CN105758270B - Wound packages Radio Fuze of Missile test system and method for testing - Google Patents
Wound packages Radio Fuze of Missile test system and method for testing Download PDFInfo
- Publication number
- CN105758270B CN105758270B CN201610188738.4A CN201610188738A CN105758270B CN 105758270 B CN105758270 B CN 105758270B CN 201610188738 A CN201610188738 A CN 201610188738A CN 105758270 B CN105758270 B CN 105758270B
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- Prior art keywords
- fuse
- signal
- module
- additional antenna
- accumulating
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- 238000012360 testing method Methods 0.000 title claims abstract description 65
- 238000000034 method Methods 0.000 title claims abstract description 25
- 238000012545 processing Methods 0.000 claims abstract description 26
- 239000002131 composite material Substances 0.000 claims abstract description 18
- 230000005284 excitation Effects 0.000 claims abstract description 9
- 238000009434 installation Methods 0.000 claims abstract description 8
- 238000004891 communication Methods 0.000 claims description 18
- 230000005611 electricity Effects 0.000 claims description 3
- 230000006978 adaptation Effects 0.000 claims description 2
- 230000006698 induction Effects 0.000 claims description 2
- 230000006378 damage Effects 0.000 abstract description 3
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 description 4
- 230000005540 biological transmission Effects 0.000 description 3
- 238000010586 diagram Methods 0.000 description 3
- 230000009286 beneficial effect Effects 0.000 description 2
- 238000001035 drying Methods 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 2
- 229910052757 nitrogen Inorganic materials 0.000 description 2
- 238000005086 pumping Methods 0.000 description 2
- 230000006641 stabilisation Effects 0.000 description 2
- 238000011105 stabilization Methods 0.000 description 2
- 230000015572 biosynthetic process Effects 0.000 description 1
- 238000013016 damping Methods 0.000 description 1
- 230000003247 decreasing effect Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000011049 filling Methods 0.000 description 1
- 238000001914 filtration Methods 0.000 description 1
- 239000007789 gas Substances 0.000 description 1
- 239000007769 metal material Substances 0.000 description 1
- 238000011056 performance test Methods 0.000 description 1
- 230000005855 radiation Effects 0.000 description 1
- 238000009666 routine test Methods 0.000 description 1
- 238000007789 sealing Methods 0.000 description 1
- 238000003786 synthesis reaction Methods 0.000 description 1
- 230000009897 systematic effect Effects 0.000 description 1
- 238000010998 test method Methods 0.000 description 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42C—AMMUNITION FUZES; ARMING OR SAFETY MEANS THEREFOR
- F42C21/00—Checking fuzes; Testing fuzes
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Radar Systems Or Details Thereof (AREA)
Abstract
The invention discloses a kind of wound packages Radio Fuze of Missile test system and method for testing, additional antenna, main control computer, command module, microwave video composite module, vxi bus cabinet, comprehensive adapter combination module, remote control cover, signal processing circuit and fuse incentive combination module that the system includes dynamic excitation device, is installed at accumulating launching tube front end, the signal processing circuit are connected with additional antenna signal end；The method includes：Feeder line and test cable are tested and removed to installation additional antenna, connection additional antenna and test system, installation test cable, electronic fuse automatically；Signal processing circuit is connected additional antenna by the system by feeder line, closed loop link is formed, without disassembling accumulating launching tube protecgulum, it is to avoid the destruction original storage condition of guided missile, improves efficiency；The method forms signal link using signal processing circuit with feeder line and additional antenna, and response signal is passed into main control computer to assess the performance of electronic fuse, safety, efficiently.
Description
Technical field
Draw the present invention relates to Radio Fuze of Missile technical field of performance test, more particularly to a kind of wound packages guided missile radio
Letter test system and method for testing.
Background technology
Certain type guided missile uses wound packages form, is usually placed in accumulating launching tube.Accumulating launching tube uses metal material, makes
External wireless electric signal cannot be introduced into cylinder, so as to protect guided missile in cylinder to avoid being influenceed by external electromagnetic environment；Launching tube
Sealing, and filling drying nitrogen, air pressure is maintained at 125kPa or so, for guided missile provides good storage condition.The guided missile is used
Electronic fuse to be located at guided missile anterior.To ensure that electronic fuse is functional, it is necessary to carry out routine test to it.
It is divided into protecgulum, cylinder, bonnet on accumulating transmitting barrel structure；Electronic fuse is located at guided missile front portion, launches with accumulating
Cylinder protecgulum correspondence.Electronic fuse surface be provided with it is left, upper right, bottom three antennas, centered on the guided missile longitudinal axis substantially according to
120 ° or so are spaced, each antenna beam center line and the guided missile longitudinal axis 70 ° or so of angle of forward direction, longitudinally asymmetric flat in guided missile
15 ° or so of half-power beam width in face, three antenna beams are covering 360 ° in longitudinal axis plane.
At present, wound packages Radio Fuze of Missile test is realized based on special test system.The test system is
The Auto-Test System of " vxi bus technology+virtual instrument technique ", also swashs comprising main control computer, microwave video combination, fuse
The equipment such as combination, dynamic excitation device, antenna feeder cover, remote control cover are encouraged, during test, system makes electronic fuse startup work, fuse
By 3 antennas to emission microwave pulse signal, fuse incentive combination is input into after being received by antenna feeder cover；Fuse incentive combination exists
On the basis of being analyzed to microwave pulse signal, corresponding analog echo signal is produced, output to antenna feeder cover and to drawing on bullet
Letter aerial radiation；Electronic fuse receives analog echo signal by antenna, and the response signal produced after analyzing and processing is defeated
Go out to vxi bus instrument, judge the performance of electronic fuse according to the signature analysis to response signal by it.
, it is necessary to unload accumulating launching tube protecgulum first in existing test process, the antenna feeder enclosure in test system is existed
On fuse, from fuse incentive combination through antenna feeder cover to fuze antenna radiated radio frequency (RF) analog echo signal, while being received by antenna feeder cover
The RF pulse signal that electronic fuse is sent by its antenna, realizes the test to electronic fuse.After being completed, also need
Accumulating launching tube protecgulum is reinstalled, to drying nitrogen is filled in accumulating launching tube to 125kPa or so, airtight test is carried out, caused
Test implementation process is cumbersome, required time is long, and guided missile departs from original storage condition, may face complicated electricity in test process
The outstanding problems such as the influence of magnetic environment.
The content of the invention
The technical problems to be solved by the invention are to provide a kind of wound packages Radio Fuze of Missile test system, at signal
Reason circuit connects additional antenna by feeder line, closed loop link is formed, without disassembling accumulating launching tube protecgulum, it is to avoid destruction guided missile is former
Beginning storage condition, improves efficiency, it is to avoid disassemble rear electronic fuse is influenceed by external electromagnetic environment.
The technical problems to be solved by the invention are also to provide a kind of wound packages Radio Fuze of Missile method of testing, using letter
Number process circuit forms signal link with feeder line and additional antenna, is done directly the signal between test system and electronic fuse
Receive and launch, and response signal can be passed to main control computer and assess the performance of electronic fuse, safety, efficiently.
In order to solve the above technical problems, the technical solution used in the present invention is：A kind of wound packages Radio Fuze of Missile is surveyed
Test system, including dynamic excitation device, the additional antenna, main control computer, command module, micro- that is installed at accumulating launching tube front end
Ripple video composite module, vxi bus cabinet, comprehensive adapter combination module, remote control cover, signal processing circuit and fuse incentive combination
Module, the signal processing circuit is connected with additional antenna signal end, and the main control computer is borrowed with microwave video composite module
Help GPIB two-way communications, the command module is by means of IEEE1394 buses and main control computer two-way communication, the order
Module and vxi bus cabinet two-way communication, vxi bus cabinet and comprehensive adapter combination module two-way communication, the comprehensive adaptation
The also supporting installation function composite module of composite module and and his like power supply, the signal processing circuit and fuse incentive combination module are double
To communication, the fuse incentive combination module and comprehensive adapter combination module two-way communication, the dynamic excitation device and synthesis
Adapter combination is bi-directionally connected, and microwave video composite module is bi-directionally connected with remote control cover, and remote control cover leads to accumulating launching tube control end
Letter, the accumulating launching tube control end connects comprehensive adapter combination module by means of test cable.
The signal processing circuit includes the first wave filter, the first amplifier, the first adjustable attenuator, the ring that are sequentially connected in series
Shape device, the second wave filter, the second amplifier and the second adjustable attenuator, the circulator connect additional antenna by feeder line, the
One wave filter receives the signal of fuse incentive combination module, the second adjustable attenuator signal output part connection fuse incentive combination mould
Block signal input.
The additional antenna is microstrip antenna array, installation SMA interfaces supporting with microstrip antenna array.
In order to solve the above technical problems, the present invention is also adopted the technical scheme that：A kind of wound packages Radio Fuze of Missile is surveyed
The method of examination, comprises the following steps：
The first step：Additional antenna is installed, microstrip antenna array is installed in accumulating launching tube front end；
Second step：Connection additional antenna and test system, the ring of additional antenna and signal processing circuit is connected using feeder line
Shape device；
3rd step:Test cable is installed, accumulating launching tube control end and comprehensive adapter combination mould are connected using test cable
Block；
4th step：Electronic fuse is tested automatically；
5th step：Feeder line and test cable are removed, test is completed.
4th step includes：
1) system drive electronic fuse, is at working condition；
2) signal processing circuit receives the microwave pulse signal of accumulating launching tube antenna transmitting, and it is sharp to pass it to fuse
Encourage composite module；
3) fuse incentive combination module produces echo, and the echo of generation is passed into additional antenna, electronic fuse shape
Into response signal, and response signal is passed into vxi bus and main control computer；
4) main control computer passes through the performance of the response signal judgement electronic fuse for receiving.
It is using the beneficial effect produced by above-mentioned technical proposal：The system connects signal processing circuit by feeder line
Additional antenna, forms closed loop link, without disassembling accumulating launching tube protecgulum, it is to avoid the destruction original storage condition of guided missile, improves effect
Rate, it is to avoid disassemble rear electronic fuse is influenceed by external electromagnetic environment.
It is using the beneficial effect produced by above-mentioned technical proposal：The method is using signal processing circuit and feeder line and attached
Plus antenna forms signal link, the signal being done directly between test system and electronic fuse is received and launched, and can be by sound
Induction signal passes to main control computer to assess the performance of electronic fuse, safety, efficiently.
Brief description of the drawings
Fig. 1 is systematic schematic diagram of the invention；
Fig. 2 is signal processing circuit schematic diagram；
Fig. 3 is additional antenna mounting structure schematic diagram；
Fig. 4 is the left view of Fig. 3.
Specific embodiment
With reference to the accompanying drawing in the embodiment of the present invention, the technical scheme in the embodiment of the present invention is carried out clear, complete
Ground description, it is clear that described embodiment is only a part of embodiment of the invention, rather than whole embodiments.It is based on
Embodiment in the present invention, it is every other that those of ordinary skill in the art are obtained under the premise of creative work is not made
Embodiment, belongs to the scope of protection of the invention.
Many details are elaborated in the following description in order to fully understand the present invention, but the present invention can be with
Other manner described here is different from using other to implement, those skilled in the art can be without prejudice to intension of the present invention
In the case of do similar popularization, therefore the present invention is not limited by following public specific embodiment.
As shown in figure 1, the invention discloses a kind of wound packages Radio Fuze of Missile test system, including dynamic exciting dress
The additional antenna that put, is installed at accumulating launching tube front end, main control computer, command module, microwave video composite module, VXI are total
Line cabinet, comprehensive adapter combination module, remote control cover, signal processing circuit (referring to accompanying drawing 2) and fuse incentive combination module, it is described
Signal processing circuit is connected with additional antenna signal end, and the main control computer is double by means of GPIB with microwave video composite module
To communication, the command module is by means of IEEE1394 buses and main control computer two-way communication, and the command module is total with VXI
Line cabinet two-way communication, vxi bus cabinet is also matched somebody with somebody with comprehensive adapter combination module two-way communication, the comprehensive adapter combination module
Set installation function composite module and and his like power supply, the signal processing circuit and fuse incentive combination module two-way communication are described
Fuse incentive combination module and comprehensive adapter combination module two-way communication, the dynamic excitation device are two-way with comprehensive adapter combination
Connection, microwave video composite module is bi-directionally connected with remote control cover, and remote control cover communicates with accumulating launching tube control end, the accumulating hair
Shooting cylinder control end connects comprehensive adapter combination module by means of test cable；The signal processing circuit includes be sequentially connected in series the
One wave filter, the first amplifier, the first adjustable attenuator, circulator, the second wave filter, the second amplifier and the second adjustable damping
Device, the circulator connects additional antenna by feeder line, and the first wave filter receives the signal of fuse incentive combination module, and second can
Controlled attenuator signal output part connects fuse incentive combination module by signal input；The additional antenna is microstrip antenna array, with
The supporting installation SMA interfaces of microstrip antenna array.
During concrete application, electronic fuse transmission signal is through accumulating launching tube additional antenna (referring to accompanying drawing 3-4)
Process circuit is received and be fed to, through circulator input filter, the ambient interferences of other frequencies is filtered, amplifier is amplified
To appropriate level, the entire gain of adjustable attenuator adjustment transmission channel so that enter the fuse transmission signal of test system
It is maintained at the available horizontal of stabilization；The pumping signal that fuse incentive combination is produced after filtering, is put through feeder line input processing circuit
Greatly, the treatment such as Gain tuning, through circulator, feeder line to additional antenna so that the pumping signal that fuze antenna is received on bullet is protected
Hold the available horizontal in stabilization.
After accumulating launching tube additional antenna, Radio Fuze of Missile only needs connecting test system as follows when testing
With tested wound packages guided missile：1. test system and process circuit are coupled together using feeder line, also can is with test by process circuit
System (fuse incentive combination) keeps connection, it is not necessary to all reconnect feeder line during test every time；2. 3 feeder lines are utilized by process circuit
SAM interfaces with 3 additional antennas on accumulating launching tube protecgulum are connected respectively.Compared to when former method, the equipment in test connects
Work is connect to be simplified.
The invention also discloses a kind of method of wound packages Radio Fuze of Missile test, comprise the following steps：
The first step：Additional antenna is installed, microstrip antenna array is installed in accumulating launching tube front end；
Second step：Connection additional antenna and test system, the ring of additional antenna and signal processing circuit is connected using feeder line
Shape device；
3rd step:Test cable is installed, accumulating launching tube control end and comprehensive adapter combination mould are connected using test cable
Block；
4th step：Electronic fuse is tested automatically；
5th step：Feeder line and test cable are removed, test is completed.
4th step includes：
1) system drive electronic fuse, is at working condition；
2) signal processing circuit receives the microwave pulse signal of accumulating launching tube antenna transmitting, and it is sharp to pass it to fuse
Encourage composite module；
3) fuse incentive combination module produces echo, and the echo of generation is passed into additional antenna, electronic fuse shape
Into response signal, and response signal is passed into vxi bus and main control computer；
4) main control computer passes through the performance of the response signal judgement electronic fuse for receiving.
During concrete application, connecting test cable first then starts test program and realizes that radio draws the method
The automatic test of letter, pulls down test cable afterwards, that is, complete test job.Compared to former testing process, accumulating transmitting is eliminated
The operation of the time and effort consuming such as gas charge and discharge, airtight test in the dismounting of cylinder protecgulum and cylinder, operating process is greatly simplified, the operating time
Greatly shorten, difficulty is decreased obviously, it is more loose to require, only have to the fixing that feeder line is connected with the SAM interfaces of additional antenna
Special requirement, reduce the uncertainty and insecurity in test process to greatest extent.
Claims (5)
1. a kind of wound packages Radio Fuze of Missile test system, it is characterised in that：Including dynamic excitation device, it is installed at accumulating hair
The additional antenna of shooting cylinder front end, main control computer, command module, microwave video composite module, vxi bus cabinet, comprehensive adaptation
Composite module, remote control cover, signal processing circuit and fuse incentive combination module, the signal processing circuit and additional antenna signal
End connection, the main control computer and microwave video composite module by means of GPIB two-way communications, the command module by means of
IEEE1394 buses and main control computer two-way communication, the command module and vxi bus cabinet two-way communication, vxi bus machine
Case and comprehensive adapter combination module two-way communication, the also supporting installation function composite module of comprehensive adapter combination module and and his like
Power supply, the signal processing circuit and fuse incentive combination module two-way communication, the fuse incentive combination module are suitable with comprehensive
With composite module two-way communication, the dynamic excitation device is bi-directionally connected with comprehensive adapter combination, microwave video composite module with
Remote control cover is bi-directionally connected, and remote control cover communicates with accumulating launching tube control end, and the accumulating launching tube control end is by means of test electricity
The comprehensive adapter combination module of cable connection.
2. wound packages Radio Fuze of Missile test system according to claim 1, it is characterised in that：The signal transacting electricity
Road includes that the first wave filter being sequentially connected in series, the first amplifier, the first adjustable attenuator, circulator, the second wave filter, second are put
Big device and the second adjustable attenuator, the circulator connect additional antenna by feeder line, and the first wave filter receives fuse excitation group
The signal of matched moulds block, the second adjustable attenuator signal output part connection fuse incentive combination module by signal input.
3. wound packages Radio Fuze of Missile test system according to claim 2, it is characterised in that：The additional antenna is
Microstrip antenna array, installation SMA interfaces supporting with microstrip antenna array.
4. the method that a kind of use test system as claimed in claim 1 carries out wound packages Radio Fuze of Missile test, it is special
Levy and be：Comprise the following steps：
The first step：Additional antenna is installed, microstrip antenna array is installed in accumulating launching tube front end；
Second step：Connection additional antenna and test system, the circulator of additional antenna and signal processing circuit is connected using feeder line；
3rd step:Test cable is installed, accumulating launching tube control end and comprehensive adapter combination module are connected using test cable；
4th step：Electronic fuse is tested automatically；
5th step：Feeder line and test cable are removed, test is completed.
5. the method that wound packages Radio Fuze of Missile according to claim 4 is tested, it is characterised in that：The 4th step bag
Include：
1) system drive electronic fuse, is at working condition；
2) signal processing circuit receives the microwave pulse signal of accumulating launching tube antenna transmitting, and passes it to fuse excitation group
Matched moulds block；
3) fuse incentive combination module produces echo, and the echo of generation is passed into additional antenna, and electronic fuse forms sound
Induction signal, and response signal is passed into vxi bus and main control computer；
4) main control computer passes through the performance of the response signal judgement electronic fuse for receiving.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610188738.4A CN105758270B (en) | 2016-03-30 | 2016-03-30 | Wound packages Radio Fuze of Missile test system and method for testing |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610188738.4A CN105758270B (en) | 2016-03-30 | 2016-03-30 | Wound packages Radio Fuze of Missile test system and method for testing |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN105758270A CN105758270A (en) | 2016-07-13 |
| CN105758270B true CN105758270B (en) | 2017-06-16 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610188738.4A Expired - Fee Related CN105758270B (en) | 2016-03-30 | 2016-03-30 | Wound packages Radio Fuze of Missile test system and method for testing |
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Families Citing this family (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109104253B (en) * | 2018-09-28 | 2023-10-31 | 中国人民解放军陆军工程大学 | Remote control hood calibrating device of missile testing system |
| CN110855379B (en) * | 2019-10-30 | 2021-12-24 | 中国空空导弹研究院 | Passive forwarding system suitable for enclosed space |
| CN111664740B (en) * | 2020-05-28 | 2023-01-17 | 中国人民解放军32181部队 | Passive microwave communication adapter and system |
| CN111692930B (en) * | 2020-06-24 | 2022-04-22 | 北京宏动科技有限公司 | Universal radio fuse throwing test system |
| CN113377081B (en) * | 2021-06-08 | 2022-11-04 | 中国人民解放军陆军工程大学 | Test system of guided missile control box |
| CN113703010B (en) * | 2021-08-25 | 2023-07-07 | 上海机电工程研究所 | Pulse Doppler radar guided missile testing equipment and testing method thereof |
Family Cites Families (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3942446A (en) * | 1974-09-06 | 1976-03-09 | The United States Of America As Represented By The Secretary Of The Army | Optical fuze and/or miss distance indicator |
| US5117230A (en) * | 1991-04-12 | 1992-05-26 | The United States Of America As Represented By The Secretary Of The Army | Electronic target radar simulator |
| CN101256230A (en) * | 2007-11-21 | 2008-09-03 | 北京理工大学 | Continuous wave chaos phase-modulation radio fuse detection system and demodulation method |
| CN103837868B (en) * | 2013-12-12 | 2016-05-25 | 江南机电设计研究所 | A kind of side direction exploring antenna fusee signal treating apparatus and method thereof |
| CN205482635U (en) * | 2016-03-30 | 2016-08-17 | 中国人民解放军军械工程学院 | Wound packages guided missile radio fuse test system |
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2016
- 2016-03-30 CN CN201610188738.4A patent/CN105758270B/en not_active Expired - Fee Related
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| CN105758270A (en) | 2016-07-13 |
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