CN201892836U - GPS (global position system) satellite synchronous clock - Google Patents
GPS (global position system) satellite synchronous clock Download PDFInfo
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- CN201892836U CN201892836U CN 201020643719 CN201020643719U CN201892836U CN 201892836 U CN201892836 U CN 201892836U CN 201020643719 CN201020643719 CN 201020643719 CN 201020643719 U CN201020643719 U CN 201020643719U CN 201892836 U CN201892836 U CN 201892836U
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Abstract
The utility model discloses a GPS satellite synchronous clock, which comprises a CPU (central processing unit) controlling and data processing module, a GPS signal receiving module, a relay output module, a display module, an indicator lamp clock module and a communication module, wherein the GPS signal receiving module is connected with the signal input terminal of the CPU controlling and data processing module; the signal output terminal of the CPU controlling and data processing module is connected with the relay output module; and the CPU controlling and data processing module is bi-directionally and electrically connected with the display module, the indicator lamp clock module and the communication module respectively. The GPS satellite synchronous clock disclosed by the utility model takes a satellite space-borne atomic clock as a time standard, so that accumulated error is avoided, and the precision is greatly improved.
Description
Technical field
The utility model relates to a kind of device of indicating the current standard time, specifically is a kind of gps satellite synchronous clock.
Background technology
The electronic clock of band RTC chip in used time display apparatus all adopts at present, this device does not have the gps satellite receiving function, is not with synchronizing pulse output, can not offer outside synchronous base, can only be as the display device of a current time.Simultaneously, because existing time display apparatus does not have synchronizing function, make that the precision of time showing is not high.
Summary of the invention
At the defective that above-mentioned prior art exists, the purpose of this utility model aims to provide a kind of gps satellite synchronous clock, adopts satellite carried atomic clock as time standard, and no cumulative errors makes precision improve greatly.
The technical scheme of taking of the present utility model is that a kind of gps satellite synchronous clock comprises CPU control and data processing module, gps signal receiver module, relay output module, display module, pilot lamp clock module and communication module; Described gps signal receiver module inserts the signal input part of described CPU control and data processing module; The signal output part cut-in relay output module of described CPU control and data processing module; Described CPU control and data processing module are respectively with display module, pilot lamp clock module with communication module is two-way is electrically connected.
According to embodiment, as preferred version, described CPU control and data processing module select for use arithmetic speed to reach the technical grade microprocessor of 100MIPS, and are built-in with temperature sensor in CPU control and data processing module.
Gps satellite synchronous clock band four road RS485 communication interfaces described in the utility model, time data of per second output; Four tunnel pulse per second (PPS)s output, the one tunnel divides pulse output, pulse in a tunnel hour output.Gps satellite synchronous clock described in the utility model adopts the high-quality GPS receiver of 12 passages, has the also ability of 12 satellites of line trace, in case initialization is finished, also can realize the time service function even lock a satellite, so this gps satellite synchronous clock has powerful antijamming capability.This gps satellite synchronous clock meets " static protective relaying device and automatic safety device general technical specifications " and " standardization center, middle Electricity Federation clock synchronization system technical manual 051222 ".The software and hardware of this gps satellite synchronous clock adopts multinomial interference protection measure.Described gps satellite synchronous clock can be with the position longitude of receiver and latitude information and temporal information by being sent to host computer on the communication port.
Gps satellite synchronous clock described in the utility model does not have cumulative errors, and precision improves greatly;
Field in the time of can being widely used in electric power, civil aviaton, railway, traffic scheduling, Digital Television, real-time Communication for Power network system etc. and needing time service and school.
Description of drawings:
Below in conjunction with drawings and Examples the utility model is further specified.
Fig. 1 is the structural representation of the described gps satellite synchronous clock of embodiment;
Fig. 2 is the panel displayed map of the described gps satellite synchronous clock of embodiment;
Fig. 3 is the tail wiring terminal distribution plan of the described gps satellite synchronous clock of embodiment.
In above-mentioned accompanying drawing:
1-CPU control and data processing module; The 2-GPS signal receiving module;
The 3-relay output module; The 4-display module; 5-pilot lamp clock module;
The 6-communication module.
Embodiment
Embodiment one:
As shown in Figure 1, present embodiment provides a kind of gps satellite synchronous clock, comprises CPU control and data processing module 1, gps signal receiver module 2, relay output module 3, display module 4, pilot lamp clock module 5 and communication module 6; Described gps signal receiver module 2 inserts the signal input part of described CPU control and data processing module 1; The signal output part cut-in relay output module 3 of described CPU control and data processing module 1; Described CPU control and data processing module 1 respectively with display module 4, pilot lamp clock module 5, communication module 6 two-way electrical connections.
The CPU control of present embodiment and data processing module 1 select for use arithmetic speed to reach as high as the technical grade microprocessor of 100MIPS, are with 128KFLASH, 32KRAM, SPI, I2C, 12 DAC passages, 2 tunnel communications or CAN interfaces; In CPU control and data processing module, be built-in with temperature sensor, can pass through computed in software, revise and draw the device working temperature.
The gps signal receiver module 2 of present embodiment: with the satnav time signal that receives, handle, adopt the universal serial bus mode to send into cpu chip through associated analog and digital circuit.
The relay output module 3 of present embodiment: adopt cpu chip I/O mouth directly to carry out the output of optical relay control signal.
The communication module 6 of present embodiment: adopt four road RS485 buses, 4 tunnel pulse per second (PPS)s, a tunnel to divide pulse, pulse in a tunnel hour output.Described RS485 bus is a prior art.Its RS485 communication realizes communication by SN65HVD17 after the light lotus root isolates; 4 tunnel pulse per second (PPS)s, one tunnel divide pulse, pulse in a tunnel hour, adopt the light lotus root to isolate directly output of back.
The pilot lamp of present embodiment and clock module 5: by two chips of SN74HC164, adopt the universal serial bus mode, CPU controls pilot lamp Push And Release state.
The display module 4 of present embodiment: adopt 6 red charactron display modules, by bus output CPU video data.
Shown in Fig. 2,3, present embodiment adopts 1U standard rack formula cabinet, and appearance looks elegant is generous, adopts wide region AC power or direct supply, can be fit to the more work scene.
The front of described gps satellite synchronous clock adopts red charactron to show current zone time; Have hour, minute, the number demonstration in second and running indicator, satellite synchro light.Described gps satellite synchronous clock adopts the serial communication port communications, and there is the pulse output interface of 2 tunnel 232 communication interfaces, 2 tunnel 485 communication interfaces and a time data of output in four tunnel one seconds at the back side.15KV ESD protection is isolated and contained to total interface in the described gps satellite synchronous clock through photoelectricity, the protection of the antisurge of the anti-thunderbolt of built-in 600W simultaneously.
When the described gps satellite synchronous clock of present embodiment can show and export any time zone of Beijing time, Coordinated Universal Time(UTC) (UTC) and other, minute, second and Gregorian calendar date year, month, day etc.Adopt LED display message content, indicate power supply with synchronous respectively with two red lights simultaneously, with four green lights indicate respectively satellite synchronizing clock operation, pulse per second (PPS), branch pulse, the time pulse information.Adopt idle contact and TTL level mode to export pulse per second (PPS) (1PPS), divide pulse (1PPM) pulse (1PPH) signal in time, realize precision high synchronously to the time.
Claims (2)
1. a gps satellite synchronous clock is characterized in that, comprises CPU control and data processing module (1), gps signal receiver module (2), relay output module (3), display module (4), pilot lamp clock module (5) and communication module (6); Described gps signal receiver module (2) inserts the signal input part of described CPU control and data processing module (1); The signal output part cut-in relay output module (3) of described CPU control and data processing module (1); Described CPU control and data processing module (1) respectively with display module (4), pilot lamp clock module (5) and two-way electrical connection of communication module (6).
2. according to the described gps satellite synchronous clock of claim 1, it is characterized in that described CPU control and data processing module (1) select for use arithmetic speed to reach the technical grade microprocessor of 100MIPS, and are built-in with temperature sensor in CPU control and data processing module.
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CN 201020643719 CN201892836U (en) | 2010-12-07 | 2010-12-07 | GPS (global position system) satellite synchronous clock |
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CN 201020643719 CN201892836U (en) | 2010-12-07 | 2010-12-07 | GPS (global position system) satellite synchronous clock |
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Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN102830614A (en) * | 2012-09-05 | 2012-12-19 | 飞亚达(集团)股份有限公司 | Civil aviation airborne cockpit clock |
CN103197535A (en) * | 2013-04-12 | 2013-07-10 | 北京空间飞行器总体设计部 | Method for satellite-ground timing with oscilloscope |
CN106163026A (en) * | 2015-03-25 | 2016-11-23 | 福建吉星智能科技股份有限公司 | Quick control implementation method is dodged in the synchronization of a kind of modulator |
CN110933384A (en) * | 2019-12-17 | 2020-03-27 | 深圳爱克莱特科技股份有限公司 | Offline play synchronous control device and control method of LED play system |
CN111240183A (en) * | 2020-03-17 | 2020-06-05 | 长沙天穹电子科技有限公司 | Testing device for satellite synchronous clock |
-
2010
- 2010-12-07 CN CN 201020643719 patent/CN201892836U/en not_active Expired - Lifetime
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN102830614A (en) * | 2012-09-05 | 2012-12-19 | 飞亚达(集团)股份有限公司 | Civil aviation airborne cockpit clock |
CN103197535A (en) * | 2013-04-12 | 2013-07-10 | 北京空间飞行器总体设计部 | Method for satellite-ground timing with oscilloscope |
CN103197535B (en) * | 2013-04-12 | 2015-04-15 | 北京空间飞行器总体设计部 | Method for satellite-ground timing with oscilloscope |
CN106163026A (en) * | 2015-03-25 | 2016-11-23 | 福建吉星智能科技股份有限公司 | Quick control implementation method is dodged in the synchronization of a kind of modulator |
CN106163026B (en) * | 2015-03-25 | 2018-11-20 | 福建吉星智能科技股份有限公司 | A kind of synchronous quick control method of sudden strain of a muscle of modulator |
CN110933384A (en) * | 2019-12-17 | 2020-03-27 | 深圳爱克莱特科技股份有限公司 | Offline play synchronous control device and control method of LED play system |
CN111240183A (en) * | 2020-03-17 | 2020-06-05 | 长沙天穹电子科技有限公司 | Testing device for satellite synchronous clock |
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Legal Events
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C14 | Grant of patent or utility model | ||
GR01 | Patent grant | ||
C41 | Transfer of patent application or patent right or utility model | ||
TR01 | Transfer of patent right |
Effective date of registration: 20111215 Address after: 410205 Hunan province Changsha high tech Zone Lusong Lu Valley Road Patentee after: HNAC Technology Co., Ltd. Address before: High tech Zone Lusong Lu Valley Road Changsha Changsha city of 410205 cities in Hunan Province Patentee before: Hunan Huazi Technology Co., Ltd. |
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CX01 | Expiry of patent term | ||
CX01 | Expiry of patent term |
Granted publication date: 20110706 |