Fundamentals and Practices of Sensing Technologies

by Dr. Keiji Taniguchi, Hon. Professor of Engineering University of Fukui, Fukui, Japan

Xií an University of Technology, Xií an, China

Dr. Masahiro Ueda, Professor of Faculty of Education and Regional Studies

University of Fukui, Fukui, Japan

Dr. Ningfeng Zeng, an Engineer of Sysmex Corporation

(A Global Medical Instrument Corporation), Kobe, Japan

Dr. Kazuhiko Ishikawa, Assistant Professor

Faculty of Education and Regional Studies, University of Fukui, Fukui, Japan

 

[Editorís Note: This paper is presented as Part II of a series of chapters from the new book ďFundamentals and Practices of Sensing TechnologiesĒ; subsequent chapters will be featured in upcoming issues of this Journal.]

 

Example 1.7An example of a block diagram for a sensing system using vision sensors and actuators is shown in Fig.1.15.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 


Example 1.8A photograph of 60(GHz) Band Communication System which can use for sensing systems is shown in Fig.1.16.

 

 

 

 

 

 

 


1.1.8 Examples for Sensing Systems

A. Power Train Control for Automotive Engine (13)

From environmental problems, exhaust emissions from automotive engines have to be reduced to lower and lower levels.

For this reason, multiple sensors and actuators are recently used for engine control as shown in Fig.1.17(a).

In this figure, several of sensors are used for measurements such as crankshaft position, intake mass air- flow, manifold pressure, coolant and cylinder head temperatures, and heated exhaust gas oxygen (HEGO, located both before and after the catalytic converter). Furthermore, some of actuators are also used for controls such as throttle valve, exhaust gas recirculation (EGR), ignition plug and fuel injector.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 


Comments

ECU ( Engine Control Unit):

mass air flow sensor throttle valve actuator  fuel injection actuator cylinder head temperature sensor crankshaft position sensor manifold pressure sensor camshaft position sensor and actuator ignition actuator

EGR Exhaust Gas RecirculationactuatorHEGOHeated Exhaust Gas Oxygensensorscoolant temperature sensor

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 


In a gasoline engine, the precise air-fuel ratio (A/F) regulation for emission control is necessary to achieve the high simultaneous conversion efficiencies in the catalytic converter.

Dynamic A/F control, closed-loop regulation of A/F for high catalyst performance, is needed for lower emission control.

Figure 1.17(b) shows the relationships between mean A/F and conversion efficiencies for the hydrocarbon (HC), the oxide of nitrogen () and the carbon mono-oxide(CO).

From this figure, it is evident that precise A/F regulation is needed for this purpose.

 

BSurgical Robot System(14)

A surgical robot system as shown in Fig.1.18 helps to save lives in remote communities, battle fields, disaster-strikes areas, etc..

It consists of a surgical robot, a video camera, communication systems,

an unmanned air vehicle, a surgical console and video monitor, two gasoline generators.

 

 

 

 

 

 

 

 

 

 

 

 

 

 


C. Accelerometer as System- on- Chip System

Figure1.19 (a) shows the electrode configuration of an accelerometer which the changes of a different capacitance with two sets of fixed and movable electrodes are sensed independently(15).

Furthermore, Fig.19 (b) shows the ADXL335 block diagram of the 3-axis accelerometer(16).

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 


1.2†† Transduction Principles for Physical Sensors

1.2.1 Transduction Principles

The most important point in selecting transducers and sensors is based on its transduction principle. Some transduction principles, which are frequently used as transducers or sensors, are shown in the following figures, and their explanations are, also, briefly described as follows:

 

A.Thermo-EMF Transduction

The measurand:, in the case of the small change of temperature , is converted into the change of electro- motive- force (EMF), which is called the active transduction element, as shown in Fig.1.20. Here, wires A and B, are dissimilar materials.

 

 

 

 

 

 

 

 

 


B. ResistiveTransduction

The measurands: ,or in the case of the small change ,orof the force , or pressure , is converted into the change of the resistance of a conductor or a semiconductor as shown in Fig.1.21, which is called the passive transduction element.

C.Relactive Transduction

The measurand: , in the case of the small change of the displacement , is converted into the change , of the AC voltage, as shown in Fig.1.22, through a small change in the relactance between both secondary coils B and C, of a transformer due to a displacement,, while an AC excitation voltage , is applied to the primary coil A, of the transformer. This is a passive transduction element.

 

 

 

 

 

 

 

 

 

 

Fig.1.22Relactive transduction

 
 

 

 

 

 

 

 

 

 

 

 

 

 

 


D.Capacitive Transduction

The measurands: ,, or , in the case of the small change , orof†† the distance ,area orelectrical permittivity , is all converted into the change of the capacitance, as shown in Fig. 1.23, which is, then, a passive transduction element.Acircuit for converting the small change of capacitance into the voltageis, therefore, required as the secondary step.

 

E.Photoconductive Transduction

The measurand: , in the case of the small change ofthe light intensity, is converted into thechange of the current ( number of carriers ( electron-hole pairs) generated) , in a photoconductive p-n junction diode reverse-biased as shown in Fig. 1.24, which is, then, a passive transduction element.

 

 

 

 

 

 

 

 

 


F.Piezoelectric Transduction

The measurand: , in this case of the small change of the mechanical stress , due to tension, or compression forces on a ceramic crystal, is converted into the change in the voltage (electrostatic charge ), as shown in Fig. 1.25, which is, then, an active transduction element.

 

G.Potentiometric Transduction

As shown in Fig. 1.26(a), the measurand: the rotation angle,is converted

into the change in the voltage .

Figure1.26 (b) shows a photograph of a rotary sensor. This sensor is used for animal robot, switch for automotive, motor drive unit, radio control equipment, car audio (navigation system, changer), etc..

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 


These details mentioned above will be described in chapter 2.

 

1.2.2†† Relationship between Measurement Object and Sensing Device

Figure 1.27 shows the relationship between measurement objects and sensing devices.

 


 

 

 

 

 

 

 

Fig.1.27†† Relationship between interested objects and sensing devices

 

 

 
 

 

 


The elements numbered by,,,, and express energy sources,interested objects, preprocess operation, measurands, and sensing devices, respectively. Some preprocesses are required for the effective extraction of the measurands from an interested object. We show here such an example. For example, the important points shown in example1. 1(See Fig. 1. 4), are as follows:

(1) The selection of DC and RF current sources.

(2) For obtaining higher sensitivity, the optimal design of an orifice in the flow

chamber as shown in Fig. 1.28. This figure shows us thatin location, white

blood cells flow randomly, butin location , they flow with continuously some

spaced intervals along the center of stream line.

This method is well known as sheath flowing techniques.

(3) A chemical processing for extracting efficiently measurands from the interested objects. This technique is shown in Fig.1.8.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 


1.2.3Configurations of Transducers and Sensors

Figure1.29 shows the relationship between a measurand and an active transducer, where no power supply is required. The thermocouple is a representative example (See Fig.2.3).

Fig. 1.29†† Configuration of an active transducer

 
 

 

 

 

 

 

 


B. Passive Transducer

Figure 1.30 shows the relationship between a measurand and a passive transducer, where a power supply is required for the conversion into a voltage. The representative exampleis a resistive temperature transducer used as a transduction element(See Fig. 2.7).

 

 

 

 

 

 

 

 

 

 


1.2.4†† Active and Passive Sensors

A.Active Sensor

Figure 1.31 shows the relationship between a measurand and an active sensor, where no power supply is required for a transduction element. The representative examples are a diaphragm used as a sensing element and a piezo electric element used as a transduction element (See Fig. 3.16).

 

 

 

 

 

 

Fig. 1.31 Configuration of an active sensor

 

 
 

 

 


B. Passive Sensor

Figure 1.32 shows the relationship between a measurand and a passive sensor, where a power supply is required for a conversion. The representative examples are a diaphragm used as a sensing element and a relactive element used as a transduction one (See Fig. 2.14).

 

 

 

 

 

 

 

 

 

 

 

 

Fig. 1.32 Configuration of a passive sensor

 
 

 

 

 


1.2.5 ††Example of Photo Sensing System (6 ), (17) ,(18)

Figure 1.33 shows the configuration of an automated hematology analyzer using a laser diode as a light generation source and two photodiodes as sensing devices.

In this figure, a mechanism of the generation of sheath flow is shown in Fig. 1.28.

Figure 1.34 shows the scattering models of laser beam caused by a white blood cell. Some definitions used in Fig.1.35 are shown in Fig.1.34.

By using the method shown in Fig.1.7, white blood cells are measured by using the photodiode-sensors set-up in the following different channels.

Figure 1.35 shows the two- dimensional scatter-grams for WBC five differential

counts.

(1) In the DIFF channel, lymphocytes, monocytes, eosinophils ,and

eutrophils+basophils are clustered by the chemical processing using the reagent 1,

and then they are measured by the intensity of the forward high diverge

scattering beam which depends on the inner structure of the white blood cell, and

the intensity of the forward low diverge scattering beam which depends on the

diameter of the white blood cell . They can be, then ,classified and counted from the

WBC/DIFF scatter-gram shown in Fig.1.35(a).

(2) In the WBC/BASO channel, basophils are separated from red cell ghosts and

other white blood cells by the chemical processing using the reagent 2.

As a result, the normal white blood cells are classified into five categories: neutrophils, eosinophils, basophils, lymphocytes and monocytes, as is shown in Fig.1.35.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 


1.3†† Radar Sensors

1.3.1†† Outlines of Radar Sensors

Radar (radio detection and ranging) sensors including sonar (sound navigation and ranging) sensors can determine the range, velocity, and direction of an object.

There are two types of radar sensors:active radar sensors and passive ones.

Firstly, we deal with the active radar sensors. An active radar sensor which radiates a beam of radio wave energy toward the object, receives an echo signal from the object and analyzes its echo signal.

There are three types of radio wave radiations: the pulse modulated wave radiation, the continuous wave (CW) radiation, and the frequency modulated wave radiation.

1.3.2†† Pulsed Radar Sensors (19)

Figure 1.36 (a) shows a block diagram of the pulsed radar sensor. It consists of a transmitter, an antenna, a transmit/receive electronic switch (T/R switch), a receiver, and a PPI (plan position indication) display scope.

The operation of this sensor is as follows:

(1) The transmitter sends a narrow width pulsed RF power signal from the antenna toward the object.

(2) The receiver receives the echo signal from the object, and the echo signal is, finally, displayed on the PPI scope after a proper signal processing.

Fig.1. 36(b) shows the relationship between the transmitting signal and its receiving signal.

A range for the object location can be determined by measuring a round-trip time of the transmitting signal. The range is expressed as follows:

†††††††††††††††††† (1.4)

where , andare the velocity of propagation of the transmitting signal, and

the round-trip time for the transmitting signal, respectively.

For the radio wave propagation in a vacuum, is approximately,

whereas for acoustic wave radiations, is approximately in air,

and in water.

Next, we will describe several items which express abilities of radar sensors.

(1) The range resolution between two objects, satisfies a following relation:

††††††††††    (1.5)

where is the pulse width of the transmitting signal.

(2) The smallest range satisfies the following relation, as is evident from

Fig. 1. 36(b):

†††††††††    (1.6)

where is the pulse width of the transmitting signal.

(3) The maximum range satisfies the following relation:

††††††††††††††††††††††††††††††††††††††† †††††††    (1.7)

where is the pulse repetition period of the transmitting signal.

(4) The detectable maximum range is expressed as follows:

,†† ††††(1.8)

where is the transmitting average power, is the transmitting peak power,isthe minimum receivable power, is the wavelength of the transmitting signal ,is the effective diameter of the antenna , is the effective area of the antenna†† , is the efficiency of the antenna , andis the radar cross section of the object.(See Ref. (1),p.29.16).

For example, the radar cross section is approximately for the large spherical object with the radius of .

The derivation of Eq.(1.8) is described in problem 1.3.

Example 1.9 Determine the rangebetween the object and the radar sensor, when the round-trip time of a pulsed radar is .

Using Eq.(1.4),

 

Example1.10In the pulsed radar sensor shown in Fig. 1.36, we let

, , , , .

Determine the following values:

(1) , (2) ,(3)Noise level: , (4) ††(5) ,(6),

where,,

,,.

(1),(2),

(3) ,

(4),

(5)

(6)

In the modulator shown in Fig. 1.37 (a), the carrier waveform, the modulation waveform, and the modulated waveform are shown in Figs. 1.37 (b), 1.37(c), and 1.37(d), respectively.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 


Figure 1. 37(e) is the angular frequency spectrum of the modulated waveform shown in Fig.1.37(d). The angular frequency in the continuous carrier wave is:

carrier wave frequencyas is evident from Fig.1.37(a). The angular frequency spectrum of modulated wave has, however the wide range of the spectrum for the pulsed modulation, as shown in Fig. 1.37(e).

The relationship between the modulated signal and its Fourier transform

is expressed as follows:

Example1.11Find the Fourier transform of ,and .

Changing to , we obtain .

 

Example1.12Find the Fourier transform of .

Using the Eulerís formula: , and the results of

Example 1.11,we obtain the following relation:

 


1.3.3†† Continuous Wave (CW) Radar Sensor (19)

Figure. 1.38 shows a simplified block diagram of a CW radar sensor.When the transmitting signal with the carrier frequency is radiated on the object moving with the speed of , the frequency of the echo signal is shifted to(+ sign expresses the approached direction to the radar sensor).††

In this situation, the Doppler frequency shift is expressed as follows:

 (1.9)

where is the speed of propagation of the carrier wave.

 

Example 1.13When , ,†† determine which is the speed of an object.

Using Eq. (1.9),

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 


1.3.4†† FM Radar Sensor (19)

The CW radar sensor described previously, canít measure the range between the object and the radar sensor. For a solution of this problem, the frequency of carrier wave is varied as a function of the time in a FM-CW radar sensor.

The block diagram of the FM-CW radar sensor is shown in Fig. 1.39, and the relationship between the transmitting signal and the receiving signal are also shown in Fig.1.40, respectively. Figure.1.40 (a) shows the frequency variation in the case that the object is moving with the speed of. The transmitting frequency with up chirp is linearly increased as a function of time, and after that, the transmitting frequency with down chirp is linearly decreased as the function of time, as is shown in this figure.

The details described above are explained as follows:

(1) The frequency of the carrier wave in the FM-CW radar sensor is expressed as a function of the time in the following form:

where is a constant and is the time.

(2) The values is†† the maximum frequency shifts due to a maximum voltage swing values of as shown in Fig. 1.40 . The value is the repetition period of a triangular wave for the FM modulation.

(3) The receiving signal is expressed as:.

(4) The value is the time, when the difference between the transmitting frequency and the receiving frequency equals to

, i.e.,.

(5) The values , andshown in Fig. 1.40(a),are expressed as follows:

, and .

The range between the object and the radar sensor is, then, expressed as

follows:

††† (1.10)

In the case of the object moving with a speed of, as shown in Fig. 1.40(b),

the relationship between the transmitting and receiving frequencies is expressed as follows:

(6) Up chirp frequency:

(7) Down chirp frequency:

(8) From (5), (6), and (7) described above, the range between the object and the radar sensor, is expressed as follows:

 ††††††††† (1.11) 

(9)Doppler frequency: ††† (1.12) 

(10) Speed of the object:,    (1.13) 

Example 1.14In the FM-CW radar sensor shown in Fig. 1.39, we let

,,.

Then we obtained following data: ,.

Determine the range between the object and the radar sensor, and the speed of the object.

From Fig.1.40 (a), . Using Eq. (1.11),

.

Using Eq.(1.12), . Using Eq.(1.13),

., .

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 


1.3.5 ††Examples of Radar Sensors for Automotive Use (20)

Radio waves, infrared rays, ultrasonic waves, and visible light rays are used as energy sources in the sensing systems for automotive uses.

Figure. 1.41 shows an example of the architectures of automotive wave sensors for holding securely cars from collisions. 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 


:Long range sensor using a carrier frequency

of 77(GHz).

Maximum range is approximately 150(m).

:Infrared sensor.

 Maximum range is approximately 120(m).

:Image sensors.

Maximum range is approximately 80(m).

:Short range sensors using a carrier frequency

of 24(GHz).

Maximum range is approximately 20(m).

:Sonar sensors, (Maximum range is approximately 3(m))

Details are described in Chapter 3.

 

Fig. 1.41 Architectures of wave sensors for holding securely cars from collisions(17)

 

 
 

 

 

 


References:

(13) J.A.Cook,D.McNamara,K.V.Prasad:Control, Computing and Communications:

Technologies for the Twenty-First Century Model T, Proceedings of the IEEE,

Vol.95, No.2, pp.334-355 (2007)

(14) J.Rosen, B. Hannaford : DOC at a DISTANCE, IEEE Spectrum,pp.28-33 (Oct.,2006)

(15) O.Brand: Microsensor Integration Into Systems-on-Chip, Proceedings of the

IEEE , Vol.94, No.6, pp.1160-1176 (2006)

(16) Datasheet, ADXL-203, Analog Devices, Norwood, MA(2004).[Online], Available:

http://www.analog.com/imems

(17)Overview of Automated Hematology analyzer SF-3000TM,Product Development

Division, Sysmex Corporation, Sysmex Journal,Vol.18, pp.11-22(1995)

 



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