
Carrier aircraft real time information, air weapon air Route Planning Method information are loaded onto air weapon；
B) the aobvious control of simulation carrier aircraft
The video frequency collection card collection being arranged in slave computer shows the picture that air weapon of participating in the experiment is uploaded, and is carried by slave computer
USB interface access auxiliary device, with simulation perform air weapon to the search of target, lock, the behaviour in the loop such as amendment
Make；
C) complete carrier aircraft and air weapon is launched the control of flow process
Air weapon is launched flow process and is controlled by fire control performance element, to complete the test of air weapon ground test.
In the present invention, video frequency collection card is inserted in the PCI slot of slave computer, and is also inserted with MBI card in PCI slot；With
Time video frequency collection card be connected with air weapon by video line, MBI card is connected with 1553B bus system by coaxial cable.
In the present invention, the auxiliary device that the USB interface that slave computer carries accesses includes numeric keypad or game paddle, with
Simulated flight person to air weapon in the loop control operation.
Beneficial effect: in the present invention carrier aircraft information system truly simulate carrier aircraft, gondola, the triangular crosslinking of air weapon,
Communication relation, provides ground test verification condition and technical support for air weapon development, effectively shortens the weapon development cycle, carries
High development efficiency, reduces checking cost；This system Construction cost is relatively low simultaneously, and composition is simple, easy to use, system integration hardware
All select prior art products, possess cheap, general, convenient displacement；And take VC++ to develop, possess good man-machine interaction circle
Face, simple to operate, carrier aircraft information system is portable preferably；Upgrading, transform convenient, can meet air weapon ground test test
Demand.
Accompanying drawing explanation
Fig. 1 is the flow chart of presently preferred embodiments of the present invention.
Detailed description of the invention
For the technological means making the present invention realize, creation characteristic, reach purpose and be easy to understand with effect, below knot
Close specific embodiment, the present invention is expanded on further.
A kind of method for low cost universal ground experiment simulation carrier aircraft system, as it is shown in figure 1, use high-performance work
Control machine is tested as carrier, is provided with carrier aircraft information system, by carrier aircraft information system in high-performance industrial computer simultaneously
To ADC(air data computer), INS(inertial navigation) Models computed, then by the fire control of Ethernet TCP/IP and slave computer
Performance element connects；MBI card, video frequency collection card are respectively inserted in the PCI slot of slave computer；Video frequency collection card by video line with
Air weapon is connected；MBI card is connected with 1553B bus system by coaxial cable；Gondola and air weapon are total with 1553B respectively
Wire system connects, and USB interface is the USB interface that slave computer carries, for external numeric keypad or game paddle with simulated flight
Member to air weapon in the loop control operation；Specifically comprise the following steps that
1) electric interfaces is formulated
Power supply logics function of supplying power according to air weapon, formulates universal electric interfaces, and electric interfaces meets GJB1188A-
1999 military standard of China, supplied character meets GJB181A-2003 requirement；
2) system cable is set
According to air weapon communication interface characteristic, carry out cable setting in conjunction with actual test environment；
3) carrier aircraft information system
Carrier aircraft information system is the Models computed of ADC, INS, and by calculation result by Ethernet ICP/IP protocol transmission under
The fire control performance element of position machine, this system uses VC++ visual development environment to carry out the system integration, for adapting to ground test, adopts
The mode loaded with configuration file is carried out, and when practical operation, according to different air weapon Trajectory examination conditions, sets up not
With carrier aircraft information text file, and carrier aircraft information text according to air weapon emulation examination ballistic conditions carry out corresponding configuration literary composition
Part realizes visualization after loading, so that test operation personnel judge loading correctness, this configuration file also may be used simultaneously
It is modified the most at any time；
4) carrier aircraft ground simulation test
Fire control performance element in slave computer, as the functional check part of carrier aircraft information system, is also air weapon control simultaneously
Part, it is as follows that its carrier aircraft ground simulation test realizes step:
A) reception and the task of carrier aircraft information loads
Fire control performance element completes to receive the carrier aircraft real-time resolving information that carrier aircraft information system passes down, and will by 1553B bus
Carrier aircraft real time information, air weapon air Route Planning Method information are loaded onto air weapon；
B) the aobvious control of simulation carrier aircraft
Video frequency collection card collection shows the picture that air weapon of participating in the experiment is uploaded, and the USB2.0 carried by slave computer accesses numeral
Keyboard or game paddle, with simulation perform air weapon to the search of target, lock, the operation in the loop such as amendment；
C) complete carrier aircraft and air weapon is launched the control of flow process
Simulation carrier aircraft performs carrier aircraft fire control and is controlled air weapon transmitting flow process, to complete the examination of air weapon ground test
Test.
In the present embodiment, carrier aircraft information system truly simulates carrier aircraft, gondola, the triangular crosslinking of air weapon, communication
Relation, provides ground test verification condition and technical support for air weapon development, effectively shortens the weapon development cycle, and raising is ground
Efficiency processed, reduces checking cost；This system Construction cost is relatively low simultaneously, and composition is simple, and easy to use, system integration hardware all selects
Select prior art products, possess cheap, general, facilitate the features such as displacement；And take VC++ to develop, possess good man-machine interaction
Interface, simple to operate, carrier aircraft information system is portable preferably；Upgrading, transform convenient, can meet air weapon ground test examination
Test demand.
The ultimate principle of the present invention and principal character and advantages of the present invention have more than been shown and described.The technology of the industry
Personnel, it should be appreciated that the present invention is not restricted to the described embodiments, simply illustrating this described in above-described embodiment and description
The principle of invention, without departing from the spirit and scope of the present invention, the present invention also has various changes and modifications, and these become
Change and improvement both falls within scope of the claimed invention.Claimed scope by appending claims and
Equivalent defines.
Claims (3)
1. the method for low cost universal ground experiment simulation carrier aircraft system, it is characterised in that use high-performance work
Control machine is tested as carrier, and gondola is connected with 1553B bus system respectively with air weapon, simultaneously at high-performance industrial computer
Inside being provided with carrier aircraft information system, the carrier aircraft information system Models computed to ADC, INS, then carrier aircraft information system passes through ether
Net is connected with the fire control performance element of slave computer, controls carrier aircraft ground simulation test by fire control performance element, and concrete steps are such as
Under:
1) electric interfaces is formulated
Power supply logics function of supplying power according to air weapon, formulates universal electric interfaces, and electric interfaces meets GJB1188A-
1999 military standard of China, supplied character meets GJB181A-2003 requirement；
2) system cable is set
According to air weapon communication interface characteristic, carry out cable setting in conjunction with actual test environment；
3) carrier aircraft information system
Carrier aircraft information system is the Models computed of ADC, INS, and by the calculation result fire control by Ethernet transmission to slave computer
Performance element, carrier aircraft information system uses VC++ visual development environment to carry out the system integration, and for adapting to ground test, employing is joined
The mode putting file loading is carried out, and when practical operation, according to different air weapon Trajectories examination conditions, sets up different
Carrier aircraft information text file, and carrier aircraft information text carries out respective profiles add according to air weapon emulation examination ballistic conditions
Realizing visualization after load, so that test operation personnel judge loading correctness, this configuration file also can be existing simultaneously
Field is modified at any time；
4) carrier aircraft ground simulation test
Fire control performance element in slave computer, as the functional check part of carrier aircraft information system, is also air weapon control simultaneously
Part, it is as follows that its carrier aircraft ground simulation test realizes step:
A) reception and the task of carrier aircraft information loads
Fire control performance element completes to receive the carrier aircraft real-time resolving information that carrier aircraft information system passes down, and will by 1553B bus
Carrier aircraft real time information, air weapon air Route Planning Method information are loaded onto air weapon；
B) the aobvious control of simulation carrier aircraft
The video frequency collection card collection being arranged in slave computer shows the picture that air weapon of participating in the experiment is uploaded, and is carried by slave computer
USB interface access auxiliary device, with simulation perform air weapon to the search of target, lock, the behaviour in the loop such as amendment
Make；
C) complete carrier aircraft and air weapon is launched the control of flow process
Air weapon is launched flow process and is controlled by fire control performance element, to complete the test of air weapon ground test.
A kind of method for low cost universal ground experiment simulation carrier aircraft system the most according to claim 1, it is special
Levying and be, video frequency collection card is inserted in the PCI slot of slave computer, and is also inserted with MBI card in PCI slot；Video frequency collection card simultaneously
Being connected with air weapon by video line, MBI card is connected with 1553B bus system by coaxial cable.
A kind of method for low cost universal ground experiment simulation carrier aircraft system the most according to claim 1, it is special
Levying and be, the auxiliary device that the USB interface that slave computer carries accesses includes numeric keypad or game paddle.
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| CN201610420238.9A CN106094566B (en) | 2016-06-13 | 2016-06-13 | A method of carrier aircraft system is simulated for the universal ground experiment of low cost |
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| CN106773777A (en) * | 2016-11-23 | 2017-05-31 | 哈尔滨工业大学 | Spacecraft ground analog simulation method based on augmented reality |
| CN107703774A (en) * | 2017-09-12 | 2018-02-16 | 江西洪都航空工业集团有限责任公司 | A kind of air weapon moving base Transfer Alignment emulation mode |
| CN107856889A (en) * | 2017-10-27 | 2018-03-30 | 北京空间技术研制试验中心 | The method of production that spacecraft platform is mutually matched with loading device |
| CN107991954A (en) * | 2017-11-08 | 2018-05-04 | 江西洪都航空工业集团有限责任公司 | A kind of safety control command simulator |
| CN112256053A (en) * | 2020-09-27 | 2021-01-22 | 中国航空工业集团公司洛阳电光设备研究所 | Fire control photoelectric system of small-sized scouting and fighting unmanned aerial vehicle |
| CN112308422A (en) * | 2020-10-30 | 2021-02-02 | 西北工业大学 | Task planning and solving simulation system and method for remote aerial support carrier |
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Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
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| CN107991954A (en) * | 2017-11-08 | 2018-05-04 | 江西洪都航空工业集团有限责任公司 | A kind of safety control command simulator |
| CN112256053A (en) * | 2020-09-27 | 2021-01-22 | 中国航空工业集团公司洛阳电光设备研究所 | Fire control photoelectric system of small-sized scouting and fighting unmanned aerial vehicle |
| CN112308422A (en) * | 2020-10-30 | 2021-02-02 | 西北工业大学 | Task planning and solving simulation system and method for remote aerial support carrier |
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| CN106094566B (en) | 2019-03-29 |
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