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Collision avoidance radar operated LC substrate based MSP antenna in vehicular systems

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This paper deals with the collision avoidance radar based antenna performance characteristics. This antenna can be placed inside the vehicle and it receives the signals from the base station and warns the driver accordingly. If any accident occurs to that vehicle, then that information is also passes to substation for help. The proposed antenna is designed on liquid crystal substrate and all its output parameters are simulated and presented in this work.

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Collision Avoidance Radar Operated LC Substrate based MSP Antenna in Vehicular Systems

1

1 Department of ECE, K L University, Guntur DT, AP, India 2

Head of the ECE Department, DJR IET, Gudavalli, AP, India

Email: madhav.mtech@gmail.com

Abstract: Road safety and precautionary measurement based instruments became part and parcel of the modern

vehicular systems Collision avoidance helps to prevent the vehicles from accidents and from unnecessary collision

while the driving When vehicle is moving with high speed and if any obstacle suddenly appears, it is very difficult to

control the vehicle If we design a system with the support of base station then we can warn the driver about the

accident occurred nearer to his way and about traffic jams etc This paper deals with the collision avoidance radar

based antenna performance characteristics This antenna can be placed inside the vehicle and it receives the signals

from the base station and warns the driver accordingly If any accident occurs to that vehicle, then that information

is also passes to substation for help The proposed antenna is designed on liquid crystal substrate and all its output

parameters are simulated and presented in this work

Keywords: Collision Avoidance, LC Substrate, MSP Antenna

1 Introduction:

Collision Avoidance System is a technology which

helps in avoiding vehicle collisions Various factors

to be taken in to consideration are Velocity of the

vehicle, direction of travel, acceleration of the

vehicle, steering angle and Yaw – rate The system

identifies a potential collision and gives warning

signal to the driver of the automobile This system is

a real – time system in which the radar to sends a

sonar signal It identifies any kind of obstacles in the

track of the vehicle Sensors are placed in the vehicle

to identify or sense the speed of the vehicles on either

side Antennas are used on the vehicle to send and

receive the signals [1-3]

The Collision Avoidance System identifies a

threat of collision well in advance depending on the

distance The distance may be user defined during the

process of design A warning signal is issued to

caution the driver to avoid the collision If the

situation goes out of control of the driver, another

system can be enforced to take the control over the

vehicle to avoid collision or mitigate the collision as

a final option which can be called an over – ride

system

In case of warning, the radar senses the obstacle in

the track followed by the vehicle and estimates the

distance Depending on the distance it warns the

driver [4] This warning can be issued by a warning

system which alerts the driver like alarm or an LED

After issue of the warning signal, the Collision

Avoidance depends on the response time or the

reaction time of the driver and the time taken for the

vehicle to decelerate or brake

The reaction time of the driver depends on various factors like the condition of the driver, reflexes of the driver, his attitude and behavior, his habits, his work stress of the day and his moods The braking time depends on the condition of the vehicle, brake efficiency, the traction of tyres and the kinematics of both the vehicles under collision [5-6]

Sensors are placed in the vehicle to identify or sense the speed of the vehicles on either side The sensors may be color video cameras and the ERIM

3-D laser range finder The major disadvantage of these systems is these are generally not very well suited for

a quick reaction to unexpected obstacles Especially

in the case of collision avoidance, a sensor is needed that can supply the relevant information fast with little data processing overhead and interact with actuators at the level of the vehicle controller

Sensors that satisfy these requirements are for example sonars, infrared sensors, pulsed 1-D laser range finders or microwave radar Compared to light based sensors Sonars have the advantage that they

do not get confused by transparent or black surfaces

On the other hand, the wavelength of ultrasound is much larger than the wavelength of lights Therefore, unless the transducer faces the reflector surface in a normal direction, only rough surfaces or edges can reflect sound waves Outdoor surfaces almost always have a type of surface roughness that enables sonar to detect the object It was therefore decided to use sonar sensors for the collision avoidance system of the vehicle [7-8]

The position of the vehicle is estimated relative to some initial point The distance travelled is provided

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by an optical encoder on the drive shaft and vehicle

orientation in 3-D space is provided by the gyroscope

of an inertial navigation system The measurements

are combined to give the x-y position and orientation

of the vehicle with respect to the world coordinates

Figure (1) Collision avoidance communication system

Figure (2) Nearer view of the system fitted in bayonet

2 Properties of Liquid crystals:

LCs is an anisotropic material showing both

properties of a crystal and a liquid All further

explanations are related to nematic LCs which shows

up to now the best dielectric properties at microwave

and millimeter-wave frequencies LC can be

processed around 300°C, has excellent electrical

properties, very low moisture absorption, light

weight, mechanical stiffness, thermal stability (CTE

= 0 to 30 ppm/°C), chemical resistance Depending

on the temperature, LC phase exists in a mesophase

between a crystalline solid and an isotropic liquid In

this state, the material can flow like a liquid but at the

same time, molecules have orientational order The

size of the molecule is typically a few nanometers

For this configuration, the electrical parameters of the

LCs are defined as ε┴ and tan δ┴ The molecules can

be rotated parallel to the RF field by applying a

voltage between the conductors in order to create an

electrostatic field in the LCs, thus changing the value

of the permittivity and loss tangent to ε║ and tan δ║

respectively

3 Results and Discussion:

Freq [GHz]

-35.00 -30.00 -25.00 -20.00 -15.00 -10.00 -5.00 0.00

Ansoft Corporation Return Loss Patch_Antenna_ADKv1

m 1

Curve Info dB(St(1,1)) Setup1 : Sw eep1 Name X Y

m1 23.8191 -34.7835

Figure (3) Return loss Vs Frequency Return Loss is a parameter which indicates the amount of power that is “lost” to the load and does not return as a reflection Figure (3) shows the return loss curve of the proposed antenna A return loss of -34.78dB is obtained at the desired frequency and it is acceptable return loss of <-10dB The input impedance of an antenna is defined as “the impedance presented by an antenna at its terminals or the ratio of the voltage to the current at the pair of terminals or the ratio of the appropriate components

of the electric to magnetic fields at a point” Hence the impedance of the antenna can be written as Zin =

Rin + jXin.Where Zin is the antenna impedance at the terminals, Rin is the antenna resistance at the terminals, Xin is the antenna reactance at the terminalsFigure (4) shows the input impedance smith chart rms of 0.74 and bandwidth enhancement of 0.87% is attained from the current model

5.00 2.00 1.00 0.50 0.20

5.00

-5.00 2.00

-2.00 1.00

-1.00 0.50

-0.50

0.20

-0.20 0.00

10 30 50 70 90 100 120

140

160

180

-170

-150

-130 -110 -90 -80 -60 -40 -20

Ansoft Corporation Input Impedance Patch_Antenna_ADKv1

Curve Info rms bandw idth(1, 0) St(1,1)) Setup1 : Sw eep1 0.7458 21.1832

Figure (4) Smith chart Gain is a measure of the ability of the antenna to direct the input power into radiation in a particular direction and is measured at the peak radiation intensity Figure (5) shows the gain curve and a typical gain of 17.71dB is obtained from the current antenna The gain value is showing very high compared to the normal antenna The high gain can

be obtained with array models but here with single patch itself we obtained higher gain

-200.00 -150.00 -100.00 -50.00 0.00 50.00 100.00 150.00 200.00

Theta [deg]

-30.00 -20.00 -10.00 0.00 10.00 20.00

Ansoft Corporation ff_2D_GainTotal Patch_Antenna_ADKv1

dB(GainTotal) Setup1 : LastAdaptive dB(GainTotal)_1 Setup1 : LastAdaptive

Name X Y m1 12.0000 17.7160

Figure (5) gain

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Figure (6) rE-phi in 3D view Besides the reflection and mutual coupling

coefficients, the far-field radiation pattern is one of

the most important parameters in antenna design

Figure (6) and (7) shows the radiation pattern of the

antenna in phi and theta directions in three

dimensional views

Figure (7) rE-theta in 3D view

Figure (8) LHCP Curve in 3D View The directivity is indicated by both the distance from

the origin in the particular direction (defined by the

angles of azimuth phi and the zenith angle theta) and

the directivity surface color Figures (8) and (9) show

the directivity for the left and right circularly

polarized components of the receive antenna

far-field

Figure (9) RHCP Curve in 3D View

The axial ratio quantifies the polarization quality for

a circularly polarized antenna Circular polarization is specified by its sense (left-hand or right-hand) and by its axial ratio The axial ratio is the ratio of the maximum to minimum response to a linear signal of any orientation and is commonly expressed in dB

Figure (10) shows the axial ratio of the antenna in three dimensional view The inherently antenna radiates elliptically polarized waves Linear polarization being a particular case of it The elliptical polarization is characterized by three quantities: axial ratio, tilt angle and the sense of rotation

Figure (10) Axial Ratio in 3D View For linear polarization, the axial ratio is zero or infinite while the tilt angle gives its orientation

Circular polarization is obtained for unit axial ratio, where the tilt angle losses its meaning Thus the quality of circularly polarized wave is determined by the axial ratio

Figure (11) Polarization in 3D View Directivity is a measure of the concentration of radiation in the direction of the maximum Directivity and gain differ only by the efficiency, but directivity

is easily estimated from patterns Figure (12) shows the directivity of the antenna in 3D view

Figure (12) Directivity in 3D View

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10.00 15.00 20.00 25.00 30.00 35.00 40.00

Freq [GHz]

0.00

10.00

20.00

30.00

40.00

50.00

60.00

70.00

80.00

90.00

Ansoft Corporation XY Plot 1 Patch_Antenna_ADKv1

m 1

Curve Info VSWRt(coax_pin_T1) Setup1 : Sw eep1 Name X Y

m1 23.8191 1.0371

Figure (13) VSWR Vs Frequency VSWR is a measure of impedance mismatch between

the transmission line and its load The higher the

VSWR, the greater is the mismatch The minimum

VSWR which corresponds to a perfect impedance

match is unity Figure (13) shows the VSWR Vs

frequency curve and VSWR of 1.03 is obtained from

the current model

4 Conclusion:

High gain antenna was designed and simulated for

collision avoidance radar based operation for

vehicular systems This antenna will be worthwhile

for getting information from base station and with the

help of advanced circuitry for desired operation

Maximum gain of 17dB and bandwidth up to 0.87%

enhancement can be obtained from the current model

All the parameters presented in this work are

showing the applicability of this antenna in the

collision avoidance system With the help of other

intelligence circuitry the speed of the vehicle and

breaks can be controlled

5 Acknowledgments:

The authors like to express their thanks to the

management of KLU and Department of ECE for

their support and encouragement during this work

Further, VGKM Pisipati acknowledges the financial

support of Department of Science and Technology

through the grant No.SR/S2/CMP-0071/2008

References:

[1] “A New Threat Assessment Measure for Collision

Avoidance Systems” by Yizhen Zhang, Erik K Antonsson

and Karl Grote (°c 2006 California Institute of Technology

Patent Pending, Serial # 60/798,516 All rights reserved.)

[2] “Sonar based Outdoor Vehicle Navigation and Collision

Avoidance” by Dirk Langer and Charles Thorpe The

Robotics Institute Carnegie Mellon University Pittsburgh,

PA 15232 (IROS '92)

[3] Economou, L & Langley, J (1998) Circular microstrip

patch antennas on glass for vehicle applications IEE

Proceedings Microwaves, Antennas and Propagation, 145

(5), pp.416-420

[4] Hoare, E & Hill, R (2000) System requirements for

automotive radar antennas In: IEEColloquium on Antennas

for Automotives pp.1/1-111

[5] “Collision Avoidance for Vehicle-Following Systems”

by Stefan K Gehrig and Fridtjof J Stein IEEE TRANSACTIONS ON INTELLIGENT TRANSPORTATION SYSTEMS, VOL 8, NO 2, JUNE

2007

[6] Low, L., Langley, R., Breden, R & Callaghan, P

(2006) Hidden Automotive Antenna Performance and Simulation IEEE Transactions on Antennas and Propagation, 54 (12), pp.3707-3712

[7] Sulic, E., Pell, B., John, S., Gupta, R., Rowe, W., Ghorbani, K & Zhang, K (2010) Deformation Evaluation

of Embedded Antennas in Vehicular Components In:

Proceedings of the World Congress of Engineering 2010

London, UK, pp.2389-2394

[8] Toriyama, H., Ohe, J., Kondo, H & Yotsuya, H (1987) Development of printed-on glass TV antenna system for

car In: 37th IEEE Vehicular Technology Conference, 1987

pp.334-342

Authors Biography

B.T.P.Madhav was born in India, A.P, in 1981 He

received the B.Sc, M.Sc, MBA, M.Tech degrees from Nagarjuna University, A.P, India in 2001, 2003, 2007, and

2009 respectively From 2003-2007 he worked as lecturer and from 2007 to till date he is working as Assistant Professor in Electronics Engineering He has published more than 55 papers in International and National journals

His research interests include antennas, liquid crystals applications and wireless communications

Prof VGKM Pisipati was born in India, A.P, in

1944 He received his B.Sc, M.Sc and PhD degrees from Andhra University Since 1975 he has been with physics department at Acharya Nagarjuna University

as Professor, Head, R&D Director He guided 22 PhDs and more than 20 M.Phils His area of research

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includes liquid crystals, nanotechnology and liquid

crystals applications He visited so many countries

and he is having more than 260 International research

publications He served different positions as

academician and successfully completed different

projects sponsored by different government and

non-government bodies He is having 5 patents to his

credit

Prof Habibulla khan born in India, 1962

He obtained his B.E from V R Siddhartha Engineering

College, Vijayawada during 1980-84 M.E from C.I.T,

Coimbatore during 1985-87 and PhD from Andhra

University in the area of antennas in the year 2007.He is

having more than 20 years of teaching experience and

having more than 20 international, national

journals/conference papers in his credit.Prof Habibulla

khan presently working as Head of the ECE department at

K.L.University He is a fellow of I.E.T.E, Member IE and

other bodies like ISTE His research interested areas

includes Antenna system designing, microwave

engineering, Electro magnetics and RF system designing

P Syam Sundar received his B.Tech from JNTU College

of Engineering, Ananthapur in 1999 and M.Tech from

JNTU College of Engineering, Ananthapur in 2006 He

currently working as Associate Professor in the department

of ECE at K L University, Vaddeswaram, Guntur DT His

field of interest includes digital communication, antennas

and signal processing He is having one International

Journal Paper Publication

Mr Kommani Vijaya Prasad,

Professor & HOD, Department of ECE, DJR

Institute of Engineering & Technology, is a well

experienced teacher of Engineering for the past 15

years He holds his B.E from Osmania University,

M.Tech form JNTU University and professional

Diploma in information technology His student &

Teacher experience have created a lot of interest in

him for research Thus he is very interested in the

areas Computer Networks, Communications, Linear

IC Application and VLSI Design He is a life

member of ISTE

K.Balaji was born on 14-12-1963 in India

He did his B.Tech in 1988 from VRSEC and M.S from Bits Pilani in 1994 He is having 22 years of Teaching experience and currently he is working as Associate professor in the Department of ECE, K L University His research area includes Antennas and Communication systems

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