CN101567129A - Solar energy spike synchronization control method - Google Patents
Solar energy spike synchronization control method Download PDFInfo
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- CN101567129A CN101567129A CNA2009100985905A CN200910098590A CN101567129A CN 101567129 A CN101567129 A CN 101567129A CN A2009100985905 A CNA2009100985905 A CN A2009100985905A CN 200910098590 A CN200910098590 A CN 200910098590A CN 101567129 A CN101567129 A CN 101567129A
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- H—ELECTRICITY
- H05—ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
- H05B—ELECTRIC HEATING; ELECTRIC LIGHT SOURCES NOT OTHERWISE PROVIDED FOR; CIRCUIT ARRANGEMENTS FOR ELECTRIC LIGHT SOURCES, IN GENERAL
- H05B47/00—Circuit arrangements for operating light sources in general, i.e. where the type of light source is not relevant
- H05B47/10—Controlling the light source
- H05B47/16—Controlling the light source by timing means
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- H—ELECTRICITY
- H05—ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
- H05B—ELECTRIC HEATING; ELECTRIC LIGHT SOURCES NOT OTHERWISE PROVIDED FOR; CIRCUIT ARRANGEMENTS FOR ELECTRIC LIGHT SOURCES, IN GENERAL
- H05B47/00—Circuit arrangements for operating light sources in general, i.e. where the type of light source is not relevant
- H05B47/10—Controlling the light source
- H05B47/165—Controlling the light source following a pre-assigned programmed sequence; Logic control [LC]
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02B—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO BUILDINGS, e.g. HOUSING, HOUSE APPLIANCES OR RELATED END-USER APPLICATIONS
- Y02B20/00—Energy efficient lighting technologies, e.g. halogen lamps or gas discharge lamps
- Y02B20/40—Control techniques providing energy savings, e.g. smart controller or presence detection
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- Road Signs Or Road Markings (AREA)
- Electric Clocks (AREA)
Abstract
The invention discloses a solar energy spike synchronization control method that uses the time service function of a geosynchronous positioning satellite, the solar energy synchronization spikes and the same time source to conduct synchronous working control on the solar energy synchronization spikes installed discretely. The solar energy synchronization spike comprises a shell, a solar cell, an accumulator battery, a charge-discharge on-off control circuit, a miniature satellite receiving antenna, a satellite receiving module, a microprocessor and an electroluminescent device. After receiving a time service signal of the geosynchronous positioning satellite, the miniature satellite receiving antenna analyzes and extracts time information and second synchronizing information through the satellite receiving module. After receiving a second synchronizing signal offered by the satellite receiving module, the microprocessor controls the synchronous turn-on and turn-off of the electroluminescent device according to preset flicker frequency and flicker duty ratio. Using synchronizing time to conduct synchronous working control on the solar energy spikes, the control method is not limited by factors such as the length and trend of roads, and is simple and convenient in implementation and reliable in control.
Description
Technical field
The present invention relates to a kind of railway spike control method, particularly a kind of solar energy spike synchronization control method, the graticule that is mainly used in the road traffic is strengthened demonstration night, uses the solar powered railway spike synchronous working of satellite time service synchro control.
Background technology
Solar energy spike is mainly used in the Dangerous Area of traffic hazard pilositys such as highway graticule, Lin Ya highway section graticule, as night trend of road strengthen indication, and the application that beautifies etc. the field in recent years at urban road night.Above-mentioned application requirements is realized synchronous working along the discrete solar energy spike of installing of roadmarking, under asynchronous duty, can produce the sensation of " dazzling ", influences the safety of road traffic.Discrete solar energy spike synchronous working of installing, the technical scheme that prior art adopts is that a concentrated Controlling Source is set, and takes controlled in wireless again or has the mode of line traffic control that the discrete solar energy spike in the control zone is carried out centralized control.The applicant first to file CN201095727 " a kind of digital radio control raised solar-energy road sign ", a kind of controlled in wireless solar energy spike is disclosed, this railway spike mainly comprises housing, display window, light emitting diode and wireless control system.This application uses the controlled in wireless mode to realize the solar energy spike synchronous working that disperses, yet the mode of this controlled in wireless is the same with wired control mode, the restriction of controlled distance, can only realize that the short distance solar energy spike in the zonule reaches numerical control work synchronously, adapt to the morning and evening track in the sensing change of change of the track of each time period traffic direction and crossing changeable driveway etc., the pattern of controlled in wireless solar energy spike synchronous working is the same with wired control mode, can't be applied to length and strengthen, and also will be limited by the implementation cost of synchro control and the operation cost of control and management apart from graticule.
Summary of the invention
Technical matters to be solved by this invention is, overcomes the defective that prior art exists, and a kind of restrictions such as link length, trend that are not subjected to are provided, implement simple, the solar energy spike synchronization control method that reliability is high.
The present invention addresses the above problem the technical scheme that is adopted: this solar energy spike synchronization control method, be characterized in: the time service function of utilizing earth synchronized positioning satellite, adopt the synchronous railway spike of sun power, use same time source that the discrete synchronous railway spike of installing of sun power is carried out synchronous working control;
The synchronous railway spike of described sun power comprises housing, solar cell, battery pack and discharges and recharges and open and close control circuit, micro-satellite receiving antenna, satellite receiver module, microprocessor and electroluminescence device; Described solar cell is to battery charging, and with charge-discharge control circuit with open and close control circuit and be connected, the micro-satellite receiving antenna connects the satellite receiver module, the satellite receiver module connects microprocessor, output end of microprocessor is connected with electroluminescence device, and electroluminescence device is by microprocessor driven and control;
After described micro-satellite receiving antenna receives the time signal of earth synchronized positioning satellite, temporal information and second synchronizing information are resolved and extracted to receiver module via satellite, after microprocessor receives that the satellite receiver module provides second synchronizing signal, lighting and closing according to the flicker frequency that presets, flicker dutycycle control electroluminescence device, the synchronous railway spike of the discrete sun power of installing uses time configuration and the start-up time that stems from the identical accurate time service of satellite, carries out the mode of operation of high level of synchronization.Use lock in time that solar energy spike is carried out synchronous working control, enforcement is simple, convenient, and control is reliable.
Solar energy spike synchronization control method of the present invention, described microprocessor distributes by the difference to the time service scheme, obtains different flicker frequency and the dutycycles of the synchronous railway spike of sun power.
Solar energy spike synchronization control method of the present invention, the time service source of the earth synchronized positioning satellite that the satellite receiver module of the synchronous railway spike of described sun power and solar energy spike synchronization control method are selected is complementary.
Solar energy spike synchronization control method of the present invention, the microprocessor of the synchronous railway spike of described sun power and satellite receiver module coupling, described microprocessor is realized the synchronous working pattern of the synchronous railway spike of sun power by programmed control.
The present invention compared with prior art has the following advantages: the present invention utilizes the time service function of earth synchronized positioning satellite that solar energy spike is carried out synchro control, the centralized control source that is provided with that difference and prior art are taked, use wireless or wired control mode that the solar energy spike in the control zone is carried out central controlled technical scheme, and use lock in time that solar energy spike is carried out management by synchronization, make the discrete solar energy spike of installing can be effectively worked at synchronous mode.This control method has overcome the prior art use and limited by area size, the defective that installation cost and operating cost are high has environments for use such as the link length of not being subjected to, trend and limits, and implements simple and convenient, reliability height, guiding are effective, and advantage such as have a extensive future.
Description of drawings
Fig. 1 is for adopting the sun power clock track pin structure schematic block diagram of embodiment solar energy spike synchronization control method.
Embodiment
Below by embodiment, the invention will be further elaborated in conjunction with the accompanying drawings.
The embodiment solar energy spike synchronization control method uses the technical scheme of lock in time the discrete solar energy spike of installing being carried out the synchro control management; The lock in time of utilizing the time service function of earth synchronized positioning satellite to provide, adopt the synchronous railway spike of sun power, control solar energy spike synchronous working.
Referring to Fig. 1, the embodiment sun synchronization can comprise housing, solar cell VS, battery pack V1, charge-discharge control circuit DA, open and close control circuit L1, micro-satellite receiving antenna TX, satellite receiver module CT, microprocessor CU and electroluminescence device by railway spike.Solar cell VS charges to battery pack V1, and is connected with keying control circuit L1 with charge-discharge control circuit DA; Solar cell VS is connected to battery pack V1 by charge-discharge control circuit DA, and charge-discharge control circuit DA is responsible for battery pack V1 is discharged and recharged control; Charge-discharge control circuit DA output is connected to and opens and closes control circuit L1, open and close control circuit L1 output and be connected to DC/DC circuit L2 and satellite receiver module CT, DC/DC circuit L2 changes operating voltage with adaptive various chip, module, the output connecting microprocessor CU of DC/DC circuit L2 and satellite receiver module CT with the voltage of battery pack V1.Micro-satellite receiving antenna TX connects satellite receiver module CT, the input of the output connecting microprocessor CU of satellite receiver module CT, wherein, the pulse per second (PPS) synchronizing signal of satellite receiver module CT is connected with the hardware interrupts input end of microprocessor CU, and the serial port of satellite receiver module CT is connected with the serial port of microprocessor CU.Microprocessor CU output terminal directly connects electroluminescence device, perhaps connect electroluminescence device again by driving circuit QD, microprocessor CU output signal control Driver Circuit QD controls lighting and closing of electroluminescence device again by driving circuit QD, and major applications does not need to connect driving circuit QD.
The control flow of embodiment solar energy spike synchronization control method is:
1, solar cell VS is by the charge or discharge of charge-discharge control circuit DA control built-in miniature battery pack V1, and controls the unlatching of electroluminescence device power supply or close by charge-discharge control circuit V1;
2, micro-satellite receiving antenna TX receives the satellite time signal that the time service function of earth synchronized positioning satellite provides;
3, after micro-satellite receiving antenna TX receives the satellite time signal, receiver module CT resolves and extracts temporal information and second synchronizing information via satellite;
4, microprocessor CU second after the synchronizing signal of receiving that satellite receiver module CT provides, light and close the electroluminescence device of the discrete synchronous railway spike of installing of sun power according to the flicker frequency that presets, flicker dutycycle.The synchronous railway spike of the discrete sun power of installing uses time configuration and the start-up time that stems from the identical accurate time service of satellite, carries out the mode of operation of high level of synchronization.Microprocessor CU distributes by the difference to the time service scheme, can obtain the synchronous railway spike of sun power different flicker frequency and dutycycle.
Utilize the satellite time signal to realize that the principle of solar energy spike synchronous working is:
The satellite positioning device that can receive within the border in China all provides the ability that the location coordinate is discerned, and accurate time service function.If when using the time service function of gps system, we can obtain the time service precision of about 100ns at present.For the synchronous railway spike of sun power, common 16 hours cumulative errors should be unable to exert an influence to the work of the synchronous railway spike of sun power less than flicker cycle 5%, and 16 hours is to set with each work maximum duration of the synchronous railway spike of sun power.With per minute 60 times flicker, per second has a flicker cycle, and by dutycycle design in 1: 1, then each flicker is bright 500ms, the 500ms that goes out, in actual motion, error less than 5% just less than 25ms.
Satellite positioning module can provide the date Hour Minute Second equal time data of coordinate information, Greenwich Mean Time, and synchronous second signal, and wherein the error of second signal is looked the configuration difference of chipset and module usually less than 100ns synchronously, and these data can be variant.After the satellite receiver module operate as normal, after promptly receiving satellite-signal and effective identification, can provide coordinate data, time data and second synchronizing signal, and not receive satellite-signal or the satellite-signal received can not discern the time, the satellite receiver module does not have above-mentioned data and signal output.The present invention with second synchronizing signal as counter enabling signal source, the meter reading precision is decided on actual request for utilization.After microprocessor identifies second synchronizing signal, beginning was counted according to the predetermined cycle, if use 1ms as the count cycle, then can obtain the count number of a 1000ms between the synchronizing signal two seconds, in this count number, can obtain any synchronous work period greater than 1ms, then another synchronous cycle has begun again 1000ms later on, so, for discrete solar energy spike, can also can be extended to several seconds synchronous signal cycle the count cycle according to designing application demand the lock in time that is obtained.Present embodiment, if the flicker frequency of railway spike is 60 times/minute, then counter is set to control signal of every 500ms output, light when synchronizing signal begins synchronously with second, continue to extinguish behind the 500ms, light when receiving second synchronizing signal more next time again, go round and begin again, the synchronous railway spike of sun power is closed when daytime.Different flicker frequencies only need be set lighting later working time and dutycycle, when for example the flicker frequency of the synchronous railway spike of sun power is set to 240 times, dutycycle 1: 1, this moment is when beginning when a second synchronizing signal, LED is the 125ms on and off at interval, begin next cycle when next second synchronizing signal arrives again.Different flicker frequencies all can obtain in different time configurations with different dutycycles, when cycle of working time during greater than 1 second, in order to obtain synchronously, need identification odd number second or even number second, as long as the Hour Minute Second signal that at this moment calls in Greenwich Mean Time is discerned.The discrete synchronous railway spike of installing of sun power will be under unified configuration lock in time synchronous working, be not subjected to the distance limit of installation site, the work synchronism between each railway spike is very good.
The housing of the synchronous railway spike of embodiment sun power adopts pressure-bearing and is fit to the profile that road traffic uses, and inner space with mounting circuit boards and battery pack V1, and the outside has the position that solar panel VS is installed.The housing of the synchronous railway spike of sun power is satisfying under the prerequisite of above-mentioned condition, can use multiple shape profiles such as circle, square, ellipse.Use square aluminum mass shell body among the embodiment, adopt 125 * 125 * 25 millimeters Al-alloy casings that meet GB/T 19813-2005 standard-required.Housing does not influence the final result of use of the synchronous railway spike of sun power.
Solar cell VS can use all types solar cell of photoelectric transformation efficiency greater than solar energy spike power demand area ratio, used polysilicon solar cell in an embodiment, adopt the polysilicon solar cell of one group of about 0.55W, solar cell VS is installed on the solar panel installation site on housing top, and covers on the solar cell with wear-resisting acrylic transparent film.The configuration of solar cell VS need be considered the power consumption requirement that circuit is formed, and makes the number at sunshine of land used, and the technical goal of railway spike etc., select adaptive; The capacity of solar cell VS does not have direct relation with realizing the target of synchronousing working, and the continuous working period of the synchronous railway spike of sun power is relevant with solar panel VS and accumulator V1 capacity.
Battery pack V1 adopts the built-in miniature battery pack, the built-in miniature battery pack can be used and meet the battery pack that the road traffic environment temperature variation required and satisfied built-in volume requirement and capacity requirement, used Ni-MH battery in an embodiment, adopt the Ni-MH battery of two joint AAA type 800mA/H capacity, the inner space of the housing of present embodiment only can hold two joint AAA batteries, and uses two joint AAA nickel-hydrogen accumulators to meet the operating voltage requirement of railway spike chipset and module.In actual use, difference with environment for use, a configurable joint, two joint or multiple batteries more, the battery of also configurable other capacity or material, its cell arrangement pattern mainly is limited by the parameters such as adaptation coefficients of the voltage that uses chipset or module, power, solar panel VS, and the effect of synchronousing working with railway spike does not have necessary relation.
Discharge and recharge and open and close in the control circuit charge-discharge control circuit DA and mainly be responsible for battery pack V1 is discharged and recharged control, prevent to overcharge or overdischarge; Keying control circuit L1 is responsible for detecting the work threshold value of solar energy spike, will close solar energy spike by day, opens solar energy spike night, accepts microprocessor CU control simultaneously, to realize the working state administration to each parts.
Satellite receiver module CT can receive the satellite time signal, can select the receiver module that uses single-chip or multicore sheet to form.The satellite time service source of selecting when satellite receiver module CT and solar energy spike are implemented synchro control is complementary, can select the receiver module of GPS System in USA, or the receiver module of Europe " Galileo " satellite, or the receiver module of Russia's " GLONASS " global navigation and position, or China's " Big Dipper " satnav receiver module, different satellite receiver modules is similar on final result of use.Satellite receiver module CT uses supporting with it micro-satellite receiving antenna TX, so that can obtain best reception and meet technology and the volume requirement that is installed in the solar energy spike.The selection of satellite receiver module CT, though but the satellite time service source that commercialization is at present used has at least four kinds, but use the GPS of USA system that remains comparatively widely in the world, and its chipset is also comparatively ripe and cheap, present embodiment uses gps system as synchronous time dissemination system source, adopts U.S. SiRF chipset as the satellite receiving chip.Usually chipset is formed have in actual use and used the module that stresses so that finally use, the actual most important applications of present embodiment is time service, adopt that Hangzhou Command Communication Equipment Co., Ltd produces based on the miniature low-power consumption module of CTCT type of U.S. SiRFIII GPS chipset as satellite receiver module CT.This module is mainly used in the industrial application that needs synchronous time service, also exports data such as Greenwich Mean Time and coordinate simultaneously, has second synchronizing signal output, the synchronous signal impulse width-adjustable, and the time precision error that is as the criterion with rising edge is smaller or equal to 15ns.
Microprocessor CU mainly finishes the signal that satellite receiver module CT is received and carries out post-processed and final output efficient synchronization control signal, microprocessor CU and satellite receiver module CT coupling, microprocessor CT realizes the synchronous working pattern of solar energy spike by programmed control.The tape program control of confession and the microprocessor of processing power are arranged in the market, under the prerequisite that satisfies power consumption/processing power/requirements such as control function/volume, almost all can adopt.The 51 Series P 89LPC915HDH type single-chip microcomputers that the microprocessor CU of present embodiment uses the tape program of ripe low-power consumption to handle, select the reason of this microprocessor to be based on it and have function and can satisfy request for utilization, and power consumption and voltage indexes also meet request for utilization.Microprocessor CU opens and closes control circuit L1 by instruction control and realizes work management to satellite receiver module CT, and when microprocessor CU was in " automatically " state, satellite receiver module CT directly obtained power supply by DC/DC circuit L2; When microprocessor CU intervenes satellite receiver module CT duty, can be by opening and closing the working power of control circuit L1 cut-out satellite receiver module CT.
Electroluminescence device can adopt LED or other electroluminescent element, and present embodiment adopts LED, and microprocessor CU is connected with led circuit.The microprocessor of not all model is driving LED directly, when needs are two-sided when lighting the LED of solar energy spike, can increase Drive and Control Circuit QD at the led circuit front end, QD is connected to led circuit by Drive and Control Circuit, driving circuit QD amplifies drive current, and driving circuit QD uses common low-power transistor to get final product; When using single face to show, P89LPC915HDH type single-chip microcomputer can directly drive required LED.The color of LED selects to look the actual needs setting, general redness, the yellow and white LED of adopting, usually the single face display window of solar energy spike is installed 3 LED, if the double-sided display window is then respectively installed 3 LED, its brightness and half strong angle should meet national standard.
The synchronous railway spike of sun power by day, to quit work when for example illumination is greater than 150LEX, when entering night, solar cell VS electromotive force is lower than closes threshold value, open and close control circuit L1 and be unlocked this moment, microprocessor CU is activated, satellite receiver module CT starts, begin to enter cold start, not output of the serial port of satellite receiver module CT and second signal output part in searching the star process, after receiver module CT receives effective satellite-signal, will will export Greenwich Mean Time and coordinate parameters from serial port simultaneously from signal Synchronization end each a second output second signal second.In the present invention, coordinate data be will abandon, real-time time data and second signal only used.Second, the pulse width of signal output can be provided with, and in receiver module CT, present embodiment has been selected signal pulse width second of 100ns, and the rising edge of signal pulse is the sign that begins of second synchronizing signal with second, and its positive negative error is less than 15ns.Microprocessor CU interrupts capturing and produced hardware interrupts after the synchronizing signal in effective second, and beginning is unit count with 1 millisecond, digit can decide on final output accuracy requirement, and step-length also can be decided as required, as long as final precision satisfies request for utilization.Since the moment that second, synchronizing signal arrived, the control signal of LED is lighted in microprocessor CU output, when predetermined ignition period finishes, the control signal of LED is closed in output, open counting again and light LED when next second synchronizing signal arrives, LED is lighted, closes in circulation, finishes until the work period, be illumination during greater than the system closing threshold value, the synchronous railway spike of whole sun power will be closed.If when using 60 flicker frequencies, when second, synchronizing signal arrived, light LED, when counting is expired 500ms, close LED, when next second synchronizing signal arrives, begin second control cycle again, until closing.
Because the control interval is very little, the clock accuracy of microprocessor satisfies the operating error requirement of the synchronous railway spike of sun power fully, so generally do not need the flow process that calibrates for error.Under the condition of time synchronized,, can realize the synchronous working state of multiple different control models by the control of software.For example, when special festivals or holidays or special application demand, need regularly start solar energy spike, its implementation method is the time conditions that startup is set in the program of microprocessor CU, use Greenwich Mean Time to carry out local zone time conversion and calibration according to the coordinate time zone again, control the opening and closing time of solar energy spike by local zone time, the time conditions that opening and closing time promptly need be provided with, microprocessor CU controls the duty of solar energy spike by the comparison time condition, when satisfying entry condition, then open, satisfy and then close solar energy spike when closing condition.
Above embodiment has done comparatively detailed description to solar energy spike synchronization control method of the present invention; but these descriptions are not in order to limit protection scope of the present invention; any technician who is familiar with this technology; change and the retouching done in not breaking away from design of the present invention and scope all should belong to protection scope of the present invention.
Claims (4)
1, a kind of solar energy spike synchronization control method is characterized in that: utilize the time service function of earth synchronized positioning satellite, adopt the synchronous railway spike of sun power, use same time source that the discrete synchronous railway spike of installing of sun power is carried out synchronous working control;
The synchronous railway spike of described sun power comprises housing, solar cell, battery pack and discharges and recharges and open and close control circuit, micro-satellite receiving antenna, satellite receiver module, microprocessor and electroluminescence device; Described solar cell is to battery charging, and with charge-discharge control circuit with open and close control circuit and be connected, the micro-satellite receiving antenna connects the satellite receiver module, the satellite receiver module connects microprocessor, output end of microprocessor is connected with electroluminescence device, and electroluminescence device is by microprocessor driven and control;
After described micro-satellite receiving antenna receives the time signal of earth synchronized positioning satellite, temporal information and second synchronizing information are resolved and extracted to receiver module via satellite, after microprocessor receives that the satellite receiver module provides second synchronizing signal, lighting and closing according to the flicker frequency that presets, flicker dutycycle control electroluminescence device, the synchronous railway spike of the discrete sun power of installing uses time configuration and the start-up time that stems from the identical accurate time service of satellite, carries out the mode of operation of high level of synchronization.
2, solar energy spike synchronization control method according to claim 1 is characterized in that: described microprocessor distributes by the difference to the time service scheme, obtains different flicker frequency and the dutycycles of the synchronous railway spike of sun power.
3, solar energy spike synchronization control method according to claim 2 is characterized in that: the time service source of the earth synchronized positioning satellite that the satellite receiver module of the synchronous railway spike of described sun power and solar energy spike synchronization control method are selected is complementary.
4, solar energy spike synchronization control method according to claim 3, it is characterized in that: the microprocessor of the synchronous railway spike of described sun power and satellite receiver module coupling, described microprocessor is realized the synchronous working pattern of the synchronous railway spike of sun power by programmed control.
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CNA2009100985905A CN101567129A (en) | 2009-05-18 | 2009-05-18 | Solar energy spike synchronization control method |
PCT/CN2010/072706 WO2010133145A1 (en) | 2009-05-18 | 2010-05-13 | Synchronisation control method for solar road studs |
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CNA2009100985905A CN101567129A (en) | 2009-05-18 | 2009-05-18 | Solar energy spike synchronization control method |
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