CN204903641U - Current detection system of GNSS module - Google Patents
Current detection system of GNSS module Download PDFInfo
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- CN204903641U CN204903641U CN201520682375.0U CN201520682375U CN204903641U CN 204903641 U CN204903641 U CN 204903641U CN 201520682375 U CN201520682375 U CN 201520682375U CN 204903641 U CN204903641 U CN 204903641U
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- gnss module
- operational amplifier
- power supply
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- current
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Abstract
The utility model relates to a current detection technical field especially relates to a current detection system of GNSS module. The utility model provides a current detection system of GNSS module, comprising an one -chip microcomputer, the current detection system still include with the singlechip links to each other, detects respectively the mains voltage commonly used of GNSS module and reserve mains voltage's voltage testing. The utility model discloses change the mode of prior art to GNSS module power commonly used and GNSS module stand -by power supply's current measurement to the improvement is to GNSS module stand -by power supply current measurement and GNSS module power current measurement's commonly used automation, makes that the data that record can be taken notes by the host computer, save and analysis.
Description
Technical field
The utility model relates to current detection technology field, particularly relates to a kind of current detecting system of GNSS module.
Background technology
Along with city is constantly expanded, market to can the demand of electronic product of location navigation also increasing.And the quality requirements of the electronic hardware module possessing GNSS (GlobalNavigationSatelliteSystem) GPS (Global Position System) function is also constantly improved.As everyone knows, in the quality check process of electronic hardware module, the measurement of various performance parameter is essential.
In prior art, metering system GNSS module standby power supply electric current and GNSS module being commonly used to source current parameter measures with Universal-current table, then by manually carrying out reading and data analysis.
Utility model content
The purpose of this utility model is the current detecting system providing a kind of GNSS module, be intended to change prior art commonly uses the current measurement of power supply and GNSS module standby power supply mode to GNSS module, thus improve the robotization standby power supply current measurement of GNSS module and GNSS module being commonly used to power-supply current measuring, make measured data can by host computer record, preservation and analysis.
The utility model realizes like this, a kind of current detecting system of GNSS module, comprise single-chip microcomputer, described current detecting system also comprises and is connected with described single-chip microcomputer, detects the conventional supply voltage of GNSS module and the voltage detection module of backup power source voltage respectively;
Described voltage detection module comprises conventional power sense circuit and standby power supply testing circuit, and each testing circuit comprises operational amplifier, inductive reactance, current-limiting resistance and a sampling resistor; Described inductive reactance is connected between both ends of power, described current-limiting resistance is connected between the simulating signal positive input terminal of power input and operational amplifier, and described sampling resistor is connected between the digital signal positive input terminal of operational amplifier and ground;
Described operational amplifier connects described single-chip microcomputer respectively by its digital signal output end, so that the conventional supply voltage value of the GNSS recorded module or backup power source voltage value are sent to described single-chip microcomputer, described single-chip microcomputer calculates the conventional power supply of GNSS module and the current value of standby power supply respectively according to the magnitude of voltage obtained.
Accordingly, the utility model also provides a kind of detection method of the current detecting system based on described GNSS module, and described method comprises:
Obtained the magnitude of voltage of the standby power supply of GNSS module by standby power supply testing circuit, be transferred to described single-chip microcomputer;
Described single-chip microcomputer according to obtain magnitude of voltage, according to relational expression:
calculate the standby power supply current value of GNSS module; Wherein, V
aPD1for the magnitude of voltage of the standby power supply of described GNSS module, R
c1, R
g1and R
1be respectively the resistance of current-limiting resistance, sampling resistor and the inductive reactance in described standby power supply testing circuit;
Obtained the magnitude of voltage of the conventional power supply of GNSS module by conventional power sense circuit, be transferred to described single-chip microcomputer;
Described single-chip microcomputer according to obtain magnitude of voltage, according to relational expression:
calculate the conventional power electric flow valuve of GNSS module; Wherein, V
aPD2for the magnitude of voltage of the conventional power supply of described GNSS module, R
c2, R
g2and R
2be respectively the resistance of current-limiting resistance, sampling resistor and the inductive reactance in described conventional power sense circuit.
The current detecting system of GNSS module of the present utility model comprises and is connected with single-chip microcomputer, detects the conventional supply voltage of GNSS module and the voltage detection module of backup power source voltage respectively; Described voltage detection module comprises conventional power sense circuit and standby power supply testing circuit, each testing circuit comprises at least one operational amplifier, described operational amplifier connects described single-chip microcomputer respectively by its digital signal output end, so that the conventional supply voltage value of the GNSS recorded module or backup power source voltage value are sent to described single-chip microcomputer, described single-chip microcomputer calculates the conventional power supply of GNSS module and the current value of standby power supply respectively according to the magnitude of voltage obtained.Change prior art commonly uses the current measurement of power supply and GNSS module standby power supply mode to GNSS module, thus improve the robotization standby power supply current measurement of GNSS module and GNSS module being commonly used to power-supply current measuring, make measured data can by host computer record, preservation and analysis.
First to detect the standby power supply of GNSS module, detect the conventional power electric flow valuve of GNSS module again, avoid when detecting GNSS module, because close the conventional power supply of GNSS module after opening the current value of the conventional power supply of the conventional power detecting GNSS module of GNSS module, make to produce residual voltage or electric current in GNSS module, ensure that the accuracy of measured data.And realize the current measurement value one_to_one corresponding of the current measurement value of the standby power supply of preset data and GNSS module and the conventional power supply of GNSS module, conveniently carry out the statistics of data, preservation and analysis.
Accompanying drawing explanation
Fig. 1 is the structural representation of the current detecting system of GNSS module of the present utility model.
Fig. 2 is conventional power sense circuit schematic diagram of the present utility model.
Fig. 3 is standby power supply testing circuit schematic diagram of the present utility model.
Fig. 4 is the method flow diagram of the current detecting of GNSS module of the present utility model, also the process flow diagram of described embodiment of the method 1.
Fig. 5 is embodiment 2 process flow diagram corresponding to the method for the current detecting of GNSS module of the present utility model.；
Fig. 6 is embodiment 3 process flow diagram corresponding to the method for the current detecting of GNSS module of the present utility model.
In Fig. 2,3V3_GPS end is the conventional power input of GNSS module; 3V3_GPS_VCC end is the conventional power output end of GNSS module; ADP5_VCC end is the digital signal output end of the first operational amplifier U1.
In Fig. 3,3_3V end is the standby power supply input end of GNSS module; VBAT end is the standby power supply output terminal of GNSS module; ADP6_VCC_VBAT end is the digital signal output end of the second operational amplifier U2.
Embodiment
In order to make the object of utility model, technical scheme and advantage clearly understand, below in conjunction with drawings and Examples, utility model is further elaborated.Should be appreciated that specific embodiment described herein only in order to explain utility model, and be not used in restriction utility model.
The current detecting system of GNSS module of the present utility model comprises and is connected with single-chip microcomputer, detects the conventional supply voltage of GNSS module and the voltage detection module of backup power source voltage respectively; Described voltage detection module comprises conventional power sense circuit and standby power supply testing circuit, each testing circuit comprises at least one operational amplifier, described operational amplifier connects described single-chip microcomputer respectively by its digital signal output end, so that the conventional supply voltage value of the GNSS recorded module or backup power source voltage value are sent to described single-chip microcomputer, described single-chip microcomputer calculates the conventional power supply of GNSS module and the current value of standby power supply respectively according to the magnitude of voltage obtained.Change prior art commonly uses the current measurement of power supply and GNSS module standby power supply mode to GNSS module, thus improve the robotization standby power supply current measurement of GNSS module and GNSS module being commonly used to power-supply current measuring, make measured data can by host computer record, preservation and analysis.
Fig. 1 shows the structural representation of the current detecting system of the utility model GNSS module.
The current detecting system of the GNSS module in the utility model, comprises host computer 10 and single-chip microcomputer 20.As shown in Figure 1, the current detecting system of described GNSS module also comprises the voltage detection module 100 for detecting GNSS module 30.In all the present embodiment of the present utility model, described host computer 10 can be the computing machine of existing data statistics, and described single-chip microcomputer 20 is electrically connected with described host computer 10, and both cooperations realize data processing, statistics and display.
As shown in Figure 1, as embodiment of the present utility model, described voltage detection module 100 comprises: conventional power sense circuit 101 and standby power supply testing circuit 102.
Concrete, as shown in Figure 1, described conventional power sense circuit 101 comprises at least one operational amplifier U, inductive reactance R
2, current-limiting resistance R
c2with sampling resistor R
g2.Described inductive reactance R is connected between conventional power supply 31 two ends of GNSS module.Described current-limiting resistance R
c1between the input end being connected to the conventional power supply 31 of GNSS module and the simulating signal positive input terminal of operational amplifier U, described sampling resistor R
gbe connected between the digital signal positive input terminal of operational amplifier U and ground.
Preferably, in the present embodiment, the conventional power supply 31 being controlled described GNSS module by described single-chip microcomputer 20 is opened, and the conventional conventional power supply 31 of power sense circuit 101 to described GNSS module is measured.Obtain the magnitude of voltage of the conventional power supply 31 of described GNSS module, the magnitude of voltage of the conventional power supply 31 of the GNSS module recorded is sent to single-chip microcomputer 20, then the current value of the conventional power supply 31 being calculated GNSS module by described single-chip microcomputer 20 is transferred to host computer 10.
As shown in Figure 1, described standby power supply testing circuit 102 comprises at least one operational amplifier U, inductive reactance R
1, current-limiting resistance R
c1with sampling resistor R
g1.Described inductive reactance R is connected between standby power supply 32 two ends of GNSS module.Described current-limiting resistance R
cbetween the input end being connected to the standby power supply 32 of GNSS module and the simulating signal positive input terminal of operational amplifier U, described sampling resistor R
gbe connected between the digital signal positive input terminal of operational amplifier U and ground.
Preferably, in the present embodiment, the conventional power supply 31 being controlled described GNSS module by described single-chip microcomputer 20 is closed, and the standby power supply 32 of standby power supply testing circuit 102 to described GNSS module is measured.Obtain the magnitude of voltage of the standby power supply 32 of described GNSS module, the magnitude of voltage of the standby power supply 32 of the GNSS module recorded is sent to single-chip microcomputer 20, then the current value calculating GNSS module standby power supply 32 by described single-chip microcomputer 20 is transferred to host computer 10.
In the present embodiment, described host computer 10 compares with standard value respectively for the conventional power supply 31 of GNSS module that calculated by described single-chip microcomputer 10 and the current value of standby power supply 32, exports the whether qualified signal of this GNSS module 30 according to comparative result.
Fig. 2 shows conventional power sense circuit schematic diagram of the present utility model.
As shown in Figure 2, based on above-described embodiment, optionally, testing circuit 101 comprises: the first operational amplifier U1, resistance R102, current-limiting resistance R103, inductive reactance R101, sampling resistor R104, the first switching tube Q1, electric capacity C203 and electric capacity C204.
As shown in Figure 2, in order to realize that the induction current at inductive reactance two ends is converted to digital signal, in the present embodiment, the dual operational amplifier of described first operational amplifier U1 to be model be AD8572ARZ, concrete, its each pinout is:
No. 1 pin: analog signal output OUT_A; No. 2 pins: simulating signal negative input end-IN_A; No. 3 pins: simulating signal positive input terminal+IN_A; No. 4 pins: negative voltage input end V-; No. 5 pins: digital signal positive input terminal+IN_B; No. 6 pins: digital signal negative input end-IN_B; No. 7 pins: digital signal output end OUT_B; No. 8 pins: positive voltage input end V+.
In the present embodiment, described inductive reactance R101 two ends connect conventional power input and the output terminal of described GNSS module respectively.
As shown in Figure 2, simulating signal positive input terminal+the IN_A of described first operational amplifier U1 is connected with the hot end of described first switching tube Q1 simultaneously, and the control end of described first switching tube Q1 is connected with digital signal positive input terminal+IN_B with the analog signal output OUT_A of described first operational amplifier U1 respectively with cold end.Digital signal positive input terminal+the IN_B of described first operational amplifier U1 is through described sampling resistor R104 ground connection.
In the present embodiment, the simulating signal negative input end-IN_A of described first operational amplifier U1 connects conventional power supply 31 output terminal by described resistance R102, and its digital signal negative input end-IN_B and digital signal output end OUT_B connects described single-chip microcomputer 20 altogether.The negative voltage input end V-ground connection of described first operational amplifier U1, its positive voltage input end V+ meets operating voltage VCC.
Optionally, described electric capacity C203 and electric capacity C204 is all as filtering, between the positive voltage input end V+ that described electric capacity C204 is connected on described first operational amplifier U1 and ground, between the digital signal positive input terminal+IN_B that described electric capacity C203 is connected to described first operational amplifier U1 and ground.
Optionally, filter capacitor C201 and electric capacity C202 is also comprised in the present embodiment, electric capacity C201 is connected to connecing altogether of described inductive reactance R101 and current-limiting resistance R103 and holds between ground, and electric capacity C202 is connected to connecing altogether of described inductive reactance R101 and resistance R102 and holds between ground.
In all embodiments of the present utility model, described first switching tube Q1 is metal-oxide-semiconductor with body diode or IGBT.
Alternatively, described first switching tube Q1 is the metal-oxide-semiconductor Q1 with body diode.The grid of the described metal-oxide-semiconductor Q1 with body diode, drain electrode and source electrode are respectively the control end of the first switching tube Q1, hot end and cold end.
Alternatively, described first switching tube Q1 can also be IGBT pipe Q1.The grid of described IGBT pipe Q1, drain electrode and source electrode are respectively the control end of the first switching tube Q1, hot end and cold end.
In actual application, can select according to the cast of circuit design requirements to the first switching tube Q1, to reach the object at utmost realizing voltage detection module overall performance.
In the present embodiment, described inductive reactance R101 can be existing electric current inductive reactance, and described inductive reactance R101 two ends connect input end and the output terminal that described GNSS module commonly uses power supply 31 respectively.When commonly using power supply 31 in described GNSS module and opening, commonly use power supply 31 by described GNSS module and apply voltage to inductive reactance R101 two ends, the voltage of described first operational amplifier U1 to described inductive reactance R101 two ends carries out signals collecting, and the analog voltage signal collected is converted to digital signal sends to single-chip microcomputer 20.Described single-chip microcomputer 20 carries out corresponding calculating to described digital signal, obtains the current value that described GNSS module commonly uses power supply 31.
Fig. 3 shows standby power supply testing circuit schematic diagram of the present utility model.
As shown in Figure 3, based on above-described embodiment, optionally, testing circuit 101 comprises: the second operational amplifier U2, resistance R105, inductive reactance R106, current-limiting resistance R107, sampling resistor R108, second switch pipe Q2, electric capacity C207 and electric capacity C208.
As shown in Figure 3, in order to realize that the induction current at inductive reactance two ends is converted to digital signal, in the present embodiment, the dual operational amplifier of described second operational amplifier U2 to be model be AD8572ARZ, concrete, its each pinout is:
No. 1 pin: analog signal output OUT_A; No. 2 pins: simulating signal negative input end-IN_A; No. 3 pins: simulating signal positive input terminal+IN_A; No. 4 pins: negative voltage input end V-; No. 5 pins: digital signal positive input terminal+IN_B; No. 6 pins: digital signal negative input end-IN_B; No. 7 pins: digital signal output end OUT_B; No. 8 pins: positive voltage input end V+.
In the present embodiment, described inductive reactance R106 two ends connect standby power supply input end and the output terminal of described GNSS module respectively.
As shown in Figure 3, simulating signal positive input terminal+the IN_A of described second operational amplifier U2 is connected with the hot end of described second switch pipe Q2 simultaneously, and the control end of described second switch pipe Q2 is connected with digital signal positive input terminal+IN_B with the analog signal output OUT_A of described second operational amplifier U2 respectively with cold end.Digital signal positive input terminal+the IN_B of described second operational amplifier U2 is through described sampling resistor R108 ground connection.
In the present embodiment, the simulating signal negative input end-IN_A of described second operational amplifier U2 connects conventional power supply 32 output terminal by described resistance R105, and its digital signal negative input end-IN_B and digital signal output end OUT_B connects described single-chip microcomputer 20 altogether.The negative voltage input end V-ground connection of described second operational amplifier U2, its positive voltage input end V+ meets operating voltage VCC.
Optionally, described electric capacity C207 and electric capacity C207 is all as filtering, between the positive voltage input end V+ that described electric capacity C208 is connected on described second operational amplifier U2 and ground, between the digital signal positive input terminal+IN_B that described electric capacity C207 is connected to described second operational amplifier U2 and ground.
Optionally, filter capacitor C205 and electric capacity C206 is also comprised in the present embodiment, electric capacity C205 is connected to connecing altogether of described inductive reactance R106 and current-limiting resistance R107 and holds between ground, and electric capacity C206 is connected to connecing altogether of described inductive reactance R106 and resistance R105 and holds between ground.
In all embodiments of the present utility model, described second switch pipe Q2 is metal-oxide-semiconductor with body diode or IGBT.
Alternatively, described second switch pipe Q2 is the metal-oxide-semiconductor Q2 with body diode.The grid of the described metal-oxide-semiconductor Q2 with body diode, drain electrode and source electrode are respectively the control end of second switch pipe Q2, hot end and cold end.
Alternatively, described second switch pipe Q2 can also be IGBT pipe Q2.The grid of described IGBT pipe Q2, drain electrode and source electrode are respectively the control end of the first switching tube Q2, hot end and cold end.
In actual application, can select according to the cast of circuit design requirements to second switch pipe Q2, to reach the object at utmost realizing voltage detection module overall performance.
In the present embodiment, described inductive reactance R106 can be existing electric current inductive reactance, and described inductive reactance R106 two ends connect input end and the output terminal of the standby power supply 32 of described GNSS module respectively.When closing at the conventional power supply 31 of described GNSS module, voltage is applied to inductive reactance R106 two ends by the standby power supply 32 of described GNSS module, the voltage of described second operational amplifier U2 to described inductive reactance R106 two ends carries out signals collecting, and the analog voltage signal collected is converted to digital signal sends to single-chip microcomputer 20.Described single-chip microcomputer 20 carries out corresponding calculating to described digital signal, obtains the current value of described GNSS module standby power supply 32.
The utility model still further provides a kind of detection method of the current detecting system based on described GNSS module.
Fig. 4 shows the detection method schematic flow sheet of the utility model based on the current detecting system of described GNSS module, and concrete steps are:
S10: the magnitude of voltage being obtained the standby power supply of GNSS module by standby power supply testing circuit, is transferred to described single-chip microcomputer;
S20: described single-chip microcomputer according to obtain magnitude of voltage, according to relational expression:
calculate the standby power supply current value of GNSS module;
S30: the magnitude of voltage being obtained the standby power supply of GNSS module by standby power supply testing circuit, is transferred to described single-chip microcomputer;
S40: described single-chip microcomputer according to obtain magnitude of voltage, according to relational expression:
calculate the conventional power electric flow valuve of GNSS module.
In above-described embodiment, step S20: in, described V
aPD1for the magnitude of voltage of the standby power supply of described GNSS module, R
c1, R
g1and R
1be respectively the resistance of current-limiting resistance, sampling resistor and the inductive reactance in described standby power supply testing circuit.Step S40: in, described V
aPD2for the magnitude of voltage of the conventional power supply of described GNSS module, R
c2, R
g2and R
2be respectively the resistance of current-limiting resistance, sampling resistor and the inductive reactance in described conventional power sense circuit.
The method of the current detecting that the utility model embodiment provides, change mode module to be measured measured with traditional multimeter, the automaticity not only making measurement GNSS module commonly use source current and GNSS module standby power supply electric current gets a promotion, but also make to measure the result that obtains and fast and generate the tables of data corresponding with electronic hardware module data to be measured efficiently, more easily can add up, preserve and data analysis.
The method of a kind of current detecting provided by the utility model, another embodiment proposed based on above-described embodiment.For the ease of carrying out data analysis and comparison, while measuring module to be measured, enumerate out by each measured value of module to be measured and ratings.
As shown in Figure 5, based on another embodiment that above-described embodiment proposes, before step S10, also comprise:
S00: close GNSS module and commonly use power supply.
Before step S30, also comprise:
S20 ': open GNSS module and commonly use power supply.
In the present embodiment, first to detect the standby power supply of GNSS module, detect the conventional power electric flow valuve of GNSS module again, avoid when detecting GNSS module, because close the conventional power supply of GNSS module after opening the current value of the conventional power supply of the conventional power detecting GNSS module of GNSS module, make to produce residual voltage or electric current in GNSS module, ensure that the accuracy of measured data.And realize the current measurement value one_to_one corresponding of the current measurement value of the standby power supply of preset data and GNSS module and the conventional power supply of GNSS module, conveniently carry out the statistics of data, preservation and analysis.
It should be noted that, in all embodiments of the present utility model, when utilizing the current detecting system of GNSS module of the present utility model to detect GNSS module in conjunction with the electric current detecting method of GNSS module of the present utility model, the conventional power sense circuit in the current detecting system of described GNSS module and standby power supply testing circuit should be understood to separate detecting unit.Therefore, in step S20, described relational expression:
described in V
aPD1for the magnitude of voltage of the standby power supply of described GNSS module, R
c1, R
g1and R
1be respectively the resistance of current-limiting resistance, sampling resistor and the inductive reactance in described standby power supply testing circuit.In step s 40, described relational expression:
described in V
aPD2for the magnitude of voltage of the conventional power supply of described GNSS module, R
c2, R
g2and R
2be respectively the resistance of current-limiting resistance, sampling resistor and the inductive reactance in described conventional power sense circuit.
In conjunction with above-described embodiment, another embodiment is proposed.
As shown in Figure 6, at described step S20: single-chip microcomputer according to obtain magnitude of voltage, according to relational expression:
after calculating the standby power supply current value step of GNSS module, also comprise:
Step S21: the current value of the GNSS module standby power supply that described single-chip microcomputer calculates by host computer compares with standard value respectively, exports the whether qualified signal of the standby power supply of this GNSS module according to comparative result.
At described step S40: single-chip microcomputer according to obtain magnitude of voltage, according to relational expression:
calculate the conventional power electric flow valuve of GNSS module; Afterwards, also comprise:
Step S41: the current value that the GNSS module that described single-chip microcomputer calculates by host computer commonly uses power supply compares with standard value respectively, exports the whether qualified signal of the conventional power supply of this GNSS module according to comparative result.
Table 1 for being numbered five different GNSS modules respectively based on above-mentioned detection method, and detects obtained tables of data to it.
Table 1
As shown in table 1, I
vBATstandard value be the conventional source current standard value of the module to be measured pre-entered, its unit is mA.Shown in associative list 1, in the present embodiment, the current value of the GNSS module standby power supply that single-chip microcomputer calculates is I
vBAT, described I
vBATdetected value equation is:
wherein, V
aPD1for standby power supply output voltage detected value, R
c1for the current-limiting resistance resistance in described standby power supply testing circuit, R
g1for the sampling resistor resistance in described standby power supply testing circuit, R
1for induced electricity resistance.In the present embodiment, I
vCCdetected value equation be:
wherein, V
aPD2for conventional electric power output voltage detected value, R
c2for the current-limiting resistance resistance in described conventional power sense circuit, R
g2for the sampling resistor resistance in described conventional power sense circuit, R
2for induced electricity resistance.
Concrete, in the present embodiment, in step S41: the current value that the GNSS module that described single-chip microcomputer calculates by host computer commonly uses power supply compares with standard value respectively, export the whether qualified signal of the conventional power supply of this GNSS module according to comparative result.
In table 1, the testing result of GNSS module 1 is as follows:
Wherein, I
vCCstandard value be 1mA, and to record detected value be 1.5mA.The detected value of the conventional electric power outputting current of this GNSS module 1 visible is greater than 1.2 times of conventional electric power outputting current standard value.Therefore, output detections information is: conventional power supply is defective.
In table 1, the testing result of GNSS module 3 is as follows:
Wherein, I
vBATstandard value be 50 μ A, and to record detected value be 60.5 μ A.The detected value of the standby power supply output current of this GNSS module 3 visible is greater than 1.2 times of standby power supply output current standard value.Therefore, output detections information is: standby power supply is defective.
Due to most of module to be measured after a loss of power, produce residual voltage or electric current, therefore in other embodiments of the present utility model, the object that step S00: closedown GNSS module commonly uses power supply is: the standby power supply current value recording module to be measured more fast more accurately, reduce the error of standby power supply current detection value, shorten detection time.
The foregoing is only preferred embodiment of the present utility model, not in order to limit utility model, any amendment done within all spirit in utility model and principle, equivalently to replace and improvement etc., within the protection domain that all should be included in utility model.
Claims (8)
1. a current detecting system for GNSS module, comprises single-chip microcomputer, it is characterized in that, described current detecting system also comprises and is connected with described single-chip microcomputer, detects the conventional supply voltage of GNSS module and the voltage detection module of backup power source voltage respectively;
Described voltage detection module comprises conventional power sense circuit and standby power supply testing circuit, and each testing circuit comprises operational amplifier, inductive reactance, current-limiting resistance and a sampling resistor; Described inductive reactance is connected between both ends of power, described current-limiting resistance is connected between the simulating signal positive input terminal of power input and operational amplifier, and described sampling resistor is connected between the digital signal positive input terminal of operational amplifier and ground;
Described operational amplifier connects described single-chip microcomputer respectively by its digital signal output end, so that the conventional supply voltage value of the GNSS recorded module or backup power source voltage value are sent to described single-chip microcomputer, described single-chip microcomputer calculates the conventional power supply of GNSS module and the current value of standby power supply respectively according to the magnitude of voltage obtained.
2. the current detecting system of GNSS module as claimed in claim 1, it is characterized in that, described current detecting system also comprises the host computer be connected with described single-chip microcomputer;
Described host computer is used for the conventional power supply of GNSS module that calculated by described single-chip microcomputer and the current value of standby power supply compares with standard value respectively, exports the whether qualified signal of this GNSS module according to comparative result.
3. the current detecting system of GNSS module as claimed in claim 1, it is characterized in that, described conventional power sense circuit also comprises:
First switching tube Q1, resistance R102, electric capacity C203 and electric capacity C204;
The simulating signal positive input terminal of described operational amplifier is connected with the hot end of described first switching tube Q1 simultaneously, the control end of described first switching tube Q1 is connected with digital signal positive input terminal with the analog signal output of described operational amplifier respectively with cold end, the simulating signal negative input end of described operational amplifier connects conventional power output end by described resistance R102, the digital signal negative input end of described operational amplifier and digital signal output end connect described single-chip microcomputer altogether, the negative voltage input end grounding of described operational amplifier, the positive voltage input termination operating voltage of described operational amplifier, described electric capacity C204 is connected between the positive voltage input end of described operational amplifier and ground, described electric capacity C203 is connected between the digital signal positive input terminal of described operational amplifier and ground, electric capacity C201 is connected to described inductive reactance and connecing altogether of current-limiting resistance is held between ground, electric capacity C202 is connected to described inductive reactance and connecing altogether of resistance R102 is held between ground.
4. the current detecting system of GNSS module as claimed in claim 3, it is characterized in that, described standby power supply testing circuit also comprises:
Second switch pipe Q2, resistance R105, electric capacity C207 and electric capacity C208;
The simulating signal normal phase input end of described operational amplifier is connected with the hot end of described second switch pipe Q2 simultaneously, the control end of described second switch pipe Q2 is connected with digital signal normal phase input end with the analog signal output of described operational amplifier respectively with cold end, the simulating signal negative-phase input of described operational amplifier connects conventional power output end by described resistance R105, the digital signal negative-phase input of described operational amplifier and digital signal output end connect described single-chip microcomputer altogether, the negative voltage input end ground connection of described operational amplifier, the positive voltage input end of described operational amplifier connects operating voltage, described electric capacity C208 is connected between the positive voltage input end of described operational amplifier and ground, described electric capacity C207 is connected between the digital signal positive input terminal of described operational amplifier and ground, electric capacity C205 is connected to described inductive reactance and connecing altogether of current-limiting resistance is held between ground, electric capacity C206 is connected to described inductive reactance and connecing altogether of resistance R105 is held between ground.
5. the current detecting system of GNSS module as claimed in claim 4, it is characterized in that, described first switching tube Q1 is the metal-oxide-semiconductor Q1 with body diode, and the grid of the described metal-oxide-semiconductor Q1 with body diode, drain electrode and source electrode are respectively the control end of the first switching tube Q1, hot end and cold end.
6. the current detecting system of GNSS module as claimed in claim 4, it is characterized in that, described first switching tube Q1 is IGBT pipe Q1, and the grid of described IGBT pipe Q1, drain electrode and source electrode are respectively the control end of the first switching tube Q1, hot end and cold end.
7. the current detecting system of GNSS module as claimed in claim 4, it is characterized in that, described second switch pipe Q2 is the metal-oxide-semiconductor Q2 with body diode, and the grid of the described metal-oxide-semiconductor Q2 with body diode, drain electrode and source electrode are respectively the control end of second switch pipe Q2, hot end and cold end.
8. the current detecting system of GNSS module as claimed in claim 4, it is characterized in that, described second switch pipe Q2 is IGBT pipe Q2, and the grid of described IGBT pipe Q2, drain electrode and source electrode are respectively the control end of second switch pipe Q2, hot end and cold end.
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| CN201520682375.0U CN204903641U (en) | 2015-09-06 | 2015-09-06 | Current detection system of GNSS module |
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| CN201520682375.0U CN204903641U (en) | 2015-09-06 | 2015-09-06 | Current detection system of GNSS module |
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| CN204903641U true CN204903641U (en) | 2015-12-23 |
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Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105116212A (en) * | 2015-09-06 | 2015-12-02 | 深圳市天工测控技术有限公司 | Current detection system of GNSS module and detection method of current detection system |
| CN106066422A (en) * | 2016-08-18 | 2016-11-02 | 中国人民公安大学 | A kind of high-accuracy voltage current sampling system |
-
2015
- 2015-09-06 CN CN201520682375.0U patent/CN204903641U/en not_active Withdrawn - After Issue
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105116212A (en) * | 2015-09-06 | 2015-12-02 | 深圳市天工测控技术有限公司 | Current detection system of GNSS module and detection method of current detection system |
| CN105116212B (en) * | 2015-09-06 | 2018-03-09 | 深圳市天工测控技术有限公司 | The current detecting system and its method of GNSS module |
| CN106066422A (en) * | 2016-08-18 | 2016-11-02 | 中国人民公安大学 | A kind of high-accuracy voltage current sampling system |
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Granted publication date: 20151223 Effective date of abandoning: 20180309 |