CN107860275A - The military control of simulation and data record apparatus - Google Patents
The military control of simulation and data record apparatus Download PDFInfo
- Publication number
- CN107860275A CN107860275A CN201711192873.7A CN201711192873A CN107860275A CN 107860275 A CN107860275 A CN 107860275A CN 201711192873 A CN201711192873 A CN 201711192873A CN 107860275 A CN107860275 A CN 107860275A
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- Prior art keywords
- test
- simulation
- pxi
- communication
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Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B35/00—Testing or checking of ammunition
- F42B35/02—Gauging, sorting, trimming or shortening cartridges or missiles
-
- 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
Abstract
The invention provides one kind to simulate military control and data record apparatus, including：Equipment self-inspection module, cross inside cable and be connected with interface adapter, complete to carry out self-test to power supply, acquisition channel, bus communication etc.；Interface adapter module, existing signal connection, signal distribution between test signal and test resource；The test signal from product and the analog signal of external equipment input are received, each feature board of PXI combinations is delivered to, so as to realize the communication of equipment and guided missile, acquisition function.The present invention can facilitate tester to carry out interpretation to guided missile state, so as to preferably improve measuring accuracy and reliability.
Description
Technical field
The present invention relates to one kind to enroll equipment, in particular it relates to a kind of military control of simulation and data record apparatus.
Background technology
Guided missile flow inspection before transmission and checking test, it is required for carrying out the flow for simulating military control test.It is only true
The instructions that guided missile missile-borne computer is sent to military control equipment are protected, correct response can be sent, indices are all by side
Follow-up formal transmitting work can be carried out.Therefore, the verification test of military flow control journey is extremely important.
Conventional each type of missile is required for newly developing the military control equipment of model specific, write when military control checking is done
Special force controls software to test snapping into row hair control, so as to verify guided missile state performance.To meet to verify needs, so need to grind
Make the military control equipment of special simulation.When guided missile general assembly is tested, military control flow testing is carried out to guided missile using the military control equipment of simulation,
The possibility that follow-up outfield hair control joint-trial is pinpointed the problems can be greatly reduced.And if simply merely military flow control journey is tested
Card, the operation conditions of many parts of guided missile on stream, implementation status can not reflect to help tester to sentence in detail
It is disconnected.So by the test interface drawn with Missile Body, analog signalses progress is passed to the bullet in flow, and collection judges in real time,
Tester can be facilitated to carry out interpretation to guided missile state, so as to preferably improve measuring accuracy and reliability.Before MISSILE LAUNCHING
The military control experiment in ground or the flow for transmitting check checking test, are required for carrying out the simplation verification of military flow control journey.And if only
It is that merely military flow control journey is verified, the operation conditions of many parts of guided missile on stream, implementation status can not be in detail
Reflect.
The content of the invention
For in the prior art the defects of, it is an object of the invention to provide one kind to simulate military control and data record apparatus, its
Solve the simplation verification of military flow control journey to that must be carried out before guided missile test, transmitting, and provide in military flow control journey, guided missile
Each component working state, the method that implementation effect is capable of automatic data collection analysis, can facilitate tester to sentence guided missile state
Read, so as to preferably improve measuring accuracy and reliability.
According to an aspect of the present invention, there is provided the military control of one kind simulation and data record apparatus, it is characterised in that including：
Equipment self-inspection module, cross inside cable and be connected with interface adapter, complete to power supply, acquisition channel, bus communication
Etc. carry out self-test；
Interface adapter module, existing signal connection, signal distribution between test signal and test resource；Receive next self-produced
Product test signal and external equipment input analog signal, deliver to PXI combination each feature board, so as to realize equipment with
The communication of guided missile, acquisition function；
PXI computer measurement and control composite modules, possess data/address bus communication function, pass through CAN2.0 buses and missile-borne computer
Communication, bookbinding target seeker parameter, revise tuning parameter and enroll bus data in real time, and show in real time in software operation interface
Show that guided missile is input to the signal of calculation machine；And calculate and show in real time test knot according to product and equipment present behavior
Fruit；
The aobvious control composite modules of KVM, it is mainly used in the military control of this simulation and terminal operation and the display of data record apparatus；
Dc source composite module, using AMTEK 28.5V and AMTEK38V dc sources, to be supplied to guided missile
Machine and steering wheel function of supplying power on bullet；
The military control of simulation and data recording module, it is the important component of the military control of whole simulation and data record apparatus, makes
Write with the Labview2012 of NI companies, possess human-computer interaction function, the installation and operation in the military control equipment PXI computers of simulation,
By CAN communication modes and instruction computer communication, receive and decision instruction computer returns the status information accused to judge
Guided missile state, and by controlling dependence test board and dc source, the bullet completed in guided missile power-up and power-up procedures passes simulation
The collecting work of signal is measured, is finally completed the test function of military control test event.
Preferably, the PXI computer measurement and controls composite module be PXIS-2670, PXI-3950/M2G, PXI-2204,
The general name of the standard hardware such as cPCI-7432, cPCI-78415 board combination.
Preferably, the equipment self-inspection module possesses power source loads self-checking function；Possess CAN communication bus self-checking function,
By the way that two CAN passages of CAN boards are connected and composed self-test loop, check whether CAN communication is normal, it is desirable to whole
Individual self-test loop includes product test cable, CAN board；Possesses acquisition channel audit function, by defeated to collection signal
Enter end and apply corresponding voltage, according to the result of display, so as to realize to test cable, collection path and PXI analog input cards
The checking of performance.
Preferably, the PXI computer measurement and controls composite module is by cabinet, A/D boards, CAN communication board, digital I/O plates
The composition such as card, all A/D boards, CAN communication board, digital I/O boards support Labview graphical programming languages.
Compared with prior art, the present invention has following beneficial effect：The present invention combines virtual instrument technique, automatic survey
Control technology, may be used primarily for the hair control experiment of the ground before MISSILE LAUNCHING or the flow for transmitting checks checking test.The present invention
It can be the military control real work flow of the complete simulated missile of tester, carry out system docking with guided missile and joint-trial is tested, so as to
Verify guided missile and the interface coordination and signal response relation of military control.The analog signalses transmitted to guided missile are gathered, shown in real time
Show and automatic discrimination function, working condition, the response feelings of all parts of the tester to guided missile in military flow control journey can be facilitated
Condition carries out analysis interpretation, preferably improves the reliability of test.
Brief description of the drawings
The detailed description made by reading with reference to the following drawings to non-limiting example, further feature of the invention,
Objects and advantages will become more apparent upon：
Fig. 1 is the structural representation of the military control of present invention simulation and data record apparatus.
Fig. 2 is the fundamental diagram of the military control of present invention simulation and data record apparatus.
Embodiment
With reference to specific embodiment, the present invention is described in detail.Following examples will be helpful to the technology of this area
Personnel further understand the present invention, but the invention is not limited in any way.It should be pointed out that the ordinary skill to this area
For personnel, without departing from the inventive concept of the premise, various modifications and improvements can be made.These belong to the present invention
Protection domain.
As shown in figure 1, the military control of present invention simulation and data record apparatus include：
Equipment self-inspection module, cross inside cable and be connected with interface adapter, can complete to power supply, acquisition channel, bus
Communication etc. carries out self-test, and its concrete function is as follows：Possesses power source loads self-checking function；Possess CAN (ControllerArea
Network, controller LAN) communication bus self-checking function, by the way that two CAN passages of CAN boards are connected and composed
Self-test loop, check whether CAN communication is normal, it is desirable to which whole self-test loop includes product test cable, CAN plate
Card；Possess acquisition channel audit function, by applying corresponding voltage to collection signal input part, according to the result of display, from
And realize the checking to test cable, collection path and PXI analog input card performances.
Interface adapter module, existing signal connection, signal distribution between test signal and test resource.Receive next self-produced
The analog signal of test signal and the external equipment input of product, delivers to PXI (PCI extensions for
Instrumentation, the PCI towards instrument system extend) each feature board of combination, so as to realize equipment and guided missile
Communication, acquisition function.
PXI computer measurement and control composite modules, possess data/address bus communication function, pass through CAN2.0 buses and missile-borne computer
Communication, bookbinding target seeker parameter, revise tuning parameter and enroll bus data in real time, and show in real time in software operation interface
Show that guided missile is input to the signal of calculation machine；And calculate and show in real time test knot according to product and equipment present behavior
Fruit.From functionally, PXI computer measurement and controls composite module is by cabinet, A/D boards, CAN communication board, digital I/O boards etc.
Composition, all A/D boards, CAN communication board, digital I/O boards support Labview graphical programming languages.PXIS-2670 is
A groove PXI cabinets of compact 14, support 3U PXI and cPCI modules；PXI-3950/M2G is internal as embedded controller
Windows XP operating systems, the driving of other boards and the military control software of simulation are pre-installed, is whole PXI computer measurement and controls combination
Core；PXI-2204 is the A/D analog input cards of a multichannel；CPCI-7841 can support one as CAN communication board
Energy independent operating or the dual-port CAN interface of bridge joint operation, for realizing the communication function of equipment and guided missile.CPCI-7432 makees
For digital I/O boards, there is provided 32 railway digitals input and the output of 32 railway digitals.Each board is that whole PXI computers are surveyed above
Control combination provides corresponding function.PXI computer measurement and control composite modules, are PXIS-2670, PXI-3950/M2G, PXI-
2204th, the general name of the standard hardware such as cPCI-7432, cPCI-78415 board combination.
The aobvious control composite modules of KVM, it is mainly used in the military control of this simulation and terminal operation and the display of data record apparatus.
Dc source composite module, using AMTEK 28.5V and AMTEK38V dc sources, to be supplied to guided missile
Machine and steering wheel function of supplying power on bullet.
The military control of simulation and data recording module, it is the important component of the military control of whole simulation and data record apparatus, makes
Write with the Labview2012 of NI companies, possess human-computer interaction function, the installation and operation in the military control equipment PXI computers of simulation,
By CAN communication modes and instruction computer communication, receive and decision instruction computer returns the status information accused to judge
Guided missile state, and by controlling dependence test board and dc source, the bullet completed in guided missile power-up and power-up procedures passes simulation
The collecting work of signal is measured, is finally completed the test function of military control test event.
The military control technology write compared to traditional military control platform, the present invention also there is certain function to extend, i.e., increased
The analog signalses collecting test function of guided missile transmission, in the flow of the military control of simulation, or even rear state is penetrated, the present invention can
Continue the collection that bullet passes analog quantity, i.e., after firing order, guided missile simulation in-flight continues all kinds of letters to guided missile passback
Number it is acquired, facilitates tester to continue interpretation to guided missile state.
Of the invention and tested guided missile product test connection figure is as shown in Fig. 2 the military control of present invention simulation and data record apparatus 1
By communicating, collection cable 2 is connected with the test mouth of tested guided missile product 3, simulates realistic objective by infrared target source, completes
Force control flowsheeting and bullet pass Signals collecting function.
The present invention completes a kind of design and development for simulating military control and data record apparatus, and the present invention has been successfully applied to
In the general assembly test of certain type of missile, equipment communication precision is suitable with actual military control equipment, and product multiple signals are carried out
Collecting test, the application effect of true military control is preferably simulated, achieves good detection verification the verifying results.
The specific embodiment of the present invention is described above.It is to be appreciated that the invention is not limited in above-mentioned
Particular implementation, those skilled in the art can make various deformations or amendments within the scope of the claims, this not shadow
Ring the substantive content of the present invention.
Claims (4)
1. the military control of one kind simulation and data record apparatus, it is characterised in that including：
Equipment self-inspection module, cross inside cable and be connected with interface adapter, complete to the side such as power supply, acquisition channel, bus communication
Face carries out self-test；
Interface adapter module, existing signal connection, signal distribution between test signal and test resource；Receive from product
Test signal and the analog signal of external equipment input, each feature board of PXI combinations is delivered to, so as to realize equipment and guided missile
Communication, acquisition function；
PXI computer measurement and control composite modules, possess data/address bus communication function, are led to by CAN2.0 buses with missile-borne computer
News, bookbinding target seeker parameter, revise tuning parameter and enroll bus data, and the real-time display in software operation interface in real time
Guided missile is input to the signal of calculation machine；And calculate and show in real time test knot according to product and equipment present behavior
Fruit；
The aobvious control composite modules of KVM, it is mainly used in the military control of this simulation and terminal operation and the display of data record apparatus；
Dc source composite module, using AMTEK 28.5V and AMTEK38V dc sources, to be supplied on Missile Body
Machine and steering wheel function of supplying power；
The military control of simulation and data recording module, it is the important component of the military control of whole simulation and data record apparatus, uses NI
The Labview2012 of company writes, and possesses human-computer interaction function, the installation and operation in the military control equipment PXI computers of simulation, passes through
CAN communication modes and instruction computer communication, are received and decision instruction computer returns the status information accused to judge guided missile
State, and by controlling dependence test board and dc source, complete the bullet in guided missile power-up and power-up procedures and pass analog quantity letter
Number collecting work, be finally completed the test function of military control test event.
2. simulation force control according to claim 1 and data record apparatus, it is characterised in that the PXI computer measurement and controls
Composite module is the standard hardware board such as PXIS-2670, PXI-3950/M2G, PXI-2204, cPCI-7432, cPCI-78415
The general name of combination.
3. simulation force control according to claim 1 and data record apparatus, it is characterised in that the equipment self-inspection module tool
Stand-by power source loads self-checking function；Possesses CAN communication bus self-checking function, by the way that two CAN passages of CAN boards are connected
Self-test loop is formed, checks whether CAN communication is normal, it is desirable to which whole self-test loop includes product test cable, CAN
Board；Possess acquisition channel audit function, by applying corresponding voltage to collection signal input part, according to the result of display,
So as to realize the checking to test cable, collection path and PXI analog input card performances.
4. simulation force control according to claim 1 and data record apparatus, it is characterised in that the PXI computer measurement and controls
Composite module is made up of cabinet, A/D boards, CAN communication board, digital I/O boards etc., all A/D boards, CAN communication board,
Digital I/O boards support Labview graphical programming languages.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711192873.7A CN107860275A (en) | 2017-11-24 | 2017-11-24 | The military control of simulation and data record apparatus |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711192873.7A CN107860275A (en) | 2017-11-24 | 2017-11-24 | The military control of simulation and data record apparatus |
Publications (1)
| Publication Number | Publication Date |
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| CN107860275A true CN107860275A (en) | 2018-03-30 |
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ID=61702659
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| CN201711192873.7A Pending CN107860275A (en) | 2017-11-24 | 2017-11-24 | The military control of simulation and data record apparatus |
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Cited By (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110119097A (en) * | 2019-04-08 | 2019-08-13 | 上海机电工程研究所 | The weapon system HWIL simulation data similarity method of inspection |
| CN110427291A (en) * | 2019-07-01 | 2019-11-08 | 江西洪都航空工业集团有限责任公司 | A kind of embedded software is from closed loop verification method |
| CN111312006A (en) * | 2020-03-03 | 2020-06-19 | 上海机电工程研究所 | Teaching demonstration device and method for mixed loading and launching control of multiple weapons |
| CN111504142A (en) * | 2019-12-15 | 2020-08-07 | 湖北航天飞行器研究所 | Universal missile simulator and simulation method |
| 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 |
| CN112857399A (en) * | 2021-01-22 | 2021-05-28 | 上海机电工程研究所 | Portable ship integrated navigation simulation system, method and medium for armed control system |
| CN113205719A (en) * | 2021-05-12 | 2021-08-03 | 中国人民解放军海军航空大学航空作战勤务学院 | Missile technology preparation simulation system |
| CN113267095A (en) * | 2021-05-14 | 2021-08-17 | 上海机电工程研究所 | Portable missile automatic test diagnosis device and diagnosis method |
| CN113377081A (en) * | 2021-06-08 | 2021-09-10 | 中国人民解放军陆军工程大学 | Simplified test module for missile equipment |
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Cited By (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110119097A (en) * | 2019-04-08 | 2019-08-13 | 上海机电工程研究所 | The weapon system HWIL simulation data similarity method of inspection |
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| CN111312006A (en) * | 2020-03-03 | 2020-06-19 | 上海机电工程研究所 | Teaching demonstration device and method for mixed loading and launching control of multiple weapons |
| 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 |
| CN112857399A (en) * | 2021-01-22 | 2021-05-28 | 上海机电工程研究所 | Portable ship integrated navigation simulation system, method and medium for armed control system |
| CN113205719A (en) * | 2021-05-12 | 2021-08-03 | 中国人民解放军海军航空大学航空作战勤务学院 | Missile technology preparation simulation system |
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| CN113267095A (en) * | 2021-05-14 | 2021-08-17 | 上海机电工程研究所 | Portable missile automatic test diagnosis device and diagnosis method |
| CN113377081A (en) * | 2021-06-08 | 2021-09-10 | 中国人民解放军陆军工程大学 | Simplified test module for missile equipment |
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Application publication date: 20180330 |