View detail for ATAN0003: Atmel ATA5279 Application Hints

APPLICATION NOTE
ATA5279 Application Hints
ATAN0003
Features
● General information
● Boost converter calculation and practical hints
● Antenna current regulation
● Oscillator aspects
Description
Most applications work with the components suggested by the typical applications in the
datasheet. Nevertheless, this note includes design hints and considerations which may
help in understanding the circuitry alignment.
An important feature of the antenna driver is the integrated boost converter, the antenna
current regulation and its related dynamic behavior. Special attention must be given to thermal considerations in system design. Therefore, please refer to the related application note
on the Atmel® Web site:
http://www.atmel.com/dyn/resources/prod_documents/doc9168.pdf
9271B-RKE-04/15
Figure 1.
Function Principle of the Antenna Current Regulation Loop
47Ω
Din
Lin
L
Iin
D
10nF
Vout
Vin
+
+
Cin
Cout
VL
PGND
ATA5279
Iout
VDS
Boost Control
Driver Stage
AxP
Sine wave
Generator
IANT
VANT
Control
AxN
Current
Regulation
Return
Line
Switch
VRLS
VSHF
IANT
Zero Cross
Detection
Sample and Hold
DAC
VSHS
VRSH
CINT
RGND
CINT
2
ATAN0003 [APPLICATION NOTE]
9271B–RKE–04/15
RSH
1.
Boost Converter
The boost converter is operated in PWM switch mode at a fixed frequency of typically 125kHz derived from a 8MHz
resonator. It is able to generate an output voltage up to 40V providing the required supply voltage VDS for the driver stage.
The antenna current regulator provides the required control voltage for the boost converter for driving the programmed
current into the antenna. Thus the antenna current is largely independent of the antenna impedance and battery voltage (see
Figure 1).
1.1
Theoretical Dependency of Boost Output Voltage
Ideally the converter output voltage depends on duty cycle (D) of the PWM control only.
However, in the real application the power conversion and thus the output voltage is reduced due to the losses of the
affected components (NMOS, L, D, C) expressed by the efficiency factor η.
For converters operated in Continuous Conducting Mode (CCM) the output voltage is determined as follows:
1
V out = V in  -------------  
1–D
(1)
V in
or D = 1 – ----------  
V out
(2)
t on
whereas D = -----T
(3)
Figure 1-1. Ripple Current through Inductance over Duty Cycle of VL Switch
VL
t
IL
ΔIL
t
toff
ton
T
Because the boost converter of the Atmel® ATA5279 is controlled within the antenna current regulation loop, the duty cycle
and thus the output voltage are automatically set to the required value to achieve the programmed antenna current.
1.2
Inductance and Resulting Ripple Current for CCM Operation
In general, the inductance of the boost coil determines the ripple current through the related components, as inductance
itself, the decoupling diode, and the smoothing capacitor at output. Seen from this standpoint, high inductance should be
selected.
But, due to the stability of the antenna current regulation and the startup time of the Atmel ATA5279 application, the
selection of the inductance is restricted (see also Section 3. “Practical Hints for Boost Converter Alignment” on page 7).
For a selected choke inductance, the ripple current results from the frequency and voltage relations:
V in 1
1
I L = ---   V out – V in   ----------  --V out L
f
(4)
The output voltage Vout = VDS to be provided by the boost converter is determined by the sinusoidal driver voltage which is
needed to drive the programmed antenna current through the impedance of the antenna used (see Figure 1-2). At the same
time the boost output voltage should be increased according to the sine wave rail margin of typical 3V.
ATAN0003 [APPLICATION NOTE]
9271B–RKE–04/15
3
Figure 1-2. Sinusoidal Signal of Antenna Driver Output
VDS
Δ3V
+VANT
0.5 x VDS
-VANT
Δ3V
GND
V out = VDS = 2   I ant_p   Z ant + R Shunt + 2  R DSon  + 3V 
(5)
The average inductor input current Iin can be determined with a power balance calculation.
1
V in_min  I in = ---  V out_max  I out

V out_max  I out
or I in = ----------------------------------V in_min  
1.3
(7)
Calculation Example Based on the Atmel ATAB5279 Evaluation Board
●
●
●
●
●
●
●
Note:
Boost inductance
L = 68µH/2.3Aavg
Antenna impedance max
Zant = 12.5
Shunt resistor
RShunt = 1
Driver stage
RDSon = 0.6
Antenna peak current (max)
Iant = 1Ap
Input voltage (nominal)
Iin = 12V
Efficiency of boost converter (assumed)
η = 0.70(1)
1.
Efficiency is decreased due to the lowered switching rise time due to EMC requirements.
The assumed values come to:
● Boost output voltage (5)
4
(6)
Vout = VDS = 2 [1Ap  (12.5 + 1 + 2  0.6) + 3V] = 35.4V
●
Average output current
1
I out = I ant  --- = 0.318A

●
Average input current (7)
34.5V  0.318A
I in = -------------------------------------- = 1.3A
12V  0.70
●
Inductor ripple current (4)
1
12V
1
I L = -------------------   35.4V – 12V   --------------  ------------- = 0.933A
125kHz
35.4V 68µH
●
Input peak current
ATAN0003 [APPLICATION NOTE]
9271B–RKE–04/15
1
1
I in_P = I in + ---  I L = 1.3A + ---  0.933A = 1.76A
2
2
1.4
Selection of the Boost Inductor
Typically the size of the inductor is determined by the required inductance and rated current.
However, in typical passive entry applications with a short operation cycle time the power dissipation of the inductor is not a
key concern. Thus, diverging from the calculation, the next lower current rate can be selected (smaller size). However,
consideration has been given to the fact that the effective inductance is reduced in relation to the specified value if the coil
current is higher than the specified saturation current.
So for the Atmel® ATAB5279 evaluation board a larger inductor size (68µH/2.3Aavg) is selected so that stress test conditions
are also covered. But in a typical PE application with a low operation cycle, a smaller size is normally acceptable.
1.5
Selecting the Output Decoupling Diode
Use of a schottky diode is recommended to minimize power dissipation. It is suitable in terms of forward voltage drop and
recovery time. Switching losses can be ignored because these are small compared to conductivity losses.
The power dissipation and peak current can be roughly calculated as:
PD ≈ VF Iout
V out
I D_P  I out  ---------V in
(8)
in the worst case
(9)
in the worst case
PD ≈ 0.5V 0.32A ≈ 0.61W
40V
I D_P  0.318A  ----------  1.06A
12V
A Schottky diode rated at 1A/60V would satisfy the requirement for the power dissipation and peak current calculated.
Nevertheless, the voltage drop and thus the power loss are reduced if a higher current rate is chosen.
1.6
Selecting the Output Capacitor
Based on the required load current the output ripple voltage depends in two ways on the capacitor. One portion is effected
by the discharge of the capacitor when loading during the conduction phase (D = ton/T) of the boost transistor. A second part
is generated during the complementary time phase (1-D) during which the charge current generates a voltage drop at the
impedance ESR of the capacitor.
I out  D
V out = -----------------fC
V in
12V
D = 1 – ---------- = 1 – ---------- = 0.7
V out
40V
I L
I out
V out = ESR   ------------- + ---------
1 – D
2 
A high capacitor value should be selected to reduce ripple voltage. Even bigger capacitors result in lower ESR values. But,
in a typical PE application a fast startup of the driver voltage VDS is required, thereby limiting the output capacitor value.
Finally it must be determined if the selected capacitor is suitable for the resulting ripple current. RMS value IC_RMS.
D I C_RMS  I out  -----------1–D
With the calculated values above Iout =0.318A and D = 0.7 the capacitor load current results in IC_RMS = 0.485mA
The new ceramic capacitors on the market are characterized by ultra low ESR values which allow high RMS current load.
For example, on the evaluation board ATAB5279 the selected ceramic capacitor 10µF/50V is specified with an ESR of
<10m. So the temperature rise of this capacitor is less than 10°C at a RMS current of 4 A.
ATAN0003 [APPLICATION NOTE]
9271B–RKE–04/15
5
2.
Selecting the Input LC Filter
The input current becomes a continuous triangular shape if an inductor Lin is used at the boost converter input. In addition, it
serves to smooth the ripple current into the input capacitor Cin.
A line input inductor may be needed to achieve EMC approval for automotive applications. Usually, the required inductance
depends on the specific application and design specification and cannot be defined precisely in advance. To minimize the
components variety, it is useful to select the same inductor used for the boost section (for example 68µH/2.3Aavg).
The input capacitor provides a low impedance source to force the boost converter and prevents any impedance interaction
with the battery power supply. Depending on the acceptable ripple voltage, recommended values range from 47µF to 220µF.
Make sure that the allowable rms ripple current of the selected capacitor is higher than the equivalent rms of the boost
inductor ripple current IL.
I L
0.933A
I Cin_rms = --------- applied to the example I Cin_rms = ----------------- = 0.538A
3
3
The capacitor Cin used with the 220µF/50V evaluation board has an rms current capability of 1290mA at 105°C, thus
complying with the above-mentioned requirement.
6
ATAN0003 [APPLICATION NOTE]
9271B–RKE–04/15
3.
Practical Hints for Boost Converter Alignment
As already mentioned before, the inductance of the boost coil determines the ripple current through the related components,
as inductance itself, the decoupling diode, and the smoothing capacitor at the output.
Considered from this perspective, a higher inductance helps smooth the ripple current and reduces the thermal load,
especially of the internal power NMOS.
Not only does higher inductance require a larger coil and cost more, it can also negatively impact boost control stability. This
occurs in particular with a low current load when the boundary from CCM to DCM operating mode has been reached.
Furthermore, higher inductance values lead to an increased oscillation effect on the NMOS switch (VL) if the converter
switches to DCM operation.
Figure 3-1. Continuous Conduction Mode CCM
Figure 3-2. Discontinuous Conduction Mode DCM
ATAN0003 [APPLICATION NOTE]
9271B–RKE–04/15
7
Figure 3-3. Discontinuous Conduction Mode DCM with RC in Parallel to Output Diode D
Here, the selection of the inductor value involves a trade-off between low ripple current and stable operation of the boost
converter. Atmel therefore recommends basing the inductor selection on the specific load conditions of the driver supply
voltage VDS which is needed to force the required antenna current through the antenna used. Table 3-1 provides guideline
values for selecting a suited inductance for the boost converter.
Table 3-1.
Guideline Values
Higher Load Range
Lower Load Range
Driver Supply Voltage VDS
25 to 40V
Up to 25V
Suggested Boost Inductance
47 to 100µH
22 to 47µH
Applications which also need to cover low loads have to be run in DCM operating mode. The resulting oscillation on the
NMOS switch output VL may be undesirable due to EMC requirements.
As seen in simulations, this oscillation can be suppressed by RC circuitry in parallel to the decoupling diode D with 10nF in
series with 47 (see Figure 1 on page 2).
8
ATAN0003 [APPLICATION NOTE]
9271B–RKE–04/15
4.
Antenna Current Regulator CINT Circuitry
The internal current regulator is designed like a transconductance op-amp and provides sink/source output current at the
CINT pin. A typical application has the capacitor CINT connected to ground so that the regulator has a pure integration
property. The resulting voltage at the CINT pin supplies the internal control for the driver sine wave amplitude as well for the
boost converter unit.
Selecting the CINT capacitor involves a trade-off between rise time and overshoot of antenna current. However, it is difficult
to calculate or simulate this value because the dynamic behavior of the antenna regulation loop also depends on the
antenna Q factor and the boost converter circuitry. Selecting an appropriate CINT value through practical measurements is
therefore recommended. For reference, the graphs in Figure 4-1 depict the impact of the CINT value on the dynamic
behavior of the antenna current. The measurements were done in combination with the Atmel® ATAB5279 antenna driver
board on which CINT = 10nF is typically used.
Figure 4-1. Antenna Current Dynamic Behavior Depending on CINT Circuitry
ATAN0003 [APPLICATION NOTE]
9271B–RKE–04/15
9
5.
Oscillator Aspects
The Atmel® ATA5279 oscillator circuit is based on the principle of a Pierce oscillator. It consists of an inverter circuit
characterized by its output resistance ROSCO and a feedback resistance RFB used for running it in linear mode. To achieve
secure and faster startup the output resistance is reduced during the switch-on phase.
For typical applications an 8MHz ceramic oscillator is used for clocking and deriving the 125kHz driver frequency. If higher
accuracy is required, it can also be operated using an appropriate crystal; however startup times up to 10 times longer must
be taken into account. Alternatively, ceramic resonators with a tolerance of 0.1% are also available.
The circuit in Figure 5-1 shows the generic inverter in combination with the equivalent circuit of the ceramic resonator used.
Figure 5-1. Equivalent Oscillator Circuitry
RFB
Figure 5-2. Inverter with Transconductance Characteristic
OSCI
ROSCO
OSCI
OSCO
C1
OSCO
C1
L1
L1
R1
C0
CL1
R1
CL2
C0
CL1
CL2
Internal Parameters Specified on the Atmel ATA5279 Datasheet:
Driver resistance during startup
ROSCO
Driver resistance during operation
Feedback resistance
0.9k to 2.2k
(See datasheet parameter 3.4)
ROSCO
1.8k to 4.4k
(See datasheet parameter 3.5)
RFB
220k to 340k
(See datasheet parameter 3.6)
Parameters of 8MHz Ceramic Resonator cstce8M00G55A (Murata):
L1 = 257µH; R1 = 6.7 (max. 40); C1 = 1.61pF; C0 = 13.07pF; CL1 = 10pF; CL2 = 10pF
The Atmel ATAB5279 application board has been approved by the resonator manufacturer in terms of oscillator startup and
frequency stability.
An important aspect in terms of the oscillator start-up time is the negative resistance –R of the active network.
According to Barkhausen stability criterion, oscillation occurs if the negative resistance exceeds the effective resistance of
the oscillator branch.
–R  Re
10
ATAN0003 [APPLICATION NOTE]
9271B–RKE–04/15
Crystal manufacturers recommend selecting negative resistance 5 to 10 times greater than the effective resistance to
overcome the effects of tolerances and temperature.
–R
The margin for oscillation startup should be: ----------  5 to 10
Re
To estimate the margin of the oscillator startup, the resistance -R and Re can be calculated by using the approximation
formula based on the Barkhausen stability criterion.
Negative resistance of active network:
gm
0,6µA/mV
- = ---------------------------------------------------------------------------------- = 2375
– R = ---------------------------------------------------------2
2
 2    f   C L1  C L2
 2    125kHz   10pF  10pF
Transconductance of the inverter
gm (min) = 0.6µA/mV (design parameter 3.9)
Load capacity of resonator
CL1/CL2 = 10pF
Effective load capacity of resonator:
C L1  C L2
10pF  10pF
C L = ------------------------- = ------------------------------- = 5pF
C L1 + C L2
10pF + 10pF
Effective resistance of resonator:
C0 2
13.07pF 2
R e = R 1   1 + ------- = 6.7   1 + ------------------- = 87,51


C L
5pF 
Margin for oscillation startup:
–R
2975
m = ---------- = ------------------ = 27.1
Re
87,51
Concluding Note Regarding Resonator Selection:
With respect to the assumed oscillator parameters, the calculated margin for oscillation startup fulfills the recommended
relation
│–R│ / Re to fall in a range between 5 and 10.
However, regardless of that estimate, it is advisable to have resonator qualification carried out as offered by most
manufacturers. This service involves a check of the customer's original PCB and provides a recommendation on the right
type of resonator and suitable external circuits.
ATAN0003 [APPLICATION NOTE]
9271B–RKE–04/15
11
6.
SPI Control
The Atmel® ATA5279 SPI slave interface allows to be operated by a clock frequency of up to 2MHz. The insertion of series
resistors into the control lines may help for decoupling to the microcontroller and limiting the dynamic current rise.
Particular care has to be taken to the VIF supply input. Therefore, at least a blocking capacitor to AGND (e.g. 100nF) has to
be placed close to the device to minimize the noise generated by the internal 8MHz clock frequency.
An enhanced suppression can be achieved when filtering the VIF noise by an additional inline ferrite bead according to
Figure 6-1.
Figure 6-1. SPI Interface
Ferrite Bead
optional
100nF
MCU
ATA5279C
6
VIF
10kΩ
38 S_CS
1kΩ
39 S_CLK
1kΩ
37 MOSI
1kΩ
36 MISO
1kΩ
41 IRQ
1kΩ
40 NRES
10kΩ
9
MACT
10kΩ
10 BCNT
7.
Revision History
Please note that the following page numbers referred to in this section refer to the specific revision mentioned, not to this
document.
12
Revision No.
History
9271B-RKE-04/15
 Put document in the latest template
ATAN0003 [APPLICATION NOTE]
9271B–RKE–04/15
XXXXXX
Atmel Corporation
1600 Technology Drive, San Jose, CA 95110 USA
T: (+1)(408) 441.0311
F: (+1)(408) 436.4200
|
www.atmel.com
© 2015 Atmel Corporation. / Rev.: 9271B–RKE–04/15
Atmel®, Atmel logo and combinations thereof, Enabling Unlimited Possibilities®, and others are registered trademarks or trademarks of Atmel Corporation in U.S. and
other countries. Other terms and product names may be trademarks of others.
DISCLAIMER: The information in this document is provided in connection with Atmel products. No license, express or implied, by estoppel or otherwise, to any intellectual property right
is granted by this document or in connection with the sale of Atmel products. EXCEPT AS SET FORTH IN THE ATMEL TERMS AND CONDITIONS OF SALES LOCATED ON THE
ATMEL WEBSITE, ATMEL ASSUMES NO LIABILITY WHATSOEVER AND DISCLAIMS ANY EXPRESS, IMPLIED OR STATUTORY WARRANTY RELATING TO ITS PRODUCTS
INCLUDING, BUT NOT LIMITED TO, THE IMPLIED WARRANTY OF MERCHANTABILITY, FITNESS FOR A PARTICULAR PURPOSE, OR NON-INFRINGEMENT. IN NO EVENT
SHALL ATMEL BE LIABLE FOR ANY DIRECT, INDIRECT, CONSEQUENTIAL, PUNITIVE, SPECIAL OR INCIDENTAL DAMAGES (INCLUDING, WITHOUT LIMITATION, DAMAGES
FOR LOSS AND PROFITS, BUSINESS INTERRUPTION, OR LOSS OF INFORMATION) ARISING OUT OF THE USE OR INABILITY TO USE THIS DOCUMENT, EVEN IF ATMEL HAS
BEEN ADVISED OF THE POSSIBILITY OF SUCH DAMAGES. Atmel makes no representations or warranties with respect to the accuracy or completeness of the contents of this
document and reserves the right to make changes to specifications and products descriptions at any time without notice. Atmel does not make any commitment to update the information
contained herein. Unless specifically provided otherwise, Atmel products are not suitable for, and shall not be used in, automotive applications. Atmel products are not intended,
authorized, or warranted for use as components in applications intended to support or sustain life.
SAFETY-CRITICAL, MILITARY, AND AUTOMOTIVE APPLICATIONS DISCLAIMER: Atmel products are not designed for and will not be used in connection with any applications where
the failure of such products would reasonably be expected to result in significant personal injury or death (“Safety-Critical Applications”) without an Atmel officer's specific written
consent. Safety-Critical Applications include, without limitation, life support devices and systems, equipment or systems for the operation of nuclear facilities and weapons systems.
Atmel products are not designed nor intended for use in military or aerospace applications or environments unless specifically designated by Atmel as military-grade. Atmel products are
not designed nor intended for use in automotive applications unless specifically designated by Atmel as automotive-grade.