This is the fourth edition of this manual, it describes the following transponders:
RI-TRP-RRHP
RI-TRP-WRHP
This Reference Manual is for customers who wish to use the TIRIS 23 mm Glass Encapsulated
Transponder in Radio Frequency Identification (RFID) installations. The manual includes
technical information concerning the function, technical specifications, application and
environmental related data.
Texas Instruments reserves the right to change its products or services at any time without
notice. TI provides customer assistance in various technical areas, but does not have full
access to data concerning the uses and applications of customer's products. Therefore TI
assumes no responsibility for customer product design or for infringement of patents and/or
the rights of third parties, which may result from assistance provided by TI.
The TIRIS logo and the word TIRIS are registered trademarks of Texas Instruments
Incorporated.
Figure 14: Determination of resonance and -3dB by monitoring pick-up coil voltage .......................... 15
Figure 15: Test set-up for powering field strength determination ........................................................ 15
Figure 16: Received signal at the pick up coil, if power field strength is sufficient .............................. 16
Figure 17: Determination of the transponder signal strength with Helmholtz aperture ........................ 17
Figure 18: Monitored signal voltage at the spectrum analyzer (time domain mode) ............................ 17
Page 3 of 22
23 mm Transponder Reference Manual 25 July 1996
1. Introduction
The TIRIS 23 mm Glass Encapsulated Pulsed FM Transponder is a key product in low frequency
RFID systems that can be used for a variety of applications, such as automotive security systems.
The device is available in Read Only (RO) and Read/Write (R/W) versions. Electro Magnetic
signals are used to power the passive (batteryless) device, to transmit the identification number to
a reader unit or to program the device with new data. The basic principle is described in Figure 1.
Both RO and R/W versions use an 80 bit non-volatile memory (EEPROM) for storage of 64
identification bits and a 16 bit Block Check Character (BCC). The RO type is factory
programmed with a unique tamperproof code that cannot be altered. The R/W version can be
programmed by the user.
The 23 mm Transponder comprises a ferrite core antenna, a charge capacitor, a resonance
capacitor and the integrated circuit (Figure 2). The antenna inductance and the resonance
capacitor form a high quality resonant circuit.
TRANSMIT/REC EIVE ANTENNA
FIELD LINES
ANTENNA AXIS
RF MODULE
CONTROL
UNIT
TIRIS READ/WRITE UNIT
CF4 5538
TRANSPONDER
Figure 1: System Configuration Showing the Reader, Antenna and Transponder
ANTENNA
TRANSPONDER
IC
CHARGE
CAPACITOR
Figure 2: Block Diagram of the TIRIS Pulsed FM Transponder
Page 4 of 22
25 July 1996 23 mm Transponder Reference Manual
2. Transponder Packaging
The dimensions of the transponder are given in Figure 3.
The 23 mm shape offers several advantages:
1. The transponder is hermetically sealed.
2. The transponder is robustly constructed to withstand vibration (IEC68-2-6) and shock
(IEC68-2-6).
3. For Applications where read range is not the most critical point the transponder can be
mounted or used in such a way that the orientation is not controlled.
Figure 3: Dimensions of the TIRIS 23 mm Transponder (in mm)
3. Product Codes
64 bit Read Only device: RI-TRP-RRHP
64 bit Read/Write device: RI-TRP-WRHP
4. Function
The Pulsed FM System uses a sequential function principle separating the transponder powering
(charge) and transponder data transmission mode. The advantages of the sequential mode are
described in Section 5.1 "Basic System Data".
4.1 Read (Reading of RO and R/W Transponders)
During the charge (or powering phase) of between 15 and 50 ms the interrogator generates an
electromagnetic field using a frequency of 134.2 kHz. The resonant circuit of the transponder is
energized and the induced voltage is rectified by the integrated circuit to charge the capacitor.
The transponder detects the end of the charge burst and transmits its data using Frequency Shift
Keying (FSK), utilizing the energy stored in the capacitor.
Page 5 of 22
23 mm Transponder Reference Manual 25 July 1996
The typical data low bit frequency is 134.2 kHz, the typical data high bit frequency is 123.2 kHz.
The low and high bits have different durations, because each bit takes 16 RF cycles to transmit.
The high bit has a typical duration of 130 µs, the low bit of 119 µs. Figure 5 shows the FM
principle used. Regardless of the number of low and high bits, the transponder response duration
is always less than 20 ms.
The data format consists of 128 bits. Different start/stop bytes and end bits are used, to allow
secure distinction between RO and R/W Transponder. Figures 6a and 6b show the format of the
received data for RO and R/W transponders.
After transmission of the data format the capacitor is discharged. The typical transponder readout
timing is described in figure 4. The charge phase is followed directly by the read phase (RO
mode).
Data encoding is done in NRZ mode (Non Return to Zero). The clock is derived from the RF
carrier by a divide-by-16 function.
Figure 4: Charge and Read Function of the Transponder, Showing the Voltage at the
Transponder and Exciter (Reader) Coil
Page 6 of 22
25 July 1996 23 mm Transponder Reference Manual
0011
134.2 kHz 123.2 kHz 134.2 kHz 123.2 kHz
129.2 µs119.9 µs
Figure 5: FM Principle Used for the Read Function of TIRIS Transponders
PRE
BITS
16
864
IDENTIFICATION DATA
Figure 6a: Read Data Format of TIRIS RO Transponder
START
PRE
BITS
16864
IDENTIFICATION DATA
Figure 6b: Read Data Format of TIRIS R/W Transponder
READ DATA
112 bits
READ DATA
112 bits
DATA
BCC
16
DATA
BCC
STOPSTART
8
STOP
81615
DISCHARGE
END
BITS
15
16 bits
MSBLSB
DISCHARGE
ENDBITS
IDENT.
DATA
16 bits
MSBLSB
Page 7 of 22
23 mm Transponder Reference Manual 25 July 1996
4.2 Write and Program
A new identification number can be written (programmed) into a R/W transponders in the following
manner: After the charge phase the R/W transponder enters the write mode providing the reader starts to
modulate the field by switching the transmitter on and off (TXCT-). Modulation index of this amplitude
modulation is 100%. The duration of the off-phase defines whether a low bit or a high bit is being
transmitted (Pulse Width Modulation). Writing means, the transponder shifts the received bits into a shift
register. After the write phase the reader's transmitter is switched on for a certain time (programming
time) in order to energize the process of programming the shift register data into the EEPROM. All 80
bits are programmed simultaneously into the EEPROM. Once the data is programmed into the EEPROM
the transponder automatically sends back the captured data to the reader to allow a security check, this
process takes place when the transmitter is switched off. Each read unit can be used as a write unit
through software change only. No hardware changes are required.
Figure 7 describes the write function by showing the transmitter (reader) RF output signal and the
transponder RF input signal. Figure 8 shows the TXCT- signal of the reader (transmitter) during the
write and program function. The data transmission format of the write mode is described in figure 9.
Charge: Continuous RF Module Transmitter output Signal
Write: Pulse width modulation of the RF module transmitter output signal
Program: Continuous RF module transmitter output signal
Read: Frequency Shift Keying of the transponder resonant circuit oscillation
Figure 7: Charge, Write and Program Principle used for TIRIS, showing the voltage at the
exciter (reader) and transponder antenna coil
Page 8 of 22
25 July 1996 23 mm Transponder Reference Manual
WRITE
TRANSMITTER OFF
TXCT -
TRANSMITTER ON
RF MODULE
TXCT- SIGNAL
t
offH
HIGH BIT
t
H
t
onH
t
offL
LOW BIT
t
onL
t
L
Figure 8: The Write and Program Function
MSB
PROGR.
15 ms
CHARGE
50 ms
LSB
112 bit
880
WRITE
KEYWORD
16 ms160 ms32 ms
8
WRITE
PASSWORD
16 ms
WRITE DATA
309 ms
16
WRITE FRAME
Figure 9: Write Data Format for Programming Function
PROGRAM
t
prog
128 bit
READ
20 ms
5. Characteristics of the Pulsed FM System
5.1 Basic System Data
The TIRIS Pulsed FM system multiplexes the power and read functions avoiding compromises.
This results in the following characteristics and options:
a) Individual optimization of the power and read functions by the system designer.
b) Variation of powering time by S/W to trade-off speed/current consumption with other
parameters
c) Absence of the high powering signal during the data reception phase
d) Data transmission by an active oscillator. This is associated with a high signal strength
level and a high transponder efficiency.
e) NRZ modulation encoding for high data speed and low transmission bandwidth.
Page 9 of 22
23 mm Transponder Reference Manual 25 July 1996
5.2 Reader and System Design Impact
*Ease of receiver and power function design and the optimization of performance due to
sequential power/read functions.
*Low field strength for transponder charge, resulting in lower cost of the power function.
*Optional performance and cost trade-offs by variation of:
interrogation speed by software down to 35 ms.
component selection to achieve different EMI performance levels.
5.3 System Performance and Functional Reliability Impact
*Inherent EMI robustness and high system Signal/Noise ratio because:
A. The transponder emits 6..20 dB higher data signal (compared to conventional systems).
B. The powering phase is noise immune and the data transmission phase duration is typically
16 ms.
C. FSK and NRZ allow a high data rate (typically 9 kbit/s).
D. Modulation is direct carrier FSK which has inherent AM noise suppression.
*Low reader power dissipation because of low charge field strength.
*Low power consumption due to pulsed operation (=low peak power x low duty cycle).
*Data telegram transmission is secured by 16 bit CRC-CCITT error detection protocol.
*The receive time is short, because the transponder protocol always starts at the beginning of
the data stream. Therefore read repetitions are not necessary.
5.4 Other Quality Factors of the TIRIS Pulsed FM System
*High and consistent transponder product quality and performance by automated high volume
manufacturing.
*The direct FSK provides enhanced separation and better position-selective reading of adjacent
transponders compared to AM systems.
*Product migration path concept from RO to R/W to Password protected and Multipage
transponders. The reader or system can be changed from RO to R/W by S/W change only.
*TIRIS transponders are 100% tested according to the procedures of TI's Total Quality
Culture.
*The reliability of TIRIS transponders is monitored through the following tests: temperature
and humidity, thermal shock, and operating life.
Page 10 of 22
25 July 1996 23 mm Transponder Reference Manual
6. EMI/EMC Performance
6.1 General
For any given RF-ID system, the EMI/EMC performance is determined by three factors:
1. The reader design and the resulting noise immunity performance
2. The signal strength of the transponder and Signal/Noise ratio at the receiver input
3. The transponder immunity to EM fields:
-The most critical EMI factor or component in a system is the reader immunity.
-A high transponder data signal facilitates reader design through the higher Signal/Noise.
ratio
-The least critical component is the transponder. Immunity levels are generally very high.
All EMI sources can be classified into three different categories:
a.Broad band "industrial" noise of sporadic or continuous nature
b.Discrete radio frequency signals unmodulated or FM /FSK modulated
c.Discrete radio frequency signals which are AM or ASK modulated.
6.2 The Automotive Environment and Factors
In an automotive environment all noise types are present and potentially cause EMI problems.
Especially the increased application of electronics and communication systems in cars employing
digital and ASK type modulation techniques can produce and emit high field strength levels.
The highest energy noise sources are in the low frequency part of the spectrum at frequencies
from a few cycles up to a few kHz. The sources are actuators, solenoid switching, ignition,
motors, control circuitry and so on. They pollute the car environment, either by direct emission,
or by induction, or by conducted radiation.
Above 10 kHz, the noise levels decay quickly at a rate of 20...40 dB/octave. RFID systems
emitting and receiving data signals at these or higher frequencies are less affected by EMI.
6.3 TIRIS Pulsed FM Transponder and System Performance
EMI measurement procedures which are most currently cited (for example the DIN 40839/part4)
are inappropriate to:
a. determine a realistic RF-ID system behavior for an automotive environment
b. determine the EMI performance and threshold of transponder
c. test systems at worst case (low frequency) conditions.
However the TIRIS transponder meets and exceeds the DIN40839/part4.
Page 11 of 22
23 mm Transponder Reference Manual 25 July 1996
The TIRIS system performance using reader and 23 mm transponder is shown in figures 10, 11
and 12.
Figure 10 shows the system immunity over a spectrum of 6 decades. At the most critical Radio
Short Wave Broadcast frequencies 400 V/m were encountered.
Figure 11 highlights the system performance simulating in-car RF communication conditions.
Figure 12 shows the performance (reading range) under induced broad band noise (white noise)
conditions.
Pulsed FM EMI System Performance
10,000
1,000
100
10
Malfunction
1
FunctionFunction
0.1
0.01
E M I FIELD STRENGTH
[VOLTS/m]
0.001
0.0010.010.11101001,000
LWSWMWFM
FREQUENCY MHz]
VHF / UHF
Figure 10: EMI Performance Test of the TIRIS System.
The graph shows the EM Immunity level in V/m as function of the frequency range from 1 kHz to
1000 MHz. Measurement condition: minimum 90% read probability at maximum read range.
Using a standard TIRIS reader.
Page 12 of 22
25 July 1996 23 mm Transponder Reference Manual
120
100
80
60
40
20
READING RANGE (%)
normalized
0
125102050100200500 1,000
430
MHz
145
MHz
900
MHz
ELECTRICAL FIELD STRENGTH (VOLTS/m)
Figure 11: EMI performance at commonly used radio communication frequencies in
automotive environment.
White noise performance of TIRIS
100
90
80
70
60
50
40
30
READING RANGE [%]
20
10
0
20253035404550556065
AM Systems
NOISE LEVEL [dB
µΑµΑ
TIRIS Pulsed FM
/m]
Figure 12: Reading range under broad band noise (white noise) conditions
Page 13 of 22
23 mm Transponder Reference Manual 25 July 1996
f
7. Measurement Set-Ups
This Section describes typical measurement set-ups to determine transponder relevant data like:
resonant frequency, bandwidth, quality factor, powering field strength and transponder signal field
strength listed in Section 9 "Rocommended Operating Conditions".
7.1 Measurement Set-Up: Resonance frequency, bandwidth, quality factor of transponder
This test set-up is suitable for resonant frequency (f
measurements as well as the determination
res)
of the -3dB bandwidth (∆f) of the transponder. The quality factor Q of the transponder resonance
circuit can be calculated with equation (1):
(1) Q
res
=
f
∆
The wires of the pick-up coil should be very thin to avoid influence on the measurement results (for
example: by damping). The choice of a 1 MΩ input resistor at the spectrum analyzer is
recommended. Figure 13 shows the test set-up. The relation between pick-up coil voltage and
frequency is shown in Figure 14.
TRANSPONDER
CO I L
PICK-UP
COIL
INPUT
TRACKING GE NERATOR
SPECTRUM
ANALYZER
Figure 13: Measurement set-up for the determination of transponder resonance frequency,
bandwidth and quality factor
Page 14 of 22
25 July 1996 23 mm Transponder Reference Manual
U
Pick-up
coil
f
Res
f
3 dB
f
Figure 14: Determination of the resonance frequency and -3dB bandwidth by monitoring
the pick-up coil voltage
7.2 Measurement Set-Up: Powering Field Strength
The following set-up is used to determine the minimum required powering field strength.
d/2
COILS
TRANSPONDER
ANTEN NA AXIS
SIGNAL
GENERATOR
Trigger
PICK-UP
COIL
d
OSCILLOSCOPE
Figure 15: Test set-up for powering field strength determination
The field between both serial connected coils is homogeneous, due to the fact that the aperture is
built according to the Helmholtz set-up. The circular coils are positioned in parallel on one axis.
The distance between the coils is half the coil diameter. The transponder is positioned in the middle
of the coil axis.
Page 15 of 22
23 mm Transponder Reference Manual 25 July 1996
d
5
2
/
Determination of the minimum powering field strength is possible by changing the field strength
through increasing the coil current. The relation between the generated magnetic flux / field
strength and coil current can either be measured with a calibrated filed probe, or calculated as
follows:
(2) B
454
µ µ
or
⋅
N I
⋅⋅
=⋅⋅
0
µ µ
H
r=⋅⋅
B: magnetic flux (Tesla=Wb/m
2)
H: magnetic field strength (A/m)
N: Number of Helmholtz Coil windings
d: Coil diameter (m)
I: Coil current (A)
µo:magnetic field constant (Vs/Am) = 4×p×10
-7
Vs/Am
µr :relative magnetic field constant (in air: =1)
The Helmholtz set-up can be used for the specification of transponders in the temperature range
from -40 to +85 ºC. Tests showed, however, that deviations of the field strength caused by
temperature negligible.
The data telegram of the transponder can be captured by a pick-up coil (for example: 10 windings,
thin wire to minimize influence) which wraps the transponder. The pulse modulated signal can be
adjusted at the signal generator. The measurement of the power pulse and transponder diagram can
be done with the help of an oscilloscope triggered by the generator signal (see Figure 15). As soon
as a data telegram is completely detected the minimum necessary field strength (calculated with
equation 2) can be monitored.
U
Power
phase
Response phase
max 20msec
t
Figure 16: Received signal at the pick up coil, if power field strength is sufficient
Page 16 of 22
25 July 1996 23 mm Transponder Reference Manual
7.3 Measurement Set-Up: Transponder Signal Strength
The 23 mm transponder has to be located into a homogeneous field (Helmholtz set-up). The
pulsed power signal is generated by a signal generator. A calibrated field strength probe picks up
the transponder signal. The field strength can be calculated by using the calibration factor of the
field strength probe.
COILS
PICK-UP
COIL
ANTENNA AXIS
SIGNAL
GENERATOR
TRANSPONDER
d
SPECTRUM
ANALYZER
Figure 17: Determination of the transponder signal strength (data transmission signal
strength) with Helmholtz aperture
U
Transponder signalPower signal
Noise
t
Power
phase
Read
phase
Figure 18: Monitored signal voltage at the spectrum analyzer (time domain mode)
Page 17 of 22
23 mm Transponder Reference Manual 25 July 1996
Ta
read
Ta
T
s
T
s
H
exc
t
exc
f
exc
t
H
t
exc
H
t
exc
H
acttexc
H
act
t
exc
t
bit
t
off L
t
off H
8. Absolute Maximum Ratings
All data given for free air operating temperature range (unless otherwise noted).
PARAMETERCONDITIONMIN.NOM.MAX.UNIT
Operating temperature
(read)
Operating temperature
(program)
Storage temperature
Storage temperature
Field strength
Prog
-4085
-4070
-40100
5 min175
134.2 kHz168
o
C
o
C
o
C
o
C
dBµA /m
9. Recommended Operating Conditions
All data given for free air operating temperature range, a charge time of 50 ms, and a transmitter
frequency of 134.2 kHz +/- 40 Hz (unless otherwise noted).
PARAMETERCONDITIONMIN.NOM.MAX.UNIT
Charge duration for
read and write
Charge frequency for
read and write
Programming time
Programming field
strength
Programming field
strength
Activation field strength
Activation field strength
Write bit duration
Write pulse pause low bit
Write pulse pause high
bit
prog
prog
prog
= 50 ms142.5
+ 25 oC
= 50 ms
= 50 ms136.5
+ 25 oC
= 50 ms
*Note2ms
*Note0.3ms
*Note1.0ms
1550ms
134.16134.2134.24kHz
15ms
dBµA/m
138.5
132.5
dBµA/m
dBµA/m
dBµA/m
Note:Depending on reader characteristics and environmental conditions.
Page 18 of 22
25 July 1996 23 mm Transponder Reference Manual
f
L
f
L
t
L
f
H
f
H
t
H
H
out
f
L
fHm
read
f
L
fHm
read
r
read
t
read
m
write
r
write
t
write
10. Characteristics
All data given for free air temperature range, a charge time of 50 ms, and a transmitter frequency
of 134.2 kHz +/- 40 Hz (unless otherwise noted).
PARAMETERCONDITIONMIN.NOM.MAX.UNIT
Operating quality factorQopNote 162
Low bit transmit
frequency
Low bit transmit
frequency
Low bit duration
High bit transmit
frequency
High bit transmit
frequency
High bit duration
Transponder output field
strength @ 5 cm
FSK Modulation index
(read);
FSK Modulation index
(read);
Data transmission rate
(read)
Data transmission time
(read)
ASK modulation index
(write)
Data transmission rate
(write)
Data transmission time
(write)
-
-
+ 25 oC132.2134.3136.2kHz
+ 25 oC121.0122.9125.0kHz
+ 25 oC11kHz
Note 2915kHz
Note 30.5kbit/s
Note 3224ms
131.5139.0kHz
0.1150.1190.121ms
120.0128.0kHz
0.1250.1300.133ms
80101
7.48.7kbit/s
1620ms
100%
dBµA/m
Note 1: Specified Qop must be met in the application over the required temperature range.
Refer to the test set-up shown in figure 13.
Note 2: Maintained over specified temperature range.
temperature
EM Radiation immunity1...512 MHz100V/m
EM Radiation immunity512..1000MHz50V/m
ESD ImmunityIEC 801-22kV
X-ray dose 2000RAD
Vibration (Note 2)IEC 68-2-6, Test Fc
ShockIEC 68-2-27, Test Ea
Note 1: Cumulative failure rate 1%.
10years
Note 2: f = 10 - 2000 Hz.
12. Memory
PARAMETERDATA
Memory size80 bits
Memory organization1 block
Identification data64 bit
Error detection (Data BCC)CRC - CCITT , 16 bit
13. Package
PARAMETERDATA
Dimensions23 mm x 3.85 mm ( see figure 3)
Weight0.6g
Page 20 of 22
25 July 1996 23 mm Transponder Reference Manual
14. Packing Symbolization
The Transponders are packed in a a carrier tape which is closed with a cover tape carrying
product information and Country of Origin information as below:
MALAYSIA
xxxxxxxxxxxxxxxx
Note:'XXXXXXXXXXXXXXXX' is the 16 digits Identification Code (ID) in hexadecimal
numbers.
Page 21 of 22
23 mm Transponder Reference Manual 25 July 1996
B
H
F
=
⋅
µ
dB
A
m
µ
dB
V
m
µ
Appendix A: Conversion Formula
Conversion formula between magnetic flux, magnetic field strength and electric field strength.
0
EZH
=⋅
H =
E
dB V / m
515.
dB Amµµ
−
;H =
;E
B = magnetic flux [Tesla = Wb/m2 =Vs/m2]; 1 mWb/m2 = 0.795 A/m
H = magnetic field strength [ A/m or in logarithmic term dBµA/m]
E = electrical field strength [ V/m or in logarithmic term dBµV/m]
µ0 = magnetic field constant = 1.257×10-6 Vs/Am
ZF = free space impedance = 120 π Ω = 377 Ω
=
Page 22 of 22
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