CN204331025U - A kind of radar antenna control system debugging tool - Google Patents
A kind of radar antenna control system debugging tool Download PDFInfo
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- CN204331025U CN204331025U CN201420826189.5U CN201420826189U CN204331025U CN 204331025 U CN204331025 U CN 204331025U CN 201420826189 U CN201420826189 U CN 201420826189U CN 204331025 U CN204331025 U CN 204331025U
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Abstract
The utility model relates to a kind of radar antenna control system debugging tool, by the power supply positive-negative input end sub-connection of the positive-negative output end of 24V direct supply and debugging tool, M tested drive plate is connected with the tested drive plate socket of debugging tool, M tested control panel is connected with the tested control panel socket of debugging tool, M the state cable of tested antenna is connected with the tested antenna condition cable socket of debugging tool, M tested antenna command word control cables is connected with the tested antenna command word control cables socket of debugging tool; Make to be realized exchanges data by tested antenna, tested drive plate, tested control panel and test computer.
Description
Technical field
The invention belongs to field of radar, be specifically related to a kind of radar antenna control system debugging tool.
Background technology
But, in the past in radar antenna control system debug process, owing to there is no special debugging tool, " control coding plate ", " drive plate " simply can only be supported by several pillar, and cable is messy, causes Commissioning field chaotic, and what once can only complete a set of product delivers for a check work, and efficiency is lower.
Summary of the invention
The technical matters solved
In order to avoid the deficiencies in the prior art part, the present invention proposes a kind of radar antenna control system debugging tool, " control coding plate ", " drive plate " is fast connected by cabinet, avoid dangerous operation, solve product and support problem, and there is raising debugging efficiency, easy to use, adjust flexible, integrated level advantages of higher.
Technical scheme
A kind of radar antenna control system debugging tool, is characterized in that comprising P.e.c. mother matrix, the socket 2 of a M tested drive plate of connection, M connects socket 3, the socket 2.1 of a M tested antenna condition cable of connection, the socket 3.1 of a M tested antenna command word control cables of connection of tested control panel and M aligns, negative supply socket 1; M the socket 2 connecting tested drive plate is positioned on the panel of the both sides of P.e.c. mother matrix with M the socket 2.1 being connected tested antenna condition cable, is connected one to one by bonding wire; M the socket 3 connecting tested control panel is positioned on the panel of the both sides of P.e.c. mother matrix with M the socket 3.1 being connected tested antenna command word control cables, is connected one to one by bonding wire; M aligns, the one side of negative supply socket 1 is the jack connecting power supply, and opposite side is connected on the power connector of socket 2 of tested drive plate with M respectively by power bus.
The socket 2 of the tested drive plate of described connection is pin type socket with the socket 3 being connected tested control panel.
The socket 3.1 of described connection tested antenna command word control cables is poroid socket with the poroid socket 3.1 being connected tested antenna command word control cables.
Described P.e.c. mother matrix is a face of frame-type machine cage.
Described M equals four.
Beneficial effect
A kind of radar antenna control system debugging tool that the present invention proposes, by the power supply positive-negative input end sub-connection of the positive-negative output end of 24V direct supply and debugging tool, M tested drive plate is connected with the tested drive plate socket of debugging tool, M tested control panel is connected with the tested control panel socket of debugging tool, M the state cable of tested antenna is connected with the tested antenna condition cable socket of debugging tool, M tested antenna command word control cables is connected with the tested antenna command word control cables socket of debugging tool; Tested antenna, tested drive plate, tested control panel and test computer is made to realize exchanges data.
Beneficial effect of the present invention:
The first, certain the model radar antenna control system frock proposed in the present invention can be assigned many " control coding plate ", " drive plate ", can complete independently certain the model radar antenna control system test of many covers.During test, every cover system can verify project by complete independently, and do not disturb each other, debugging efficiency improves three times.
The second, certain the model radar antenna control system frock proposed in the present invention, due to " control coding plate ", " drive plate " assigns in frock, and cable is placed in order, and Commissioning field environment improves greatly.
3rd, certain the model radar antenna control system frock proposed in the present invention can facilitate " control coding plate ", and the plug of " drive plate ", avoids the damage of product connector.
4th, certain the model radar antenna control system frock proposed in the present invention, based on frame-type machine cage, is conducive to " control coding plate ", the heat radiation of " drive plate ", and effectively can prevents the short circuit problem of product.
5th, certain the model radar antenna control system frock proposed in the present invention can complete the debugging verifying work of this antenna control system reliably.
Accompanying drawing explanation
Fig. 1: the panel layout of tested drive plate and tested control panel faced by debugging tool of the present invention;
1-power input terminal; 2-connects the socket of tested drive plate; 3-connects the socket of tested control system;
Fig. 2: in the face of the panel layout of tested antenna in debugging tool of the present invention;
1.1-is welded on the power input terminal on mother matrix; 2.1-connects the socket of tested antenna condition cable, and 3.1-connects the socket of tested antenna command word control cables.
Embodiment
Now in conjunction with the embodiments, the invention will be further described for accompanying drawing:
Frock part: as shown in accompanying drawing 1 accompanying drawing 2, frock part comprises frame-type machine cage, power supply interface, private bus motherboard three part.The design of frame-type machine cage conveniently can plug " control coding plate " and " drive plate ", and is conducive to " control coding plate ", the heat radiation of " drive plate ", effectively can prevent the short circuit problem of product.Power supply interface adopts umbilical connector, double plug cable is adopted during power supply, power supply is facilitated to be connected with debugging tool, four power interfaces adopt double-end cable to be connected with admittedly big SPD3606 power output end, by the service cable connecting interface XS01 at bus mother board back, XS02, XS03 and XS04 provide 24V direct supply for frock.The present invention utilizes frame enclosure that " control coding plate " is connected with private bus motherboard with " drive plate ", thus carry out data processing at special mother intralamellar part, motherboard inside comprises internal bus interface (XS1, XS2, XS7, XS8, XS13, XS14, XS19, XS20 and XS5, XS11, XS17, XS23), wherein XS1, XS2, XS7, XS8, XS13, XS14 and XS19, XS20 insert four cover control coding plates respectively, and XS5, XS11, XS17 and XS23 are the special socket of four cover drive plates respectively, special mother backboard portion comprises external telecom-munications cable interface (XS3, XS6, XS9, XS12, XS15, XS18, XS21, XS24, and XS4, XS10, XS16, XS22), external telecom-munications cable is patched during work, with external computer system, antenna mount system carries out exchanges data, wherein XS3 and XS6, XS9 and XS12, XS15 and XS18, XS21 and XS24, drive plate and the exchanges data between control coding plate and outer computer is completed by special self-control cable, XS4, XS10, XS16 and XS22 is used for connection 4 independently antenna base, complete the data processing of computer control system and antenna base.Control coding plate is via in internal bus interface XS1, XS2 insertion machine cage, be connected with external telecom-munications cable interface XS3 by motherboard winding displacement, and external telecom-munications cable interface XS3 and XS6 connects with special self-control cable, the connection with drive plate XS5 is completed by motherboard winding displacement, like this, control coding plate and drive plate just complete internal data processing capacity, other internal bus interface also can be connected with external telecom-munications cable interface by special self-control cable equally, completes the internal data processing capacity of other three cover control coding plates and drive plate.
Computing machine part: computer system is by serial communication via " the control coding plate " on motherboard, and " drive plate " calculation process sends control command to antenna pedestal, receives the state sampled data from antenna pedestal simultaneously.
The radar antenna control system debugging tool adopting the present embodiment to provide carries out radar antenna control system adjustment method:
Power unit: this frock adopts independent 24V DC power supply, adopt solid big SPD3606 power output end by self-control double-end cable respectively with the four-way power supply cable connection port of debugging tool: the first power supply, second source, 3rd power supply is connected with the 4th power supply, so can the change of reflecting voltage real-time on digital power SPD3606 and electric current, convenient debugging.
M tested drive plate is connected with the tested drive plate socket of debugging tool, M tested control panel is connected with the tested control panel socket 3 of debugging tool, M the state cable of tested antenna is connected with the tested antenna condition cable socket 2.1 of debugging tool, M tested antenna command word control cables is connected with the tested antenna command word control cables socket 3.1 of debugging tool; Tested antenna, tested drive plate, tested control panel and test computer is made to realize exchanges data.
Claims (5)
1. a radar antenna control system debugging tool, is characterized in that comprising P.e.c. mother matrix, the socket (2) of a M tested drive plate of connection, M connects socket (3), the socket (2.1) of a M tested antenna condition cable of connection, the socket (3.1) of a M tested antenna command word control cables of connection of tested control panel and M aligns, negative supply socket (1); M the socket (2) connecting tested drive plate is positioned on the panel of the both sides of P.e.c. mother matrix with M the socket (2.1) being connected tested antenna condition cable, is connected one to one by bonding wire; M the socket (3) connecting tested control panel is positioned on the panel of the both sides of P.e.c. mother matrix with M the socket (3.1) being connected tested antenna command word control cables, is connected one to one by bonding wire; M aligns, the one side of negative supply socket (1) is the jack connecting power supply, and opposite side is connected on the power connector of socket (2) of tested drive plate with M respectively by power bus.
2. radar antenna control system debugging tool according to claim 1, is characterized in that: the socket (2) of the tested drive plate of described connection is pin type socket with the socket (3) being connected tested control panel.
3. radar antenna control system debugging tool according to claim 1, is characterized in that: the socket (3.1) of described connection tested antenna command word control cables is poroid socket with the poroid socket (3.1) being connected tested antenna command word control cables.
4. radar antenna control system debugging tool according to claim 1, is characterized in that: described P.e.c. mother matrix is a face of frame-type machine cage.
5. radar antenna control system debugging tool according to claim 1, is characterized in that: described M equals four.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420826189.5U CN204331025U (en) | 2014-12-23 | 2014-12-23 | A kind of radar antenna control system debugging tool |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420826189.5U CN204331025U (en) | 2014-12-23 | 2014-12-23 | A kind of radar antenna control system debugging tool |
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| Publication Number | Publication Date |
|---|---|
| CN204331025U true CN204331025U (en) | 2015-05-13 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201420826189.5U Active CN204331025U (en) | 2014-12-23 | 2014-12-23 | A kind of radar antenna control system debugging tool |
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| Country | Link |
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| CN (1) | CN204331025U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104614712B (en) * | 2014-12-23 | 2017-02-22 | 西安电子工程研究所 | Radar antenna control system debugging tool and debugging method |
-
2014
- 2014-12-23 CN CN201420826189.5U patent/CN204331025U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104614712B (en) * | 2014-12-23 | 2017-02-22 | 西安电子工程研究所 | Radar antenna control system debugging tool and debugging method |
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