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        Development and Test of Software Method to Achieve Constant-Temperature-Difference Control for Thermal Wind Sensor*

        2016-11-08 09:25:12WANGFangQINMing
        傳感技術(shù)學(xué)報(bào) 2016年10期
        關(guān)鍵詞:熱式王芳東南大學(xué)

        WANG Fang,QIN Ming

        (Key Laboratory of MEMS of Ministry of Education,Southeast University,Nanjing 210096,China)

        Development and Test of Software Method to Achieve Constant-Temperature-Difference Control for Thermal Wind Sensor*

        WANG Fang,QIN Ming*

        (Key Laboratory of MEMS of Ministry of Education,Southeast University,Nanjing 210096,China)

        A software method for controlling constant temperature difference(CTD)mode for the thermal wind sensor has been presented.As control unit,MCU is utilized to sample ambient temperature and chip temperature and adjust the power for output in order to maintain the state of CTD.The experiment shows that by means of the software method for control,the thermal wind sensor could almost maintain the output constant during the temperature range from-20℃to 40℃.Besides,it can measure the wind speed during 0~20 m/s with relative error less than 8%which has a response speed of less than 15 seconds.

        MEMS;thermal wind sensor;CTD mode;MCU control

        EEACC:11222doi:10.3969/j.issn.1004-1699.2016.10.002

        A thermal wind sensor which usually consists of heaters and temperature sensitive elements measures wind speed by monitoring the change of thermal field induced by an airflow that passes along the chip[1-3].The thermal field is generated by heaters that work on constant-temperature-difference(CTD)mode or constant-power(CP)mode.Nowadays,the CTD mode is utilized widely.By making use of an additional resistive temperature sensor,the average temperature of the thermal wind sensor is kept a constant temperature above the ambient temperature ensuring the output is independent of the ambient temperature so that it can solve the problem of temperature drift and has a large measurement range theoretically[4-5].

        On CTD mode,the wind sensor system has to sample chip temperature Thand ambient temperature Taconsecutively and calculate the difference between the chip temperature and the ambient temperature[6]and compareΔT with the defaultΔT0in order to adjust the heating power for a CTD state.However,the temperature drift is a key factor affecting the performance of the wind sensor system[6].The temperaturecompensation methods for CTD mode are divided into three categories.One is to improve the temperature compensation circuit[7-10].In 2010,Christoph Sosna and his partners proposed a circuit with two Wheatstone bridges which could maintain the temperature difference between the chip and the environment and has a preferable performance[7].The second method is to revise the structure and the fabrication of the wind sensor chip which is a fundamental method to improve the property of the wind sensor system but is not enough for improvement,such as manufacturing some pendent structures[9-13].And the third is to use some modeling methods to compensate the output.This method is effective but has a complex procedure and needs too much compute[14].In this paper,another method to realize CTD control has been proposed.MCU,which was utilized as the main unit,aided by peripheral circuits can achieve the purpose of CTD control,for it has reduced as many components as possible which is an important factor attributing to the temperature drift.Besides,it allows the temperature sensors including chip temperature sensor and ambient temperature sensor have different resistances and different temperature coefficient of resistance(TCR)favorable for manufacture.

        1 Principle and System Scheme of Thermal Wind Sensor System

        A software method has been developed to make the sensor work on CTD mode and then complete one dimensional wind velocity measurement.The main procedure is presented below:①Sampling the signals from chip temperature sensor and environment temperature sensor;②Calculating the amount of regulation according to the difference between sampleΔT and defaultΔT0,and theΔT is equal to the difference between chip temperature and ambient temperature;③Outputting the heating power.

        All these functions above are controlled by MCU.And in order to fulfill these functions,the system is designed from two parts-hardware module and software module.

        1.1Hardware module

        The hardware module is divided into five sections covering power section,heating control section,MCU processing section and the thermal wind sensor chip.The schematic diagram is as follows.

        Fig.1 Schematic diagram of thermal wind sensor system which works on CTD mode controlled by software

        The thermal wind sensor chip is a one dimensional wind speed sensor chip containing two metal resistors,of which one called Ramonitors the ambient temperature and the other called Rhis heated to form thermal field and also senses the chip temperature.In order to avoid the self-heating influence of Ra,the current through Rashould be small enough.The resistance and TCR of Raand Rhcan be measured through experiment.

        1.1.1Information collection section

        In this paper,a subtraction circuit has been applied as a signal processing circuit in consideration of the level mismatching between the output of resistive temperature sensors and the sampling scale of MCU.Through the circuit,the difference between the power voltage and the sample signal is served as the input to MCU for post compute.The diagram is showed in Fig.2.

        1.1.2Heating control section

        For thermal wind sensor system in this paper,the heating control circuit regulates the heating power by changing current through the heater Rh.The heating circuit is a constant current source circuit capable of amplifying the current outputted from MCU with the purpose of providing larger power for Rh.As is show in Fig.2,the amplifying factor can be adjusted by changing the ratio between resistors R10and R11.Besides,with the current configured by MCU and the voltage sampled by information collection section,the temperature of the heater can be obtained.

        1.2Software module

        The main part of software module is coding the control program for MCU.The software flow chart is showed in Fig.3.

        Fig.2 Interface circuit of thermal wind sensor system which includes three parts-simplified sensor structure diagram(No.1),information collection section(No.2)and heating control section(No.3).

        Fig.3 Software flow chart of CTD mode control.

        1.2.1Temperature calculation

        The resistances of Raand Rhare dependent on the environment temperature.TCR is a coefficient reflecting this phenomenon.The relation of TCR,resistance and temperature can be presented as follow:

        WhereR1andR2are values of the same resistor at different environment temperatures ofT1andT2respectively.Andα1is TCR of the resistor showing the change of resistance induced by ambient temperature.For metal material,α1is positive.During normal temperature range,the relationship between resistance and temperature is linear.Owing to this linear relationship,MCU can calculate current temperature of the chip and the environment on the basis of the formula below.

        WhereUis the voltage on the heater or the temperature sensor at the temperature ofT2,and I is corresponding current.R1is the resistance at the temperature ofT1.

        1.2.2CTD control

        In order to obtain accurate chip temperatureThand ambient temperatureTa,a filter has been used and the sample data have been averaged.After getting accurateThandTa,the regulating factoradjis concluded by comparing default value with the calculated differenceΔT.The factor adj can be computed as follows:

        Where k is a factor to control the response speed.It may been set different values at different situations in case of current overshoot of the circuit.

        2 Experiment and Results

        Measurement of resistance and TCR of the heater and the temperature sensor has been conducted and the heater is 99.158Ω of which TCR is 0.003 08/℃at room temperature.For the temperature sensor,the resistance is 2.3 kΩand its TCR is 0.002 51/℃.

        To test the operation of the thermal wind sensor,wind speed experiment and static property experiment have been performed.

        Wind speed measurement was done with the wind sensor in a wind tunnel capable of setting the flow rate of air,which has then been measured with the thermal wind sensor.

        This experiment has been repeated three times and the results are showed in Fig.4 and Fig.5.These figures display that the presented wind sensor system is working well during the wind range from 0 m/s to 20 m/s with accuracy of less than 0.5 m/s.Its relative error is less than 8%when wind speed is lower than 10 m/s and 4%at a wind speed higher than 10 m/s.

        Fig.4 Relationship between wind speed tested by the thermal wind sensor and wind speed set by the wind tunnel

        Fig.5 Relative error of the output of the thermal wind sensor at different wind speed

        Fig.6 shows the result of response speed experiment,which illustrates that the output reaches a stable value in 15 seconds after wind speed changed.The figure also shows that there is inconformity between different wind curves,which is induced by experiment methods.For the wind speed was changed gradually by manual operation,the time that flow rate of air in the wind tunnel need to change and reach steady state can not be the same in multiple operations and then the difference of response speed between different wind curves appeared.This phenomenon can be promoted in future experiment by adjusting experimental operation.

        Fig.6 Output of the thermal wind sensor changes with time when wind in the environment changes

        The test about static property of the wind sensor system has been done in the climate chamber.With the help of the climate chamber,the air temperature was varied from-20℃ to 40℃.The result showed that the static output is almost independent on the air temperature.The deviation observed here is in the range of 0.4 m/s caused by the climate chamber which has air flow when changing the air temperature in it(Fig.7).

        Fig.7 The relationship between the output of the thermal wind sensor and the ambient temperature when there is no wind in the environment

        3 Conclusion

        The software method for CTD control of the thermal wind sensor has been developed in this paper.Experiments show that this method can maintain the CTD mode of the wind sensor which can reduce the temperature drift effectively.This wind sensor system can also monitor wind speed from 0 m/s to 20 m/s in less than 20 seconds with accuracy of less than 0.5 m/s.This method has less limit to the material of temperature sensitive resistors and also reduces the scale of the peripheral circuit.The wind sensor can have greater performance by improving the algorithm and test methods.

        [1]Van Oudheusden B W.Silicon Fow Sensors[J].Control Theory and Application,IEE Proceedings,1988,135(5):373-380.

        [2]Li Wei,Li Jiechao,Yan Weiping.Performance Analysis of Thermal Micro Flow Sensor Above Room Temperature[J].Chinese Journal of Sensor and Acturators,2015,28(2):160-164.

        [3]Zhao Weiguo,Song Zhihuan,Huang Zhenwei.Thermal Gas Flow Measurement Based on Single Sensor[J].Chinese Journal of Sensor and Acturators,2009,22(3):442-446.

        [4]Cheng Haiyang,Qin Ming.Study on the Controlling and Measring Circuits of the Two Dimensional CMOS Silicon Wind Sensor[J].Micronanoelectronic Technology,2004(6):38-43.

        [5]Que Ruiyi,Zhu Rong,Zhen Weiqing,et al.Temperature Compensation for Thermal Anemometers Using Temperature Sensors Independent of Flow Sensors[J].Meas Sci Technol,2011,22(8):1312-1327.

        [6]Chen Bei,Zhu Yanqing,Yi Zhenxiang,et al.Temperature Effects on the Wind Direction Measurement of 2D Solid Thermal Wind Sensors[J].Sensors,2015,15(12):29871-29881.

        [7]Sosna C,Buchner R,Lang W.A Temperature Compensation Circuit for Thermal Flow Sensors Operated in Constant-Temperature-Difference Mode[J].IEEE Trans Instrum Meas,2010,59(6):1715-1721.

        [8]Nam T,Kim S,Park S.The Temperature Compensation of a Thermal Flow Sensor by Changing the Slope and the Ratio of Resistances[J].Sensors&Acturators A Physical,2004,114(2-3):212-218.

        [9]Dijkstra M,Lammerink T S J,De Boer M J,et al.Thermal Flowsensor Drift Reduction by Thermopile Voltage Cancellation via Power Feedback Control[J].J Microelectromech Syst,2014,23(4):908-917.

        [10]Bruschi P,Dei M,Piotto M.An Offset Compensation Method with Low Residual Drift for Integrated Thermal Flow Sensors[J].IEEE Sensors J,2011,11(5):1162-1168.

        [11]Zhu Yanqing,Chen Bei,Qin Ming,et al.2-D Micromachined Thermal Wind Sensors-A Review[J].IEEE Internet Things J,2014,1(3):216-232.

        [12]Dong Ziqiang,Huang Qingan,Qin Ming.Thermal Asymmetry Compensation of a Wind Sensor Fabricated on Ceramic Substrate[J].IEEE,2010,143(2):595-599.

        [13]Van Oudheusden B W,Herwaarden A W V.High-Sensivity 2-D Flow Sensor with an Etched Thermal Isolation Structure[J].Sensors&Actuators A Physical,1990,22(1-3):425-430.

        [14]Huang Qingan,Chen Bei,Zhu Yanqing,et al.Modeling of Temperature Effects on Micromachined Silicon Thermal Wind Sensors[J].J Microelectromech Syst,2015,24(6):2033-2039.

        王芳(1991-),女,碩士研究生,東南大學(xué)MEMS教育部重點(diǎn)實(shí)驗(yàn)室,主要從事傳感器系統(tǒng)信號(hào)檢測與控制方面的研究;

        秦明(1967-),男,博士生導(dǎo)師,教授,博士,東南大學(xué)MEMS教育部重點(diǎn)實(shí)驗(yàn)室,從事CMOS兼容MEMS熱式風(fēng)速風(fēng)向傳感器、CMOS集成濕度傳感器、CMOS氣壓傳感器等項(xiàng)目的研究,mqin@seu.edu.cn。

        熱式風(fēng)速計(jì)恒溫差控制的軟件實(shí)現(xiàn)及其性能測試*

        王芳,秦明*

        (東南大學(xué)MEMS教育部重點(diǎn)實(shí)驗(yàn)室,南京210096)

        介紹了一種利用軟件實(shí)現(xiàn)熱式風(fēng)速風(fēng)向傳感器恒溫差模式(CTD)控制的方案。傳感器系統(tǒng)采用單片機(jī)作為主控單元,對芯片溫度和環(huán)境溫度進(jìn)行采樣,并以此為依據(jù)調(diào)節(jié)輸出功率,從而實(shí)現(xiàn)恒溫差狀態(tài)的控制。實(shí)驗(yàn)表明,采用這種軟件控制方案,在無風(fēng)狀態(tài)下,在-20℃到40℃的環(huán)境溫度變化范圍內(nèi),熱式風(fēng)速風(fēng)向傳感器能夠基本維持輸出信號(hào)恒定不變。除此之外,該風(fēng)速風(fēng)向傳感器系統(tǒng)還可以實(shí)現(xiàn)對0~20 m/s風(fēng)速范圍內(nèi)的風(fēng)速測量,最大測量誤差不超過8%,并且具有低于15 s的響應(yīng)速度。

        MEMS;熱式風(fēng)速計(jì);CTD模式;單片機(jī)控制

        TN409

        A

        1004-1699(2016)10-1478-05

        2016-05-16修改日期:2016-06-25

        項(xiàng)目來源:國家高技術(shù)研究發(fā)展計(jì)劃項(xiàng)目(2013AA041106)

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