CN205787882U - A kind of antitank missile launching guidance opening machine system test device - Google Patents
A kind of antitank missile launching guidance opening machine system test device Download PDFInfo
- Publication number
- CN205787882U CN205787882U CN201620497008.8U CN201620497008U CN205787882U CN 205787882 U CN205787882 U CN 205787882U CN 201620497008 U CN201620497008 U CN 201620497008U CN 205787882 U CN205787882 U CN 205787882U
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- circuit
- missile launching
- self
- antitank missile
- machine system
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- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
Abstract
The utility model discloses a kind of antitank missile launching guidance opening machine system test device, including test board and usb data capture card, test board connects usb data capture card;Test board includes power circuit, digital quantity circuit, analog quantity circuit, signal source circuit, self-checking circuit and infrared light source device, and power circuit connects digital quantity circuit, analog quantity circuit, signal source circuit, self-checking circuit and infrared light source device respectively.Utilize this utility model, can realize detecting the technical parameter of antitank missile launching guidance system.
Description
Technical field
This utility model relates to equipping detection technique field.
Background technology
Antitank missile launching guidance system is used for laying wound packages guided missile, searches for and capture target, launch a guided missile and guide guided missile.My the tactics antitank missile kind of army's equipment is more at present, the missile equipment of every kind of model is equipped with detecting accordingly equipment, but quite a few detection reliability of equipment, maintainability and automaticity etc. are poor, this causes very big inconvenience to the daily management of equipment and use, makes the supportability in wartime seriously be restricted.
Utility model content
The technical problems to be solved in the utility model is for above-mentioned the deficiencies in the prior art, it is provided that a kind of antitank missile launching guidance opening machine system test device, utilizes this device, can realize detecting the technical parameter of antitank missile launching guidance system.
For solving above-mentioned technical problem, technical solution adopted in the utility model is: a kind of antitank missile launching guidance opening machine system test device, and including test board and usb data capture card, test board connects usb data capture card;Test board includes power circuit, digital quantity circuit, analog quantity circuit, signal source circuit, self-checking circuit and infrared light source device, and power circuit connects digital quantity circuit, analog quantity circuit, signal source circuit, self-checking circuit and infrared light source device respectively.
Preferably, also including analog switching circuit, the outfan of described digital quantity circuit connects the I/O port of described usb data capture card, and the outfan of described analog quantity circuit connects the A/D port of described usb data capture card by described analog switching circuit.
Preferably, power circuit output ± 20V, ± 12V, the regulated power supply of+5V.
Preferably, the digital signal that signal shaping is Transistor-Transistor Logic level in the antitank missile launching guidance system that digital quantity circuit will detect.
Preferably, signal source circuit provides analog signals and the on-off model of test antitank missile launching guidance system.
Preferably, self-checking circuit includes the self-checking circuit of analog quantity channel, the self-checking circuit of digital quantity passage, the self-checking circuit of supply voltage.
Preferably, usb data capture card uses USB2008 capture card.
Use and have the beneficial effects that produced by technique scheme: this utility model provides a kind of antitank missile launching guidance opening machine system test device, utilize this device, the technical parameter of detection antitank missile launching guidance system can be realized, this test device integration degree is high, volume is little, faults itself is pointed out automatically, maintains easily and repairs.
Accompanying drawing explanation
Fig. 1 is structure and the work process schematic diagram of one embodiment of this utility model;
Fig. 2 is that TT & C software module forms schematic diagram.
Detailed description of the invention
With detailed description of the invention, this utility model is described in further detail below in conjunction with the accompanying drawings, but protection domain of the present utility model is not limited to the following stated.
As it is shown in figure 1, be an embodiment of this utility model a kind of antitank missile launching guidance opening machine system test device, including test board and usb data capture card, test board connects usb data capture card;Test board includes power circuit, digital quantity circuit, analog quantity circuit, signal source circuit, self-checking circuit and infrared light source device, and power circuit connects digital quantity circuit, analog quantity circuit, signal source circuit, self-checking circuit and infrared light source device respectively.
Power circuit output ± 12V, the regulated power supply of+5V, for test board;The regulated power supply of output ± 20V, for measurand.
The digital signal that signal shaping is Transistor-Transistor Logic level in the antitank missile launching guidance system that digital quantity circuit will detect, output is to usb data capture card I/O port.
Analog quantity circuit: process each input voltage within usb data capture card A/D conversion range, send into usb data capture card A/D port by analog switching circuit and measure.
Signal source circuit provides analog signals and the on-off model of test antitank missile launching guidance system.
Self-checking circuit includes the self-checking circuit of the analog quantity channel of this test device, the self-checking circuit of digital quantity passage, the self-checking circuit of supply voltage.
Infrared light source device: the infrared signal source of simulated target, for the performance parameter test of clinometer circuit.
Usb data capture card uses USB interface data collecting card USB2008, completes Control & data acquisition function.The features such as SB2008 card is the data collecting card that usb bus is compatible, can access computer through USB cable, have volume little, plug and play, its key technical indexes is as follows:
(1) A/D part: analog voltage input range: ± 10V;A/D conversion resolution: 12Bit, 32K word FIFO memory ensures the integrity of AD data;16 both-end analogue signal inputs.
(2) D/A part: analog voltage output area: ± 5V;D/A conversion resolution: 12BIT.
(3) I/O part: 16 way switch amount inputs;16 way switch amount outputs.
TT&C software in this device is as shown in Figure 2.There is main menu after starting in TT&C software.After selecting respective menu project, mastery routine then starts corresponding test program, self-check program, data administrator etc., in corresponding self-inspection with test program, carries out self-inspection and test according to screen prompt.After completing corresponding task, can preserve or print data file.
Use process: the test board in this test device is able to receive that the control instruction that notebook computer, usb data capture card send, to antitank missile launching guidance system with excitation, and the signal of antitank missile launching guidance system output is converted into the usb data receptible analog or digital signal of capture card, it is delivered to usb data capture card, notebook computer exports after processing and preserve test result.
After using technique scheme, it is provided that a kind of antitank missile launching guidance opening machine system test device, utilize this device, can realize the technical parameter of detection antitank missile launching guidance system, this test device integration degree is high, and volume is little, faults itself is pointed out automatically, maintains easily and repairs.
Claims (7)
1. an antitank missile launching guidance opening machine system test device, it is characterised in that: including test board and usb data capture card, described test board connects described usb data capture card;Described test board includes power circuit, digital quantity circuit, analog quantity circuit, signal source circuit, self-checking circuit and infrared light source device, and described power circuit connects digital quantity circuit, analog quantity circuit, signal source circuit, self-checking circuit and infrared light source device respectively.
A kind of antitank missile launching guidance opening machine system test device the most according to claim 1, characterized by further comprising analog switching circuit, the outfan of described digital quantity circuit connects the I/O port of described usb data capture card, and the outfan of described analog quantity circuit connects the A/D port of described usb data capture card by described analog switching circuit.
A kind of antitank missile launching guidance opening machine system test device the most according to claim 1, it is characterised in that described power circuit output ± 20V, ± 12V, the regulated power supply of+5V.
A kind of antitank missile launching guidance opening machine system test device the most according to claim 1, it is characterised in that the digital signal that signal shaping is Transistor-Transistor Logic level in the antitank missile launching guidance system that described digital quantity circuit will detect.
A kind of antitank missile launching guidance opening machine system test device the most according to claim 1, it is characterised in that described signal source circuit provides analog signals and the on-off model of test antitank missile launching guidance system.
A kind of antitank missile launching guidance opening machine system test device the most according to claim 1, it is characterised in that described self-checking circuit includes the self-checking circuit of analog quantity channel, the self-checking circuit of digital quantity passage, the self-checking circuit of supply voltage.
A kind of antitank missile launching guidance opening machine system test device the most according to claim 1, it is characterised in that described usb data capture card uses USB2008 capture card.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
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CN201620497008.8U CN205787882U (en) | 2016-05-27 | 2016-05-27 | A kind of antitank missile launching guidance opening machine system test device |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
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CN201620497008.8U CN205787882U (en) | 2016-05-27 | 2016-05-27 | A kind of antitank missile launching guidance opening machine system test device |
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CN205787882U true CN205787882U (en) | 2016-12-07 |
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CN201620497008.8U Expired - Fee Related CN205787882U (en) | 2016-05-27 | 2016-05-27 | A kind of antitank missile launching guidance opening machine system test device |
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Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN108415264A (en) * | 2018-01-15 | 2018-08-17 | 上海机电工程研究所 | Integrated simulation equipment for guided missile with flying experiment |
CN109542078A (en) * | 2018-09-19 | 2019-03-29 | 北京旋极信息技术股份有限公司 | Detection method, device, computer storage medium and the terminal of launch control unit |
CN109682268A (en) * | 2019-03-15 | 2019-04-26 | 江南机电设计研究所 | A kind of micro missile test device |
-
2016
- 2016-05-27 CN CN201620497008.8U patent/CN205787882U/en not_active Expired - Fee Related
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN108415264A (en) * | 2018-01-15 | 2018-08-17 | 上海机电工程研究所 | Integrated simulation equipment for guided missile with flying experiment |
CN109542078A (en) * | 2018-09-19 | 2019-03-29 | 北京旋极信息技术股份有限公司 | Detection method, device, computer storage medium and the terminal of launch control unit |
CN109682268A (en) * | 2019-03-15 | 2019-04-26 | 江南机电设计研究所 | A kind of micro missile test device |
CN109682268B (en) * | 2019-03-15 | 2021-04-06 | 江南机电设计研究所 | Miniature guided missile testing arrangement |
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C14 | Grant of patent or utility model | ||
GR01 | Patent grant | ||
CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20161207 Termination date: 20200527 |
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CF01 | Termination of patent right due to non-payment of annual fee |