TLE4943C [INFINEON]

Infineon´s XENSIVTM TLE4943C is an integrated, active magnetic field sensor for wheel speed applications based on Hall technology. Its basic function is to measure the speed of a pole wheel or a ferromagnetic toothed wheel. It has a two wire-current interface using the AK protocol for communication.This protocol provides beside the speed signal additional information as direction of wheel rotation and air gap information. The sensor combines a fast power-up time with a low cut-off frequency. Excellent sensitivity and accuracy combined with its wide operational temperature range makes the sensor ideally suited for harsh automotive requirements. The TLE4943C is additionally provided with an overmolded 1.8nF capacitor for improved EMC performance.;
TLE4943C
型号: TLE4943C
厂家: Infineon    Infineon
描述:

Infineon´s XENSIVTM TLE4943C is an integrated, active magnetic field sensor for wheel speed applications based on Hall technology. Its basic function is to measure the speed of a pole wheel or a ferromagnetic toothed wheel. It has a two wire-current interface using the AK protocol for communication.This protocol provides beside the speed signal additional information as direction of wheel rotation and air gap information. The sensor combines a fast power-up time with a low cut-off frequency. Excellent sensitivity and accuracy combined with its wide operational temperature range makes the sensor ideally suited for harsh automotive requirements. The TLE4943C is additionally provided with an overmolded 1.8nF capacitor for improved EMC performance.

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Differential Speed Sensor with AK Protocol  
TLE4943C  
Data Sheet  
V 1.2, July 2018  
Edition July 2018  
Published by  
Infineon Technologies AG  
81726 München, Germany  
© 2007 Infineon Technologies AG  
All Rights Reserved.  
Legal Disclaimer  
The information given in this document shall in no event be regarded as a guarantee of conditions or  
characteristics. With respect to any examples or hints given herein, any typical values stated herein and/or any  
information regarding the application of the device, Infineon Technologies hereby disclaims any and all warranties  
and liabilities of any kind, including without limitation, warranties of non-infringement of intellectual property rights  
of any third party.  
Information  
For further information on technology, delivery terms and conditions and prices, please contact the nearest  
Infineon Technologies Office (www.infineon.com).  
Warnings  
Due to technical requirements, components may contain dangerous substances. For information on the types in  
question, please contact the nearest Infineon Technologies Office.  
Infineon Technologies components may be used in life-support devices or systems only with the express written  
approval of Infineon Technologies, if a failure of such components can reasonably be expected to cause the failure  
of that life-support device or system or to affect the safety or effectiveness of that device or system. Life support  
devices or systems are intended to be implanted in the human body or to support and/or maintain and sustain  
and/or protect human life. If they fail, it is reasonable to assume that the health of the user or other persons may  
be endangered.  
TLE4943C  
33  
Revision History: July 2018, V 1.2  
Previous Version:  
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Updated due to PCN 2017-106  
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remove confidential status Version 1.2 July 2018  
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Data Sheet  
3
V 1.2, July 2018  
TLE4943C  
1
1.1  
1.2  
Product Description . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5  
Overview . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5  
Features . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5  
2
2.1  
2.2  
2.3  
2.4  
2.5  
2.6  
2.7  
2.7.1  
2.7.2  
2.7.3  
2.7.4  
2.7.5  
2.7.6  
2.8  
Functional Description . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6  
General . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6  
Pin Configuration and Sensitive Area . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7  
Marking and Data Matrix Code Description . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 8  
Block Diagram . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 9  
Functional Block Description . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 9  
Typical Application Circuit . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 10  
Protocol Description . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 11  
Definition of Rotation Direction . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 13  
Manchester Encoding . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 14  
Protocol at Normal Speed . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 15  
Protocol for High Speed . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 16  
Data Protocol for Standstill . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 17  
Bit Stump Suppression . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 20  
Operating Modes and States . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 23  
Uncalibrated and Calibrated Mode . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 23  
Under Voltage and Start-up Behavior . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 26  
2.8.1  
2.9  
3
Specification . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 27  
Test Circuit . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 27  
Absolute Maximum Ratings . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 30  
ESD Robustness . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 31  
Operating Range . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 32  
Electrical Characteristics . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 33  
Magnetic Characteristics . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 36  
Degradation of Direction Signal . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 38  
Change of Direction of Encoder . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 39  
Watchdog Reset after Offset Jump . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 41  
3.1  
3.2  
3.2.1  
3.3  
3.4  
3.5  
3.6  
3.7  
3.8  
4
Electro Magnetic Compatibility . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 42  
5
Package Information . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 44  
Lead Pull Out Force . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 44  
Glass Transition Temperature . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 44  
Packing and Package Dimensions of PG-SSO2-53 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 45  
Packing . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 47  
5.1  
5.2  
5.3  
5.4  
Data Sheet  
4
V 1.2, July 2018  
Hall Based Differential Wheel Speed Sensor with AK  
Protocol  
TLE4943C  
1
Product Description  
1.1  
Overview  
The TLE4943C is an integrated, active magnetic field sensor for wheel  
speed applications based on Hall technology. Its basic function is to  
measure the speed of a pole wheel or a ferromagnetic toothed wheel. It  
has a two wire-current interface using the AK protocol for communication.  
This protocol provides beside the speed signal additional information as  
direction of wheel rotation and air gap information. The sensor combines  
a fast power-up time with a low cut-off frequency. Excellent sensitivity and  
accuracy combined with its wide operational temperature range makes  
the sensor ideally suited for harsh automotive requirements. The TLE4943C is additionally provided with an  
overmolded 1.8nF capacitor for improved EMC performance.  
1.2  
Features  
Two wire current interface according AK protocol  
Hall based principle  
Integrated magnetic field sensor for wheel speed measurement  
Detection of rotation direction  
Additional airgap information  
Single chip solution  
High sensitivity  
Large operating air-gaps  
Magnetic pre-induction possible  
Automotive qualified temperature ranges from TJ= -40°C to 150°C  
1.8nF overmolded capacitor  
Wide operating range from 6.5V to 20V  
Green package with lead-free plating  
Product Name  
Product Type  
Ordering Code  
Package  
TLE4943C  
TLE4943C  
SP001963054  
PG-SSO-2-53  
Data Sheet  
5
V 1.2, July 2018  
TLE4943C  
2
Functional Description  
2.1  
General  
The basic operation of the TLE4943C is to measure the differential magnetic field of ferromagnetic or permanent  
magnet target wheels and generate an output signal which represents the motion of these objects. Additionally  
the direction of rotation of a rotating target wheel and the quality (strength) of the magnetic signal are detected.  
For the applications with ferromagnetic toothed wheels a back bias magnet is required. The magnetic  
measurement is based on three equally spaced Hall elements, integrated on the IC. The two outer Hall elements  
have a distance of 2.5mm, the third Hall element is placed in the middle between the outer Hall elements. The  
outer Hall elements generate a differential signal which corresponds to the speed of the detected object. All three  
Hall elements are used for the information of direction detection. The IC has a three-level current interface which  
corresponds to the AK-protocol described below in this data sheet.  
Magnetic offsets of up to +/-30mT are cancelled by a self-calibration algorithm. Only a few magnetic edges after  
start-up (uncalibrated mode) are necessary to finish the self-calibration and providing offset corrected signals in  
calibrated mode. Independent of the mode every increment of the encoder triggers a signal output. The output  
signal frequency represents the increment frequency, e.g. 100 increments per second are equal to 100Hz. The  
frequency of the magnetic signal is half of the output signal frequency.  
Increment n+2  
Increment  
n
Increment n+1  
dB  
Zero  
Crossing  
t
T
IH  
Sensor output  
current I  
s
IM  
IL  
Figure 1  
Definition of increment  
Data Sheet  
6
V 1.2, July 2018  
TLE4943C  
2.2  
Pin Configuration and Sensitive Area  
Figure 2  
Pin configuration and sensitive area (view on frontside marking of component)  
Data Sheet  
7
V 1.2, July 2018  
TLE4943C  
2.3  
Marking and Data Matrix Code Description  
GND  
VDD  
VDD  
GND  
G:  
YY:  
WW:  
green package  
production year  
production week  
123456:  
43CA Æ TLE4943C  
Figure 3  
Marking of PG-SSO-2-53  
Data Sheet  
8
V 1.2, July 2018  
TLE4943C  
2.4  
Block Diagram  
Speed Signal dB = B2 – B1  
Direction Signal dB = B3 – ( B1+B2 )/2  
dir  
B2 (right)  
B3 (center)  
B1 (left)  
speed signal path  
Main  
Σ
-
dB  
LPF  
D-Core  
Tracking  
ADC  
Tracking-ADC  
Algorithm  
Peak Detection  
and  
Offset Calculation  
Offset-  
DAC  
dBdir  
Direction  
Detection  
Direction  
ADC  
Σ
3 current  
modulator  
LPF  
AK Protocol:  
- Peak value  
- timing  
direction signal path  
Figure 4  
Block Diagram  
2.5  
Functional Block Description  
TLE4943C is composed of the following main blocks:  
Hall elements (B1, B2, B3)  
Analog to Digital Converter in the speed signal path (ADC)  
Offset Digital to Analog Converter (Offset DAC)  
Low Pass Filter (LPF)  
Three Current modulator  
Main Comparator (Main)  
Analog to Digital Converter in the direction path (Direction ADC)  
Digital Core (D-core)  
Amplifier for speed and direction path  
Current modulator  
The speed signal dB, calculated out of B2-B1, is amplified and low pass filtered. Afterwards signal is digitized.  
Algorithms in the D-Core for peak detection and offset calculation are executed. The offset is calculated out of two  
detected extrema (max+min)/2. This offset is fed back into speed signal path with an Digital to Analog converter  
to correct any offsets. The main comparator compares the speed signal with zero value. During uncalibrated  
mode, output of speed pulse is triggered in the D-Core by exceeding a certain threshold (2 x dBlimit).  
The direction signal is calculated out of all three Hall elements (described in Figure 4). The direction signal is  
amplified, filtered and digitized. In the D-Core the direction is determined and the data protocol is issued and  
converted into a current modulated signal. The protocol consists of the speed pulse, issued by zero crossing, and  
other data bits determined by the D-Core.  
Data Sheet  
9
V 1.2, July 2018  
TLE4943C  
2.6  
Typical Application Circuit  
The circuit below shows the recommended application circuit with reverse bias and overvoltage protection.  
D1  
R1  
TLE4943C  
VS  
VDD  
GND  
D2  
C1  
Components  
D1: 1N4007  
Uout  
RM  
D2:  
C1:  
R1:  
RM:  
Z-Diode, 22V  
10µF, 35V  
10Ω  
50Ω  
Figure 5  
Application circuit  
Data Sheet  
10  
V 1.2, July 2018  
TLE4943C  
2.7  
Protocol Description  
The protocol consists of a pre-bit, a speed pulse and a nine data information bits (data protocol). The data protocol  
is Manchester-coded. This means the value of a bit is coded in a rise- or a fall of the signal between the mid-current  
value (Imid) and low-current (Ilow) in a certain time window. “0” is represented by a mid-low transition and “1” is  
coded by a low-mid transition. Unused bits are output as default values.  
I
Ihigh  
Imid  
Ilow  
t
Figure 6  
Table 1  
Coding of data bits.  
Coding of Additional Information  
Bit # Meaning  
Name  
Value after power  
up / under voltage  
Condition  
0
1
LR  
0
“1” if dB<dBLR (1=error)  
Error bit,  
Airgap reserve  
SLM  
1
Validity of  
signal  
0=measurement of LM0, LM1, LM2 is valid;  
1=invalid  
amplitude  
measurement  
2
3
0
0
not assigned  
Direction  
validity  
GDR  
DR  
“1” = valid, “0” = invalid  
“0” =direction positive  
4
Direction of  
rotating  
0
information  
Data Sheet  
11  
V 1.2, July 2018  
TLE4943C  
Table 1  
Coding of Additional Information (cont’d)  
Bit # Meaning  
Name  
Value after power  
up / under voltage  
Condition  
5
6
7
8
Air gap gauge  
LM0  
0
0
0
LSB of airgap gauge  
LM1  
LM2  
P
MSB of airgap gauge  
Parity  
to be currently  
calculated  
Always set to get even parity (inclusive Parity bit  
itself)  
Data Sheet  
12  
V 1.2, July 2018  
TLE4943C  
2.7.1  
Definition of Rotation Direction  
The direction of rotation is positive if the direction of rotation and the positive Y – axis of the sensor head are  
pointing in the same direction. This is shown in Figure 7. The coordinate system must be regarded as fixed in the  
sensor head. This must be taken into consideration with assembly variations. In the left representation, frontside  
of the sensor (=marking) points to multipole ring (=encoder) located behind. For positive direction of rotation the  
direction of rotation bit (DR) is set to "0".  
Figure 7  
Definition of rotation direction, Sensor Marking (=Frontside) points to encoder  
Positive Magnetic Field  
N
S
Back  
GND VDD  
Positive Movement direction  
of target wheel  
Figure 8  
Definition of rotation for back bias application, Sensor Marking (=Frontside) points to encoder  
For better understanding three different modes have to be considered: data protocol at normal speed, at high  
speed and standstill. Explanations will follow on next pages.  
Data Sheet  
13  
V 1.2, July 2018  
TLE4943C  
2.7.2  
Manchester Encoding  
The data protocol is Manchester-coded. This means the value of a bit is coded in a rising- or a falling of the signal  
between the middle-current value (Imid) and low-current (Ilow) in a certain time window. A transition from low to  
middle corresponds to "1", a transition from middle to low corresponds to "0". Falling and rising edge of sensor  
output current starts in the middle of data protocol (=tp/2), see bottom of example in Figure 9.  
cr
zero ossing  
Speed pulse  
Data protocol  
3*tp/2  
tp  
tp  
tp  
tp  
tp  
tp  
tp  
tp  
tp  
tp  
tp/2  
Sensor output current  
bit 0  
bit1  
bit2  
bit3  
bit4  
bit5  
bit6  
bit7  
Parity  
Is  
tp/2  
tp  
Figure 9  
Manchester Encoding  
Data Sheet  
14  
V 1.2, July 2018  
TLE4943C  
2.7.3  
Protocol at Normal Speed  
At normal speed (signal frequencies less than 1800Hz) all data bits are transmitted. At the beginning the initial bit  
(Ilow) is sent for tp/2. Then the speed pulse with duration tp is issued which is followed by a current level Ilow for tp/2.  
After that the data protocol is sent.  
Zero crossing  
Ihigh  
bit0  
bit1  
bit2  
bit3  
bit4  
bit5  
bit6  
bit7 Parity  
bit0  
bit1  
bit2  
bit3  
bit4  
bit5  
bit6  
bit7 Parity  
Imid  
Ilow  
3*tp/2  
tp  
tp  
tp  
tp  
tp  
tp  
tp  
tp  
tp  
tp  
tp  
tp  
3*tp/2  
tp  
tp/2  
tp/2  
Bit is  
completely  
transmitted  
Figure 10 Protocol at normal speed  
Data Sheet  
15  
V 1.2, July 2018  
TLE4943C  
2.7.4  
Protocol for High Speed  
For higher speeds the data protocol is shortened (last bits are cut off). The table below shows how many bits are  
transmitted at different signal frequencies. The serial data protocol is shortened at high speeds, because the time  
to the next speed pulse is shorter than the protocol cycle. The data bits at the end are therefore "cut off". In each  
speed range, the maximum possible number of bits of additional information are transferred.  
The output of partially transmitted bits called “bit stumps” are suppressed. See also Chapter 2.7.6. The shortening  
of the protocol does not result in any "bit stumps" (bits which have not been completely transferred). This means  
that the bits affected by the shortening in any case will be transmitted completely, means, a bit which has been  
started must also be transferred to the end. Instead of the bits affected by the shortening, the current level Ilow must  
be output. The suppression of bit stumps does function reliably in all speed ranges and in all regular operating  
states of the sensor, i.e. also in the standstill protocol. This ensures that no compatibility problems occur in any  
regular operating cases caused by e.g. EMC.  
Table 2  
Transmitted bits at electric signal frequency  
Electric Signal frequency1)  
< 1818Hz (1800Hz)  
< 2000 Hz (2000Hz)  
< 2222 Hz (2200Hz)  
< 2500 Hz (2400Hz)  
< 2857 Hz (2800Hz)  
< 3333 Hz (3200Hz)  
< 4000 Hz (4000Hz)  
< 5000 Hz (5000Hz)  
Typical Number of data bits transmitted  
9 (bit0 - bit8)  
8 (bit0 - bit7)  
7 (bit0 - bit6)  
6 (bit0 - bit5)  
5 (bit0 - bit4)  
4 (bit0 - bit3)  
3 (bit0 - bit2)  
2 (bit0 - bit1)  
1) Note: electric signal frequency is equal to two times of magnetic frequency  
Note: Frequencies in brackets are according AK specification  
Data Sheet  
16  
V 1.2, July 2018  
TLE4943C  
2.7.5  
Data Protocol for Standstill  
If for a longer time than tstop no increment is recognized, the IC starts to send the standstill-protocol. This protocols  
is sent every 150ms +/- 20%. In this protocol the current value of the speed-pulse is set to Imid and all the other  
bits are transmitted like described before. For very slow wheel speeds more than one standstill protocol can be  
issued between consecutive speed pulses.  
dB  
Increment n+2  
Increment  
n
Increment n+1  
Incremental  
protocol  
Data Burst:  
on Zero Crossing  
250 ms  
500 ms  
Iout  
28mA  
Incremental  
protocol  
Standstill Protocol  
Data Burst:  
150ms after  
550µs Data Bursts  
Increment Protocol  
Data Burst  
Standstill  
Protocol  
14mA  
7mA  
time  
150ms  
150ms  
150ms  
Figure 11 Standstill protocol  
Data Sheet  
17  
V 1.2, July 2018  
TLE4943C  
Zero Crossing  
tstop  
Speed pulse  
Data protocol  
tp  
tp  
tp  
tp  
tp  
tp  
tp  
tp  
tp  
tp  
tp/2  
tp/2  
bit0  
bit1  
bit2  
bit3  
bit4  
bit5  
bit6  
bit7  
Parity  
Sensor output  
current I  
s
Speed replacement  
pulse  
Initial bit  
Initial bit  
Figure 12 Protocol at standstill  
Note on the standstill - travel transition:  
If an increment of the magnetic encoder is detected, the standstill protocol will be aborted. The speed pulse Ihigh  
with the initiating initial bit (with the level Ilow) has precedence. Due to the suppression of "bit stumps" also required  
in the standstill protocol, the cutting of the protocol can actually only take place between two data bits, and not  
during an ongoing bit transmission. The initial bit enables the speed pulse to always be preceded by a current level  
Ilow for a duration of at least tp/2. This is helpful for the detection of the speed pulse in the ECU (electronic control  
unit).  
Data Sheet  
18  
V 1.2, July 2018  
TLE4943C  
dB  
Increment  
out  
1) Last started bit of standstill protocol will be tranmitted completely  
2) Delay of 25us at llow  
3) Speed pulse issued  
28mA  
Standstill protocol due to  
no edge within last150 ms  
14mA  
7mA  
50us tp/2=25 µs  
Figure 13 Starting wheel movement during standstill protocol using bit stump suppression  
Handling of “Direction Validity” and “Direction” at the standstill protocol:  
At any standstill DR is transmitted as zero (default value) and GDR is transmitted as invalid (=0). With the first 5  
standstill protocols in a row, the direction algorithm is reset. Therefore at following next three zero crossings  
(speed pulses) direction detection and change of direction detection takes place (GDR=invalid, DR=default) and  
GDR is valid and correspondig direction is output at third speed pulse after standstill.  
Handling of “Validity of signal amplitude measurement” within standstill protocol:  
Validity (SLM) of signal measurement is transmitted as 1 (invalid) and signal amplitude (Level in relation to LR) is  
transmitted as 0 during standstill protocol. With the first 5 standstill protocols in a row, the SLM/LM is reset to  
invalid. SLM remains invalid until two new extrema in dB are found. Depending on the amplitude of dB and phase  
of the standstill protocol, SLM is valid with the second, third or fourth speed protocol after every 5th standstill  
protocol.  
Handling of Error Bit “Air Gap Reserve” (=LR bit) within standstill protocol:  
It is transmitted as "0" (no error) in the standstill protocol.  
It is reset to 0 with the first 5 standstill protocols in a row. The standstill protocol LR remains “0” (no error) until two  
new extrema in dB are found.  
.
The initial bit enables the speed pulse to always be preceded by a current level Ilow for a duration of at least tp/2.  
This is helpful for the detection of the speed pulse in the ECU.  
Data Sheet  
19  
V 1.2, July 2018  
TLE4943C  
2.7.6  
Bit Stump Suppression  
The suppression of bit stumps in the wheel speed sensor (WSS) is implemented and described in this paragraph.  
Following principle is used to realize a bit stump suppression:  
Constant time shift of output of speed pulse and data protocol:  
The sensor output is always completely shifted by a bit time tp when a new protocol starts. This is equivalent to a  
time output offset, which has the following effect:  
The initial bit is not started immediately at the moment in which a new protocol starts, what could occur during an  
ongoing data protocol at high speed. Instead, tp is always initially waited for a time offset within which the last  
ongoing protocol output is monitored. For the case a bit output is still active, this will be completely transferred  
without being cut off. This will effectively prevent the occurrence of bit stumps. Within this offset time tp,  
suppression of the next possible data bit of the last protocol will be introduced. In this way a current bit transfer  
will be completed and the transfer of any further bits (of the last protocol) will be prevented. At the end of this offset  
time, the transfer of the initial bit will start. Advantage of this procedure: it is also effective in the standstill protocol,  
i.e. if a new increment of the encoder is detected during an ongoing standstill protocol, a current ongoing bit  
transfer are not be ended in any "bit stump". The transmission of additional bits is suppressed. After delay phase,  
the new transfer begins with the initial bit tp/2, followed by speed pulse and data protocol.  
The following figures show the effect of the bit stump suppression according to the method described above using  
3 representative cases.  
1st case: No cutting off of the preceding protocol. The time between two consecutive protocols is sufficient to  
transfer all bits. Nevertheless, the new protocol begins at the moment of a new increment of the encoder with the  
constant-time output offset of the length tp. This is followed by the initial bitwidth tp/2, then the speed pulse, etc.  
Zero crossing  
Preceding protocol  
bit0  
bit1  
bit2  
bit3  
bit4  
bit5  
bit6  
bit7 Parity  
tp  
tp  
tp  
tp  
tp/2  
tp/2  
Subsequent  
protocol  
Initial bit  
Time output offset  
bit0  
bit1  
bit2  
bit3  
bit4  
tp  
tp  
tp  
tp  
tp/2  
tp/2  
Figure 14 Case 1 - No cutting of the preceding protocol  
Data Sheet  
20  
V 1.2, July 2018  
TLE4943C  
2nd case: The last bit of the preceding protocol is cut off.  
The time between 2 consecutive protocols is no longer sufficient and a new increment of the encoder occurs, while  
the last bit of the preceding protocol is still being transferred. At this moment the new protocol begins again with  
the constant-time output offset of the length tp. However now it is realized in the sensor that a bit transfer is still  
running. This is completely transmitted within the currently running output offset. After the output offset ends, the  
initial bit follows with tp/2, then the speed pulse, etc.  
Zero crossing  
bit0  
bit1  
bit2  
bit3  
bit4  
bit5  
bit6  
bit7 Parity  
Preceding protocol  
tp  
tp  
tp  
tp  
tp/2  
tp/2  
Bit is  
completely  
transmitted  
Initial bit  
bit0  
bit1  
tp  
bit2  
bit3  
bit4  
bit5  
bit6  
Subsequent  
protocol  
Time output offset  
tp  
tp  
tp  
tp/2  
tp/2  
Figure 15 Case 2 - last bit of preceding protocol is cut off  
Data Sheet  
21  
V 1.2, July 2018  
TLE4943C  
3rd case: several bits of the preceding protocol are cut off  
Zero crossing  
Bits #7 and #8 are no  
longer transmitted  
bit0  
bit1  
bit2  
bit3  
bit4  
bit5  
bit6 bit7  
Parity  
Preceding protocol  
tp  
tp  
tp  
tp  
tp/2  
tp/2  
Bits #6 is completely  
transmitted  
Initial bit  
bit0  
bit1  
bit3  
bit4  
bit5  
bit6  
Parity  
bit2  
bit7  
Subsequent  
protocol  
Time output offset  
tp  
tp  
tp  
tp  
tp/2  
tp/2  
Figure 16 Case 3 - several bits of the preceding protocol are cut off  
A new increment of the encoder occurs while, for example, bit #6 of the preceding protocol is still being transferred.  
At this moment the new protocol begins again with the constant time output offset of the length tp. It is realized in  
the sensor that a bit transfer is still running. Bit #6 of the preceding protocol is completely transmitted within the  
current running output time-offset. In addition, the bits #7 and #8 (parity) still missing are suppressed and no longer  
transmitted. As a result, the line is clean again and following the end of the output offset the initial bit follows with  
tp/2, then the speed pulse, etc.  
Data Sheet  
22  
V 1.2, July 2018  
TLE4943C  
2.8  
Operating Modes and States  
The basic operation of the TLE4943C is to measure the differential magnetic field of a rotating target wheel and  
generate an output signal which represents the wheel speed and provides information about rotation direction and  
signal quality. The IC has a three level current interface. The functionality of the TLE4943C can be distinguished  
in two different phases: uncalibrated and calibrated mode.  
2.8.1  
Uncalibrated and Calibrated Mode  
After an initial calibration delay time td_input, the differential magnetic signal dB is tracked by an analog to digital  
converter (ADC) and monitored within the digital circuit. For detection the signal needs to exceed the internal  
threshold DNC (digital noise constant). When the signal slope is identified as a falling (or rising) edge and the  
signal change exceeds the DNC, the first extrema is located and first output pulse is triggered. The digital noise  
constant value is changed accordingly to magnetic field amplitude, leading to a change in phase shift between  
magnetic input signal and output signal. This value of the digital noise constant is determined by the signal  
amplitude. First DNC (=2 x dBlimit), indicated as arrows in figure below. A second output is triggered when the  
signal change exceeds again the value of the new DNC (calulated by (min1 + max 1)/2)in the following rising  
(respectively falling) edge. When a maximum and minimum was found an offset correction will take place. This  
leads to a phase shift of output signal and the sensor enters the calibrated mode. In calibrated mode switching is  
triggered by the zero crossing of the differential magnetic signal. The min/max detection is reduced to 1/4 of peak-  
peak. In calibrated mode minimal DNC is 2 x dBlimit .Out of this consecutive speed pulses have a nominal delay of  
about 180°.  
Handling of additional information bits in uncalibrated and calibrated mode:  
Signal amplitude measurement: SLM is valid if two valid extrema are found (the first extrema after power on is  
invalid). Latest with fourth protocol SLM is valid.  
Startup at high frequencies could lead to shortened protocol. The bit suppression according Chapter “Bit Stump  
Suppression” is executed.  
Data Sheet  
23  
V 1.2, July 2018  
TLE4943C  
dB  
max1  
2 x dBlimit  
(min1+max1)/2  
Offset  
correction  
min1  
(min2+max1)/2  
min2  
Phase Shift Change  
Uncalibrated Mode  
Calibrated Mode  
Figure 17 Example for startup behavior and change form uncalibrated into calibrated mode  
Data Sheet  
24  
V 1.2, July 2018  
TLE4943C  
dB  
max1  
2 x dBlimit  
(min1+max1)/2  
Offset  
correction  
min1  
(min2+max1)/2  
min2  
Phase Shift Change  
Uncalibrated Mode  
Calibrated Mode  
dBdir = center – (left + right) / 2  
max1  
dBdir  
dB_dirmin  
Direction detecion  
min1  
Figure 18 Output triggering in calibrated mode and direction detection  
Direction detection  
Direction signal is always sampled with the main comparator switching (75us +/-25%) before the sensors output  
switching (speed protocol). After two consecutive samples of the direction signal, offset of them is calculated and  
then the third sample is compared with the offset value. The direction is given by the sign of the third sample  
direction signal and the direction of the edge (rising or falling) of the magnetic speed signal. Using this direction  
detection method, detected direction is valid latest with the 4th output speed protocol. GDR bit gives the  
information if the detected direction is valid. On TLE4943C the direction detection is valid if the difference between  
the two consecutive samples of the direction signal (also used for the calculation of the direction) is greater than  
two times dBdirmin and speed signal is four times greater than dBlimit  
.
Data Sheet  
25  
V 1.2, July 2018  
TLE4943C  
2.9  
Under Voltage and Start-up Behavior  
The voltage supply comparator has an integrated hysteresis Vhys with the maximum value of the release level Vrel.  
This determines the minimum required supply voltage VDD of the chip. A minimum hysteresis Vhys is implemented  
thus avoiding a toggling of the output when the supply voltage VDD is modulated due to the additional voltage drop  
at RM when switching from low to high current level at VDD = 4.5V (designed for use with RM=50Ω). As long as VDD  
does not exceed Vrel sensor stays in low level (VDD>Vres).  
Speed pulse  
Data bits  
VDD*  
Vrel  
Vhys  
Vres  
Vhys= Vrel - Vres  
*direct on pins  
Figure 19 Start-up and under voltage behavior  
Data Sheet  
26  
V 1.2, July 2018  
TLE4943C  
3
Specification  
3.1  
Test Circuit  
Following test circuit is used for evaluating electrical parameters:  
VDD  
VS  
GND  
RM = 50Ω  
Integratedcap on leads  
Vout  
Figure 20 Test circuit  
ΔI  
Figure 21 Definition of rise and fall time  
ΔI refers to 80% positive and negative edges of Ilow to Imid and Ilow to Ihigh and vice versa. Slew rate is calculated by  
division of ΔI/tr (rise time) or ΔI/tf (fall time).  
Data Sheet  
27  
V 1.2, July 2018  
TLE4943C  
B[mT]  
Right Hall Element  
Left Hall Element  
[mA]  
Ihigh  
Imid  
Ilow  
Sensor Top View  
Top View  
North  
South  
Left  
(VDD  
Right  
(GND)  
43CA  
)
1
3
2
Hall  
Elements  
left  
right  
Branded Side  
(front side)  
Sensor head is folded  
towards viewer  
Definition of magnetic field  
Positiv is considered when  
South pole shows to back side of IC housing or when  
North pole shows to front side (=branded) of IC housing  
(Gaussmeter: positiv at north pole. Dot towards viewer)  
Figure 22 Definition of field direction and sensor switching  
Data Sheet  
28  
V 1.2, July 2018  
TLE4943C  
Increment n+2  
Increment  
n
Increment n+1  
Zero Crossing  
T
t
Sensor output  
current Is  
DC = t / T * 100%  
Figure 23 Definition of Duty Cycle  
T
speed pulse  
Is  
bit code  
Ti  
Ti+1  
Ti+2  
t
n
ΔT 2  
1
i=1  
δ =  
T
n 1  
T= Ti + Ti+1 (mean value)  
Figure 24 Definition of Jitter  
Data Sheet  
29  
V 1.2, July 2018  
TLE4943C  
3.2  
Absolute Maximum Ratings  
Attention: Stresses above the max. values listed here may cause permanent damage to the device. Exposure to  
absolute maximum rating conditions for extended periods may affect device reliability. Maximum  
ratings are absolute ratings; exceeding only one of these values may cause irreversible damage to the  
integrated circuit.  
TJ=-40°C to 150°C, 4.5V VDD 20V if not indicated otherwise  
Table 3  
Absolute Maximum Ratings  
Symbol  
Parameter  
Values  
Unit  
Note / Test Condition  
Min.  
Typ. Max.  
Supply voltage  
VDD  
-0.3  
-
V
TJ<80°C  
16.5  
20  
22  
24  
24  
26  
TJ=170°C  
TJ=150°C  
t=10x5min  
t=2min; TJ=-40°C..60°C  
t=10x5min, RM50Ω  
t=400ms, RM50Ω included  
in VDD  
Junction temperature 1)  
TJ; Either  
OR  
-40  
110  
125  
150  
160  
170  
190  
°C  
12500h  
10000h  
5000h  
OR  
OR  
2500h  
OR  
500h  
Additional  
4h, VDD<16.5V  
Reverse polarity voltage  
Reverse polarity current  
-16  
V
RM=50Ω included in VDD  
t<1h  
200  
300  
200  
mA  
mA  
mA  
external current limitation  
required, t<4h  
external current limitation  
required, t<1h  
external current limitation  
required, t<10h, T=25°C  
Thermal resistance of package  
Number of power on cycles  
Immunity to external fields  
RthJA  
190  
2
K/W2)  
cycles  
T
500.000  
equivalent to 1600kA/m3);  
TJ=-40..175°C  
Passive lifetime1)  
Processability  
15  
2
a
a
TJ50°C, U=0V  
after Datecode  
1) This lifetime statement is an anticipation based on an extrapolation of Infineon's qualification test results. The actual lifetime  
of a component depends on its form of application and type of use etc. and may deviate from such statement. The lifetime  
statement shall in no event extend the agreed warranty period.  
2) Can be significantly improved by further processing like overmolding  
3) Conversion: B= μ*H ( μ=4*π*10-7)  
Data Sheet  
30  
V 1.2, July 2018  
TLE4943C  
3.2.1  
ESD Robustness  
Table 4  
ESD Protection  
Characterized according to Human Body Model (HBM) tests in compliance with Standard  
EIA/JESD22-A114-B HBM (covers MIL STD 883D)  
Parameter  
Symbol  
Test Result  
Unit  
Notes  
ESD-Protection  
VESD  
± 12  
kV  
R = 1.5 kΩ,  
C = 100 pF  
or >8000V for TLE4943C (H3B according AEC Q100)  
Note:Tested at room temperature  
Data Sheet  
31  
V 1.2, July 2018  
TLE4943C  
3.3  
Operating Range  
All parameters specified in the following sections refer to these operating conditions unless otherwise noticed.  
Table 5  
Operating Range  
Parameter  
Symbol  
Values  
Unit  
Note / Test Condition  
Min.  
Typ. Max.  
Supply voltage  
VDD Hysteresis  
VDD  
6.5  
20  
V
Directly on IC leads; does  
not include voltage drop at  
RM  
Vres  
Vhys  
Vrel  
4.0V 4.2  
4.5  
2.3  
6.5  
6
V
AK: reset voltage  
1.6  
5.8  
1.8  
AK: return voltage  
Supply voltage modulation  
Junction temperature  
VAC  
Vpp  
VDD=13V;  
0<fmod<150kHz1)  
Tj  
Either  
OR  
OR  
OR  
OR  
Bo  
-40  
110  
125  
150  
160  
170  
500  
7.5  
°C  
12500h2)  
10000h2)  
5000h  
2500h  
500h  
Pre induction  
-500  
-7.5  
mT  
K
Temperature change per  
magnetic period for valid DR  
dTj_Dir  
3) valid for dBdir > 1.9mT  
4)valid for dB > 3mT  
Temperature change at standsill dTj_Speed  
-150  
-30  
50  
30  
K
Pre induction offset between  
outer probes  
Bstat l/r  
mT  
Differential induction  
dB  
-120  
-30  
120  
30  
mT  
mT  
Pre-induction offset between  
mean of outer probes and center  
probe  
Bstat m/o  
Signal frequency  
f
0
50005)  
0.83  
Hz  
Hz  
Minimum magn. frequency for  
direction detection  
fdir_min  
0.54  
0.66  
1) sine wave  
2) This lifetime statement is an anticipation based on an extrapolation of Infineon's qualification test results. The actual  
lifetime of a component depends on its form of ap plication and type of use etc. and may deviate from such statement. The  
lifetime statement shall in no event extend the agreed warranty period.  
3) The permissible change of the temperature is, e.g. 7.5K per one magnetic periode. For example a magnetic signal of 10Hz  
(Tmag = 0.1s) results in a max change of temperature = 7.5K / 0.1s = 75K / s. A wrong direction info may occure if dTj_Dir  
is exceeded.  
4) More than 2 speed protocols might be lost if the temperature change during standstill is exceeded at re-drive.  
5) 5000Hz electric signal frequency are equal to 2500Hz magnetic signal frequency (one sin period has two increments).  
Data Sheet  
32  
V 1.2, July 2018  
TLE4943C  
3.4  
Electrical Characteristics  
All values specified at constant amplitude and offset of input signal, over operating range, unless otherwise  
specified. Typical values correspond to VDD=12V and TA=25°C  
Table 6  
Electrical Characteristics1)  
Symbol  
Parameter  
Values  
Typ.  
Unit  
Note / Test Condition  
Min.  
5.9  
11.8  
23.6  
1.8  
3.6  
1
Max.  
8.4  
Supply current low  
Ilow  
Imid  
Ihigh  
7
mA  
mA  
mA  
Supply current mid  
14  
28  
2.0  
4
16.8  
33.6  
2.6  
Supply current high  
Supply current ratio middle/low  
Supply current ratio high/low  
Supply current @ VDD >= Vres_min  
Line regulation  
I
mid/Ilow  
high/Ilow  
I
5.0  
8)  
8)  
mA  
dIx/dVDD  
90  
0
uA/V  
Number of pulses suppressed  
8)after power on and  
internal reset  
8)  
Magnetic edges required for first  
output pulse  
1
4
4
4
edge  
Number of pulses required for  
initial offset calibration  
nstart  
edges 5th “pulse” is offset  
corrected2)8)  
8)  
Number of pulses required for  
initial LM measurement  
3
pulses  
Number of pulses required for  
initial valid direction detection3)  
nDR-start  
pulses 4th pulse has valid  
direction information,  
dBdir>=2*dBdirmin  
4)8)  
7
pulses 7th pulse has valid  
direction info  
2*dBdirmin>dBdir>=dBdirmin  
4)8)  
Valid direction after change of  
direction5)  
3
6
pulses 3rd pulse has valid  
direction information,  
4)8)  
dBdir>=2*dBdirmin  
pulses 6th pulse has valid  
direction info  
2*dBdirmin>dBdir>1.8*dBdirmin  
4)8)  
7
pulses 7th pulse has valid  
direction info  
1.8*dBdirmin>dBdir>dBdirmin  
4)8)  
Frequency limit for direction  
information availability  
fdir-limit  
27006)8)  
Hz  
due to bit stump  
suppression  
Power up time  
1
ms  
us  
%
time for stable current8)  
additive to power up time8)  
dB >=2mT sine wave  
Initial calibration delay time  
Duty cycle in calibrated mode  
td,input  
DCcal  
220  
50  
300  
60  
40  
Data Sheet  
33  
V 1.2, July 2018  
TLE4943C  
Table 6  
Electrical Characteristics1) (cont’d)  
Parameter  
Symbol  
Values  
Typ.  
Unit  
Note / Test Condition  
Min.  
20  
Max.  
80  
Duty cycle in uncalibrated mode DCuncal  
%
%
dB >=2mT sine wave8)  
Jitter, 1Hz < f < 5000Hz  
Jitter, 1Hz < f < 5000Hz  
Jitter for speed pulse  
Sjit-close  
,
±2  
dB >=2mT; 1sigma  
value7)8)  
Tj150°C  
Sjit-close,  
Tj170°C  
Sjit-far,  
Tj150°C  
Sjit-far,  
Tj170°C  
±3  
%
%
%
us  
±4  
2mT > dB >dBlimit ; 1sigma  
value8)  
±6  
0
+0.7  
rising edge of speed pulse  
relative to magnetic edge  
change8)  
Jitter @ board net ripple  
f<5000Hz  
Sjit-AC,  
±0.5  
%
VDD=13V±6Vpp;  
0<fmod<150kHz;  
dB=15mT8)  
Current ripple @ ΔVDD =0V  
dI @dV  
=0V  
pulse shape: triangular8)  
pulse  
height  
1
mA  
ns  
pulse  
400  
length  
Pulse width for speed pulse  
Pulse width for data bits  
Standstill time  
tp  
40  
50  
50  
150  
25  
50  
60  
us  
us  
ms  
us  
us  
Triggerlevel=10.5mA8)  
8)  
tp  
40  
60  
8)  
8)  
8)  
tstop  
120  
20  
180  
30  
Pulse width tp/2 for initial bit  
tp/2  
Pulse width tp for time output  
offset due to bit stump  
suppression  
tp_Bit_supp  
40  
60  
Systematic phase error of output  
edges during start-up and  
uncalibrated mode  
-90  
90  
°
°
Systematical phase error of  
“uncal” edge;  
nth vs. n + 1th edge (does  
not include random phase  
error)8)  
8)  
Phase shift from uncalibrated to  
calibrated mode  
-10  
8
10  
26  
16  
Current slew rate  
SRr, SRf  
nswd  
mA/us 10% and 90% value  
RM=50Ω, TJ<170°C  
9)8)  
Signal watchdog reset  
16  
edges  
1) All parameters refer to described test circuit in this document. See chapter 3.1 Test circuit  
2) after power on or chip reset  
3) Same direction assumed  
4) After power, chip reset or direction reset (after timer watchdog)  
Data Sheet  
34  
V 1.2, July 2018  
TLE4943C  
5) Change of direction of rotation only once assumed  
6) Direction information is updated at every speed protocol! The direction bit corresponds in any case with the physical reality  
of the direction of rotation.  
7) due to digital quantization jitter can not be below 0.7us. Additional analog jitter  
8) Not subject to production test, verified by design/characterization  
9) If no switching of sensor is detected during 750ms (+/-20%) signal watchdog is activated and direction detection is resetted  
(GDR=0). After 16 edges (detected with dB_2 x dBlimit) sensor resets itself and goes into uncalibrated mode  
Data Sheet  
35  
V 1.2, July 2018  
TLE4943C  
3.5  
Magnetic Characteristics  
Table 7  
Magnetic characteristic (amplitude values)  
Parameter  
Symbol  
Values  
Unit  
Note / Test Condition  
Min.  
Typ.  
Max.  
1.34  
+3  
Limit threshold1) 2)  
Limit threshold drift  
dBlimit  
0.3  
0.8  
mT  
%
99% criteria (1 of 96)3)  
dBlimit:Drift -5  
additional drift over lifetime  
at 25°C for one and the  
same sensor  
Limit range Bit1)  
dBLR  
1.02  
1.28  
dBLR_Drift -5  
1.6  
1.6  
2.18  
1.92  
+3  
mT  
mT  
%
+/-36%, 99% criteria  
TJ=10..40°C, 99% criteria  
Limit range bit drift  
additional drift over lifetime  
at 25°C for one and the  
same sensor  
Ratio dBLR / dBlimit  
1.7  
2.0  
0.8  
2.5  
1.441)  
Minimum signal for direction  
detection  
dBdirmin  
0.4  
mT  
valid for GDR=0;  
dB_dir=center-(left+right)/2  
; cal mode, 99% criteria  
Validity of signal amplitude  
measurement  
SLM  
“0” = valid, invalid after  
under-voltage and initial  
value after power up  
Signal amplitude (Level in relation LM=0  
to LR)  
LM=1  
<0.8  
>0.8  
<=1  
>1  
<=1.2  
>1.2  
99% criteria, according to  
AK  
LM=2  
LM=3  
LM=4  
LM=5  
LM=6  
LM=7  
>1.48 >1.75  
>2.1  
>2.5  
>4.2  
>7.0  
>2.95  
>4.95  
>8.25  
>3.6  
>6.0  
>9.9  
>12.0 >14.2  
>21.0 >24.7  
>17.1  
>29.7  
1) value tested at 0h  
2) valid and characterized for f >1Hz  
3) 50% criterion has typ. value of 0.7mT .  
Note:All magnetic values are calculated out of measured sensitivity of each single Hall element.  
Data Sheet  
36  
V 1.2, July 2018  
TLE4943C  
Figure 25 LM bits which are transferred at protocol with increasing magnetic field dB  
Data Sheet  
37  
V 1.2, July 2018  
TLE4943C  
3.6  
Degradation of Direction Signal  
Direction signal is calculated as following “dB_direction = center - (left + right) / 2”. The direction detection is  
optimized for a target wheel pitch of 5 mm. For pitches other than 5 mm the magnetic input signal has to be  
increased to compensate signal loss accordingly. For an ideal pitch of 5mm the absolute speed signal in mT is two  
times higher than direction signal due to differential principle. Speed signal in figure below is normalized to  
magnetic speed signal for a pitch of 5mm. Also direction signal is normalized to speed signal (means degradation  
factor=0.5) and to an ideal pitch of 5mm. Absolute values in mT are half of speed signal.  
1,0  
Deg_speed_norm  
0,9  
Deg_dir_norm  
0,8  
0,7  
0,6  
0,5  
0,4  
0,3  
0,2  
0,1  
0,0  
0
1
2
3
4
5
6
7
8
9
10  
11  
12  
Pitch / mm  
Figure 26 Degradation of speed and direction signal dependent on used target wheel pitch  
Data Sheet  
38  
V 1.2, July 2018  
TLE4943C  
3.7  
Change of Direction of Encoder  
A local extremum (maximum or minimum) of the magnetic input signal can be caused during a reversal of rotation  
direction. In this case the local extremum can be detected by the IC and used for offset calibration. (E.g. the local  
maximum marked by an arrow in the diagram below.) Obviously the calculated offset value will be incorrect with  
respect to the following signal. As worst case a duty cycle up to max. 15% to 85% could occur for a few pulses.  
After a re-calibration, which typically takes place after 2...3 zero-crossings the offset will be correct again and  
hence the duty cycle. A local extremum is detected when the extremum exceeds the value of half of the difference  
between the two previous extreme (dB > 0.25*dBpp). Smaller extrema are not deteced. As a result of "bad" duty  
cycle after fast direction reversal the sampling points for direction detection are at unusual signal phase angles  
also.  
At a change of rotation direction in calibrated mode two consecutive samples of dBdir have the same sign therefore  
direction detection is set to invalid. To guarantee a valid direction the next zero crossings after change of direction  
are used to detect direction. The direction information validity at those two speed pulses is set to invalid and  
direction of rotation is set to default. Also, the validity of signal amplitude measurement is set to invalid, signal  
amplitude contains default values and LR is set to 0 (no error). At the latest with the third pulse after direction  
reversal, direction information is valid and direction is issued again. Signal amplitude validity is set to valid and its  
according signal amplitude measurement and LR is issued after two new valid extrema are found.  
Data Sheet  
39  
V 1.2, July 2018  
TLE4943C  
Change of direction of rotation  
dBmaximum1  
dB  
2 x  
dB  
(dBminimum1+dBmaximum1)/2  
dBminimum1  
limit  
(dBminimum2+dBmaximum1)/2  
dBminimum2  
GDR=inv  
SLM=inv  
DR =def  
LM =def  
LR=OK  
GDR=inv  
GDR=inv  
SLM=inv  
DR =def  
LM =def  
LR=OK  
GDR=inv  
SLM=inv  
DR =def  
LM =def  
LR=OK  
SLM=inv  
DR =def  
LM =def  
LR=OK  
dBdir[n-2]  
dBdir  
negative  
dBdir[n-1]  
negative  
dBdir[n]  
Actual time: n  
positive direction  
negative direction  
detected  
Figure 27 Signal behavior when direction of rotation changes  
Data Sheet  
40  
V 1.2, July 2018  
TLE4943C  
3.8  
Watchdog Reset after Offset Jump  
C
D
B
dB  
Offsetjump  
A
Watchdog timer  
Signal watchdog  
Uncal Mode  
Reset  
Standstill protocol  
Figure 28 Reset is triggered after watchdog delay time and signal watchdog  
When an offset jump, greater than the amplitude of the magnetic speed signal occurs, no zero crossing is passed  
anymore and therefore sensor outputs no speed pulse. Instead, standstill protocol is issued. After transmitting five  
standstill protocols (typ. 750ms) the signal watchdog starts. If still no speed pulse is output sensor starts to detect  
extreme with minimum DNC (digital noise constant). After detecting nswd extreme and still no speed pulse issued,  
sensor triggers internal reset and enters uncalibrated mode. Therefore validity of direction, direction information,  
validity of airgap and airgap measurement are set to default values. This represents the same status as after  
power on. Therefore offset calibration starts again.  
Data Sheet  
41  
V 1.2, July 2018  
TLE4943C  
4
Electro Magnetic Compatibility  
EMC Test Circuit Figure 28 is used.  
Additional Information:  
Characterization of Electro Magnetic Compatibility are carried out on sample base of one qualification lot. Not all  
specification parameters have been monitored during EMC exposure. Only key parameters e.g. switching current  
and duty cycle have been monitored.  
Table 8  
Ref. ISO 7637-2; 2004; (values depend on RM); dB=2mT (amplitude of sinus signal);  
V
DD=13.5V; fB=100Hz, T=25°C, RM=30Ω  
Parameter  
Symbol  
Level/Typ  
IV / -100V  
Status  
Testpulse 1  
VEMC  
C/ A (after stress)  
Testpulse 2a1)  
Testpulse 2b  
Testpulse 3a  
Testpulse 3b  
Testpulse 4  
IV / 75  
A2)  
C3)  
A
- / 10V  
IV / -150V  
IV / 100V  
IV / -7V  
A
B
Testpulse 5a  
Testpulse 5b  
IV / 86.5V  
Us* = 28.5V4)  
C
C
1) ISO 7637-2 describes internal resistance = 2 Ω (former 10 Ω)  
2) Node A (see figure 1) does not exceed 22V clamping voltage of D2 in any case.  
3) Ri = 0.01 Ω  
4) A central load dump protection of 42V is used. Us* = 42V - 13.5V  
Table 9  
Ref. ISO 7637-3 Release 19951); dB=2mT (amplitude of sinus signal); VDD=13.5V; fB=100Hz,  
T=25°C, RM=30Ω  
Parameter  
Testpulse 1  
Testpulse 2  
Testpulse 3a  
Testpulse 3b  
Symbol  
Level/Typ  
IV / -30V  
Status  
VEMC  
A
A
A
A
IV / 30V  
IV / -60V  
IV / 40V  
1) Testpulse 1 and 2 are carried out with capacitive coupling clamp even if ISO7637-3 test pulse 1 and 2 is not requesting for  
capacitive coupling clamp  
Table 10  
Ref. ISO 11452-3, 2nd edition 2001-03-01 measured in TEM-cell  
Parameter  
Symbol  
Level/Typ  
IV / 250V/m  
Status  
ETemCell  
CW; AM=80%, f=1kHz  
Data Sheet  
42  
V 1.2, July 2018  
TLE4943C  
VDD  
Figure 29 EMC Test Circuit  
Components:  
D1 = Reverse polarity protoection diode, e.g. 1N4007  
D2 = 22V  
C1= 10uF  
C2 = 1nF  
RM = 30 Ω  
Data Sheet  
43  
V 1.2, July 2018  
TLE4943C  
5
Package Information  
Pure tin covering (green lead plating) is used. Lead frame material is copper based, e.g. K62. Product is RoHS  
(Restriction of Hazardous Substances) compliant and marked with the letter G in front of the data code marking  
and contains a data matrix code on the rear side of the package. Please refer to your key account team or regional  
sales if you need further information.  
d=0.3±0.08mm  
Distance chip to front side  
(date code) of IC  
Figure 30 Distance chip to upper side of IC  
5.1  
Lead Pull Out Force  
The lead pull out force according IEC 60068-2-21 (fifth edition 1999-1) is 10N for each lead.  
5.2  
Glass Transition Temperature (TG)  
Typical glass transition temperature is 165°C (minimum 160°C) measured according dynamic-mechanical-  
analysis (DMA). The glass transition temperature can not be measured in production as separate test vehicle is  
needed for DMA. Material properties are covered by process parameters and handling instruction for post mold  
curing.  
The typical glass transition temperature is 165°C according DSC method. A TG measurement according DMA on  
test vehicle for every incoming material batch is carried out.  
Data Sheet  
44  
V 1.2, July 2018  
TLE4943C  
5.3  
Packing and Package Dimensions of PG-SSO2-53  
Figure 31 Packing Dimensions in mm of PG-SSO-2-53 (Plastik Single Small Outline Package)  
Data Sheet  
45  
V 1.2, July 2018  
TLE4943C  
Figure 32 Package Dimensins in mm of PG-SSO-2-53 (Plastic Single Small Outline Package)  
Data Sheet  
46  
V 1.2, July 2018  
TLE4943C  
5.4  
Packing  
You can find all of our packages, sort of packing and others on our Infineon Internet Page “Products”:  
http://www.infineon.com/products  
Data Sheet  
47  
V 1.2, July 2018  
w w w . i n f i n e o n . c o m  
Published by Infineon Technologies AG  

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