CN105954609B - A kind of whole bullet emulation testing conversion adaptive device of guided munition - Google Patents
A kind of whole bullet emulation testing conversion adaptive device of guided munition Download PDFInfo
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- CN105954609B CN105954609B CN201610259690.1A CN201610259690A CN105954609B CN 105954609 B CN105954609 B CN 105954609B CN 201610259690 A CN201610259690 A CN 201610259690A CN 105954609 B CN105954609 B CN 105954609B
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- G—PHYSICS
- G01—MEASURING; TESTING
- G01R—MEASURING ELECTRIC VARIABLES; MEASURING MAGNETIC VARIABLES
- G01R31/00—Arrangements for testing electric properties; Arrangements for locating electric faults; Arrangements for electrical testing characterised by what is being tested not provided for elsewhere
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- 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
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- General Physics & Mathematics (AREA)
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- General Engineering & Computer Science (AREA)
- Keying Circuit Devices (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
Abstract
The invention discloses a kind of whole bullet emulation testings of guided munition to convert adaptive device comprising conversion circuit, adapter circuit, conversion control circuit and pulse-generating circuit；Advantage is：The present invention is to check the characterisitic parameter, work schedule, data communication etc. of guided munition entirety, simulate, and being monitored to entire Test condition；There is the present invention stronger scalability can complete the testing requirement of new model guided munition based on the present invention, can also meet the testing requirement of digital guided munition.
Description
Technical field
The invention belongs to guided munition technical field of measurement and test, are related to a kind of whole bullet electrical property emulation testing dress of guided munition
It sets.
Background technology
Typically, guided munition product is the sophisticated electronic product constituted based on ten million component, or by several groups
The Complex Structural System of part and component composition.And the Support of Complex Structural System more levels off to a great system engineering.
In this system engineering, it is important that a part be then test system, it mainly completes the various parameters of Complex Structural System
Test and functional verification, including reliability test, ground simulation etc..
Guided munition product univers parameter and functional verification are to test the important process of guided munition overall system performance, nothing
By being preparation stage before production acceptance phase or long term storage stage and transmitting, whole the bullets electrical property of guided munition emulates
Test is all the main method of routine test.
Invention content
Technical problem to be solved by the invention is to provide it is a kind of can by body reserve test interface to guidance
Ammunition integrally carries out the whole bullet emulation testing conversion adaptive device of guided munition of intelligent test.
Used technical solution is to solve above-mentioned technical problem：A kind of whole bullet emulation testing conversion adaptation of guided munition
Device comprising conversion circuit, adapter circuit, conversion control circuit and pulse-generating circuit；
The conversion circuit includes the 25th to the 28th relay and the 18th relay；
The adapter circuit is connected with the corresponding port of Missile Body X8 and selecting switch respectively；
The pulse-generating circuit difference and function generator, number I/O modules are connected with the corresponding port of programmable power supply
It connects；
The conversion control circuit is connected with the corresponding port of digital I/O modules and programmable power supply respectively；
1st normally opened contact KDT25-1s of the port DY1+ of programmable power supply through the 25th relay connects the electricity of Missile Body X8
The positive port DTZ in source；2nd normally opened contact KDT25-2s of the port DY1- of programmable power supply through the 25th relay meets Missile Body X8
The ports GND DTGD；
1st normally opened contact KDT18-1s of the port DY2- of programmable power supply through the 18th relay connects the electricity of Missile Body X8
Source negative terminal mouth DTF；2nd normally opened contact KDT18-2s of the port DY2+ of programmable power supply through the 18th relay meets Missile Body X8
The ports GND DTGD；
The fin test points port DT6 of Missile Body X8 connects described through the 1st normally opened contact KDT28-1 of the 28th relay
The corresponding port of pulse-generating circuit；2nd normally opened contacts of the ports the GND DTGD of Missile Body X8 through the 28th relay
KDT28-2 connects the corresponding port of the pulse-generating circuit；
1st normally opened contact KDT26-1s of the ports the z DT4 of Missile Body X8 through the 26th relay meets the-Y of Missile Body X8
Port DT7；2nd normally opened contact KDT26-2s of the ports the y DT5 of Missile Body X8 through the 26th relay meets the-Z of Missile Body X8
Port DT8；
The fin test points port DT6 of Missile Body X8 connects guided missile through the 1st normally opened contact KDT27-1 of the 27th relay
The ports the VA DT18 of body X8.
The pulse-generating circuit includes phase inverter U11A, phase inverter U11B, counter U12, selector U13, switching molding
Block U14, resistance R90, the first Pulse Width Control relay, port MZ1 and port MGD1；
1st normally opened contact KMZ1-1s of the output end XF1 of function generator through the first Pulse Width Control relay meets institute
State 4 feet of switch module U14；
2nd normally opened contact KMZ1-2s of the output end XF2 of function generator through the first Pulse Width Control relay meets institute
State 3 feet of switch module U14；
11 feet of the switch module U14 meet the output end XF1D of function generator；
12 feet of the switch module U14 meet the output end XF2D of function generator；
2 feet and 5 feet of the switch module U14 meet the port MZ1 respectively；
1st normally opened contact KDT28-1s of the port MZ1 through the 28th relay connects the fin test points of Missile Body X8
Port DT6；
10 feet and 13 feet of the switch module U14 meet the port MGD1 respectively；
2nd normally opened contact KDT28-2s of the port MGD1 through the 28th relay connects the ports GND of Missile Body X8
DTGD；
1 foot of input terminal of the phase inverter U11A meets the port CLK of digital I/O modules；
1 foot of the selector U13 to 4 feet meet the corresponding port D3 ~ D0 of digital I/O modules respectively；The selector U13
12 feet to 15 feet meet the corresponding port D7 ~ D4 of digital I/O modules respectively；
2 foot of output end of the phase inverter U11A connects 5 feet of the counter U12；
3 feet of the counter U12 connect 11 feet of the selector U13；2 feet of the counter U12 connect the selection
10 feet of device U13；6 feet of the counter U12 connect 9 feet of the selector U13；
7 feet of the counter U12 connect its 14 foot；
6 feet of the selector U13 connect 3 foot of input terminal of the phase inverter U11B；The output end 4 of the phase inverter U11B
Foot meets the port+5V+ of programmable power supply through the resistance R90；
4 feet, 11 feet and 16 feet of the counter U12 meet the port+5V+ of programmable power supply respectively；The counter U12's
15 feet, 1 foot, 10 feet, 9 feet and 8 feet are grounded respectively；16 feet of the selector U13 meet the port+5V+ of programmable power supply；The choosing
7 feet and 8 feet for selecting device U13 are grounded respectively；
14 feet of the switch module U14 meet the port+15V+ of programmable power supply；8 feet of the switch module U14 connect program-controlled
Port-the 15V- of power supply.
The adapter circuit includes R10-R13 and port DT11A-DT14A；
The resistance R13 is connected between port DT11A and the ports DT11 of Missile Body X8；
The resistance R12 is connected between port DT12A and the ports DT12 of Missile Body X8；
The resistance R11 is connected between port DT13A and the ports DT13 of Missile Body X8；
The resistance R10 is connected between port DT14A and the ports DT14 of Missile Body X8；
The port DT11A-DT14A connects the corresponding port of selecting switch respectively.
The conversion control circuit includes buffer U1-5, rp-drive U1-11 and exclusion RP1；
Input terminal 1A ~ 6A of the buffer U1-5 connects the corresponding port of digital I/O modules respectively；The buffer U1-5
Output end 1Y ~ 6Y connect the foot of 6 foot of correspondence input terminal of the rp-drive U1-11 ~ 1 respectively；The electricity of the buffer U1-5
Source VCC meets the port+5V+ of programmable power supply；The ground terminal GND ground connection of the buffer U1-5；The rp-drive U1-11
9 feet meet the port+24V+ of programmable power supply；8 feet of the rp-drive U1-11 are grounded；
The foot of 1 foot of input terminal of the rp-drive U1-11 ~ 6 connects the not common end respective tube of the exclusion RP1 respectively
Foot；Port+the 5V+ of the public termination programmable power supply of the exclusion RP1；
The coil KDT25 of 25th relay is connected on 11 foot of output end and program-controlled electric of the rp-drive U1-11
Between the port+24V+ in source；
The coil KDT26 of 26th relay is connected on 12 foot of output end of the rp-drive U1-11 and the journey
Between the port+24V+ for controlling power supply；
The coil KDT27 of 27th relay is connected on 13 foot of output end and program-controlled electric of the rp-drive U1-11
Between the port+24V+ in source；
The coil KDT28 of 28th relay is connected on 14 foot of output end and program-controlled electric of the rp-drive U1-11
Between the port+24V+ in source；
The coil KDT18 of 18th relay is connected on 15 foot of output end and program-controlled electric of the rp-drive U1-11
Between the port+24V+ in source；
The coil KMZ1 of the first Pulse Width Control relay be connected on 16 foot of output end of the rp-drive U1-11 with
Between the port+24V+ of programmable power supply.
The model of the phase inverter U11A and phase inverter U11B is 74LS04；The model of the counter U12
74LS193；The model 74LS151 of the selector U13；The model DG303AAK of the switch module U14；The buffering
The model 74LS07 of device U1-5；The model MC1413 of the rp-drive U1-11.
The beneficial effects of the invention are as follows：The present invention is the characterisitic parameter, work schedule, data communication to guided munition entirety
Etc. being checked, simulated, and entire Test condition is monitored；The present invention has stronger scalability, is with the present invention
Basis can complete the testing requirement of new model guided munition, can also meet the test of digital guided munition.
Description of the drawings
Fig. 1 is principle of the invention block diagram.
Fig. 2 is conversion circuit schematic diagram.
Fig. 3 is pulse-generating circuit schematic diagram.
Fig. 4 is adapter circuit schematic diagram.
Fig. 5 is conversion control circuit schematic diagram.
Fig. 6 is the present invention for the whole functional block diagram for playing electrical property simulation testing device of guided munition.
Specific implementation mode
The embodiment shown in Fig. 1-6 is it is found that it includes industrial personal computer, router, digital multimeter, function generator, journey
Control power supply, selecting switch, number I/O modules, conversion circuit, adapter circuit, conversion control circuit and pulse-generating circuit；
The conversion circuit includes the 25th to the 28th relay and the 18th relay；
The digital multimeter, programmable power supply, function generator, selecting switch and number I/O modules pass through routing respectively
Device is connected with the industrial personal computer；
The digital multimeter is connected with the corresponding port of the selecting switch；
The selecting switch is connected with the corresponding port of Missile Body X8 and the adapter circuit respectively；
The adapter circuit is connected with the corresponding port of Missile Body X8；
The function generator is connected with the corresponding port of the pulse-generating circuit；
The number I/O modules are connected with the corresponding port of the pulse-generating circuit and conversion control circuit respectively；
The programmable power supply is connected with the corresponding port of conversion control circuit and pulse-generating circuit respectively；
1st normally opened contact KDT25-1s of the port DY1+ of the programmable power supply through the 25th relay meets Missile Body X8
Power positive end mouth DTZ；2nd normally opened contact KDT25-2s of the port DY1- of the programmable power supply through the 25th relay connects
The ports the GND DTGD of Missile Body X8；
1st normally opened contact KDT18-1s of the port DY2- of the programmable power supply through the 18th relay meets Missile Body X8
Power supply negative terminal mouth DTF；2nd normally opened contact KDT18-2s of the port DY2+ of the programmable power supply through the 18th relay connects
The ports the GND DTGD of Missile Body X8；
The fin test points port DT6 of Missile Body X8 connects described through the 1st normally opened contact KDT28-1 of the 28th relay
The corresponding port of pulse-generating circuit；2nd normally opened contacts of the ports the GND DTGD of Missile Body X8 through the 28th relay
KDT28-2 connects the corresponding port of the pulse-generating circuit；
1st normally opened contact KDT26-1s of the ports the z DT4 of Missile Body X8 through the 26th relay meets the-Y of Missile Body X8
Port DT7；2nd normally opened contact KDT26-2s of the ports the y DT5 of Missile Body X8 through the 26th relay meets the-Z of Missile Body X8
Port DT8；
The fin test points port DT6 of Missile Body X8 connects guided missile through the 1st normally opened contact KDT27-1 of the 27th relay
The ports the VA DT18 of body X8.
The pulse-generating circuit includes phase inverter U11A, phase inverter U11B, counter U12, selector U13, switching molding
Block U14, resistance R90, the first Pulse Width Control relay, port MZ1 and port MGD1；
1st normally opened contact KMZ1-1s of the output end XF1 of the function generator through the first Pulse Width Control relay
Connect 4 feet of the switch module U14；
The output end XF1D of the function generator connects 11 feet of the switch module U14；
2nd normally opened contact KMZ1-2s of the output end XF2 of the function generator through the first Pulse Width Control relay
Connect 3 feet of the switch module U14；
The output end XF2D of the function generator connects 12 feet of the switch module U14；
2 feet and 5 feet of the switch module U14 meet the port MZ1 respectively；
1st normally opened contact KDT28-1s of the port MZ1 through the 28th relay connects the fin test points of Missile Body X8
Port DT6；
10 feet and 13 feet of the switch module U14 meet the port MGD1 respectively；
2nd normally opened contact KDT28-2s of the port MGD1 through the 28th relay connects the ports GND of Missile Body X8
DTGD；
1 foot of input terminal of the phase inverter U11A meets the port CLK of the number I/O modules；
1 foot of the selector U13 to 4 feet meet the corresponding port D3 ~ D0 of the number I/O modules respectively；The selection
12 feet of device U13 to 15 feet meet the corresponding port D7 ~ D4 of the number I/O modules respectively；
2 foot of output end of the phase inverter U11A connects 5 feet of the counter U12；
3 feet of the counter U12 connect 11 feet of the selector U13；2 feet of the counter U12 connect the selection
10 feet of device U13；6 feet of the counter U12 connect 9 feet of the selector U13；
7 feet of the counter U12 connect its 14 foot；
6 feet of the selector U13 connect 3 foot of input terminal of the phase inverter U11B；The output end 4 of the phase inverter U11B
Foot meets the port+5V+ of the programmable power supply through the resistance R90；
4 feet, 11 feet and 16 feet of the counter U12 meet the port+5V+ of the programmable power supply respectively；The counter
15 feet, 1 foot, 10 feet, 9 feet and 8 feet of U12 are grounded respectively；16 feet of the selector U13 connect the port of the programmable power supply+
5V+；7 feet and 8 feet of the selector U13 are grounded respectively；
6 feet and 9 feet of the switch module U14 connect 4 foot of output end of the phase inverter U11B respectively；
14 feet of the switch module U14 meet the port+15V+ of the programmable power supply；
8 feet of the switch module U14 meet the port -15V- of the programmable power supply；
7 feet of the switch module U14 connect respectively port+15V-, port -15V+ and the port of the programmable power supply+
5V-。
The adapter circuit includes R10-R13 and port DT11A-DT14A；
The resistance R13 is connected between port DT11A and the ports DT11 of Missile Body X8；
The resistance R12 is connected between port DT12A and the ports DT12 of Missile Body X8；
The resistance R11 is connected between port DT13A and the ports DT13 of Missile Body X8；
The resistance R10 is connected between port DT14A and the ports DT14 of Missile Body X8；
The port DT11A-DT14A connects the corresponding port of the selecting switch respectively.
The conversion control circuit includes buffer U1-5, rp-drive U1-11 and resistance R1-1 ~ R1-6；
Input terminal 1A ~ 6A of the buffer U1-5 connects the corresponding port of the number I/O modules respectively；The buffer
Output end 1Y ~ 6Y of U1-5 connects the foot of 6 foot of correspondence input terminal of the rp-drive U1-11 ~ 1 respectively；The buffer U1-5
Power end VCC meet the port+5V+ of the programmable power supply；The ground terminal GND ground connection of the buffer U1-5；The reverse phase is driven
9 feet of dynamic device U1-11 meet the port+24V+ of the programmable power supply；8 feet of the rp-drive U1-11 are grounded；
Port+the 5V+ of the public termination programmable power supply of the 9 foot exclusion RP1, wherein the 6 of the 9 foot exclusion RP1
A not common end pipe foot connects the foot of 1 foot of input terminal of the corresponding rp-drive U1-11 ~ 6 respectively；
The coil KDT25 of 25th relay is connected on 11 foot of output end of the rp-drive U1-11 and the journey
Between the port+24V+ for controlling power supply；
The coil KDT26 of 26th relay is connected on 12 foot of output end of the rp-drive U1-11 and the journey
Between the port+24V+ for controlling power supply；
The coil KDT27 of 27th relay is connected on 13 foot of output end of the rp-drive U1-11 and the journey
Between the port+24V+ for controlling power supply；
The coil KDT28 of 28th relay is connected on 14 foot of output end of the rp-drive U1-11 and the journey
Between the port+24V+ for controlling power supply；
The coil KDT18 of 18th relay is connected on 15 foot of output end of the rp-drive U1-11 and the journey
Between the port+24V+ for controlling power supply；
The coil KMZ1 of the first Pulse Width Control relay be connected on 16 foot of output end of the rp-drive U1-11 with
Between the port+24V+ of the programmable power supply.
The model 34405A of the digital multimeter；The model 33210A of the function generator；The program-controlled electric
The model N6700B in source；The model L4421A of the selecting switch；The model L4450A of the number I/O modules.
The model of the phase inverter U11A and phase inverter U11B is 74LS04；The model of the counter U12
74LS193；The model 74LS151 of the selector U13；The model DG303AAK of the switch module U14；The buffering
The model 74LS07 of device U1-5；The model MC1413 of the rp-drive U1-11.
The test method of Missile Body input and output inspection of the present invention is as follows：Industrial personal computer sends out instruction and passes through number I/O modules
It is transferred to conversion control circuit, so that the normally opened contact of the 18th relay and the 25th relay is closed, powers on；Make the 26th relay
The normally opened contact of device and the 27th relay is closed, short circuit respective terminal, and consumption electric current is read from programmable power supply.
Steering wheel potentiometer PR1, PR2 and "-Y ", "-Z " and signal value:Industrial personal computer sends out instruction and is passed by number I/O modules
It is defeated by conversion control circuit, the normally opened contact of the 28th relay is made to be closed, accesses function generator, pulse command is generated, by work
Control machine controls digital multimeter, and corresponding port data are read in selection.
Rudder electromechanical magnetic valve winding on voltage and STT missile signal "-Y ", "-Z " and voltage:Number is controlled by industrial personal computer
Corresponding port data are read in multimeter, selection.
Embodiment described above is merely a preferred embodiment of the present invention, and the simultaneously exhaustion of non-present invention possible embodiments.
It is any aobvious to made by it under the premise of without departing substantially from the principle of the invention and spirit for persons skilled in the art
And the change being clear to, it should all be contemplated as falling within the claims of the present invention.
Claims (4)
1. adaptive device is converted in a kind of whole bullet emulation testing of guided munition, it is characterised in that：Including conversion circuit, adapter circuit,
Conversion control circuit and pulse-generating circuit；
The conversion circuit includes the 25th to the 28th relay and the 18th relay；
The adapter circuit is connected with the corresponding port of Missile Body X8 and selecting switch respectively；
And function generator, number I/O modules are connected the pulse-generating circuit with the corresponding port of programmable power supply respectively；
The conversion control circuit is connected with the corresponding port of digital I/O modules and programmable power supply respectively；
1st normally opened contact KDT25-1s of the port DY1+ of programmable power supply through the 25th relay is connecing the power supply of Missile Body X8 just
Port DTZ；2nd normally opened contact KDT25-2s of the port DY1- of programmable power supply through the 25th relay meets the GND of Missile Body X8
Port DTGD；
The power supply that 1st normally opened contact KDT18-1s of the port DY2- of programmable power supply through the 18th relay meets Missile Body X8 is negative
Port DTF；2nd normally opened contact KDT18-2s of the port DY2+ of programmable power supply through the 18th relay meets the GND of Missile Body X8
Port DTGD；
The fin test points port DT6 of Missile Body X8 connects the pulse through the 1st normally opened contact KDT28-1 of the 28th relay
The corresponding port of generation circuit；2nd normally opened contact KDT28-2s of the ports the GND DTGD of Missile Body X8 through the 28th relay
Connect the corresponding port of the pulse-generating circuit；
1st normally opened contact KDT26-1s of the ports the z DT4 of Missile Body X8 through the 26th relay connect Missile Body X8-Y-port
DT7；2nd normally opened contact KDT26-2s of the ports the y DT5 of Missile Body X8 through the 26th relay connects the ports-Z of Missile Body X8
DT8；
The fin test points port DT6 of Missile Body X8 meets Missile Body X8 through the 1st normally opened contact KDT27-1 of the 27th relay
The ports VA DT18.
2. adaptive device is converted in the whole bullet emulation testing of a kind of guided munition according to claim 1, it is characterised in that：It is described
Pulse-generating circuit includes phase inverter U11A, phase inverter U11B, counter U12, selector U13, switch module U14, resistance
R90, the first Pulse Width Control relay, port MZ1 and port MGD1；The model of the phase inverter U11A and phase inverter U11B is
74LS04；The model 74LS193 of the counter U12；The model 74LS151 of the selector U13；The switch module
The model DG303AAK of U14；
1st normally opened contact KMZ1-1s of the output end XF1 of function generator through the first Pulse Width Control relay connects described open
Close 4 feet of module U14；
2nd normally opened contact KMZ1-2s of the output end XF2 of function generator through the first Pulse Width Control relay connects described open
Close 3 feet of module U14；
11 feet of the switch module U14 meet the output end XF1D of function generator；
12 feet of the switch module U14 meet the output end XF2D of function generator；
2 feet and 5 feet of the switch module U14 meet the port MZ1 respectively；
1st normally opened contact KDT28-1s of the port MZ1 through the 28th relay connects the fin test points port of Missile Body X8
DT6；
10 feet and 13 feet of the switch module U14 meet the port MGD1 respectively；
2nd normally opened contact KDT28-2s of the port MGD1 through the 28th relay meets the ports the GND DTGD of Missile Body X8；
1 foot of input terminal of the phase inverter U11A meets the port CLK of digital I/O modules；
1 foot of the selector U13 to 4 feet meet the corresponding port D3 ~ D0 of digital I/O modules respectively；The 12 of the selector U13
Foot to 15 feet meet the corresponding port D7 ~ D4 of digital I/O modules respectively；
2 foot of output end of the phase inverter U11A connects 5 feet of the counter U12；
3 feet of the counter U12 connect 11 feet of the selector U13；2 feet of the counter U12 meet the selector U13
10 feet；6 feet of the counter U12 connect 9 feet of the selector U13；
7 feet of the counter U12 connect its 14 foot；
6 feet of the selector U13 connect 3 foot of input terminal of the phase inverter U11B；4 foot of output end of the phase inverter U11B passes through
The resistance R90 meets the port+5V+ of programmable power supply；
4 feet, 11 feet and 16 feet of the counter U12 meet the port+5V+ of programmable power supply respectively；The 15 of the counter U12
Foot, 1 foot, 10 feet, 9 feet and 8 feet are grounded respectively；16 feet of the selector U13 meet the port+5V+ of programmable power supply；The selection
7 feet and 8 feet of device U13 are grounded respectively；
14 feet of the switch module U14 meet the port+15V+ of programmable power supply；8 feet of the switch module U14 connect programmable power supply
Port -15V-.
3. adaptive device is converted in the whole bullet emulation testing of a kind of guided munition according to claim 2, it is characterised in that：
The adapter circuit includes R10-R13 and port DT11A-DT14A；
The resistance R13 is connected between port DT11A and the ports DT11 of Missile Body X8；
The resistance R12 is connected between port DT12A and the ports DT12 of Missile Body X8；
The resistance R11 is connected between port DT13A and the ports DT13 of Missile Body X8；
The resistance R10 is connected between port DT14A and the ports DT14 of Missile Body X8；
The port DT11A-DT14A connects the corresponding port of selecting switch respectively.
4. adaptive device is converted in the whole bullet emulation testing of a kind of guided munition according to claim 3, it is characterised in that：It is described
Conversion control circuit includes buffer U1-5, rp-drive U1-11 and exclusion RP1；The model of the buffer U1-5
74LS07；The model MC1413 of the rp-drive U1-11；
Input terminal 1A ~ 6A of the buffer U1-5 connects the corresponding port of digital I/O modules respectively；The buffer U1-5's is defeated
Outlet 1Y ~ 6Y connects the foot of 6 foot of correspondence input terminal of the rp-drive U1-11 ~ 1 respectively；The power end of the buffer U1-5
VCC meets the port+5V+ of programmable power supply；The ground terminal GND ground connection of the buffer U1-5；The 9 of the rp-drive U1-11
Foot meets the port+24V+ of programmable power supply；8 feet of the rp-drive U1-11 are grounded；
The foot of 1 foot of input terminal of the rp-drive U1-11 ~ 6 connects the not common end respective pin of the exclusion RP1 respectively；Institute
State the port+5V+ of the public termination programmable power supply of exclusion RP1；
The coil KDT25 of 25th relay is connected on 11 foot of output end and programmable power supply of the rp-drive U1-11
Between+the 24V+ of port；
The coil KDT26 of 26th relay is connected on 12 foot of output end of the rp-drive U1-11 and the program-controlled electric
Between the port+24V+ in source；
The coil KDT27 of 27th relay is connected on 13 foot of output end and programmable power supply of the rp-drive U1-11
Between+the 24V+ of port；
The coil KDT28 of 28th relay is connected on 14 foot of output end and programmable power supply of the rp-drive U1-11
Between+the 24V+ of port；
The coil KDT18 of 18th relay is connected on 15 foot of output end and programmable power supply of the rp-drive U1-11
Between+the 24V+ of port；
The coil KMZ1 of the first Pulse Width Control relay be connected on 16 foot of output end of the rp-drive U1-11 with it is program-controlled
Between the port+24V+ of power supply.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610259690.1A CN105954609B (en) | 2016-04-25 | 2016-04-25 | A kind of whole bullet emulation testing conversion adaptive device of guided munition |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610259690.1A CN105954609B (en) | 2016-04-25 | 2016-04-25 | A kind of whole bullet emulation testing conversion adaptive device of guided munition |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN105954609A CN105954609A (en) | 2016-09-21 |
| CN105954609B true CN105954609B (en) | 2018-07-27 |
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| CN201610259690.1A Expired - Fee Related CN105954609B (en) | 2016-04-25 | 2016-04-25 | A kind of whole bullet emulation testing conversion adaptive device of guided munition |
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Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4996520A (en) * | 1988-06-17 | 1991-02-26 | Williams Instruments, Inc. | Overvoltage detection test apparatus for military aircraft weapons systems |
| CN102353865A (en) * | 2011-09-05 | 2012-02-15 | 西安石油大学 | Automatic testing device and method universally used for multiple bus processor modules |
| CN205620714U (en) * | 2016-04-25 | 2016-10-05 | 中国人民解放军63908部队 | Whole emulation test conversion adapter device that plays of gun -launched missile |
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Patent Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4996520A (en) * | 1988-06-17 | 1991-02-26 | Williams Instruments, Inc. | Overvoltage detection test apparatus for military aircraft weapons systems |
| CN102353865A (en) * | 2011-09-05 | 2012-02-15 | 西安石油大学 | Automatic testing device and method universally used for multiple bus processor modules |
| CN205620714U (en) * | 2016-04-25 | 2016-10-05 | 中国人民解放军63908部队 | Whole emulation test conversion adapter device that plays of gun -launched missile |
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| CN105954609A (en) | 2016-09-21 |
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