Infineon AppNote AN251 GPS GNSS Low Noise Amplifier BGA915N7

B GA 915 N 7
Highl y Lin ear and L ow Nois e A mplif er
for Gl obal Na vi gati o n S atelli te S ys te m s G PS/ G L O NA S S/ Gal ileo/ C O M PA S S fr o m
1550 MHz to 1 615 M Hz Appli c ations
Applic atio n N ote A N 251
Revision: Rev. 1.3
2011-09-13
RF and P r otecti on D evic es
Edition 2011-10-04
Published by
Infineon Technologies AG
81726 Munich, Germany
© 2011 Infineon Technologies AG
All Rights Reserved.
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THIS APPLICATION NOTE.
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BGA915N7
Highly Linear LNA for Global Navigation Satellite Systems
GPS/GNSS/Galileo/COMPASS
Application Note AN251
Revision History: 2011-09-13
Previous Revision: AN251 Rev.1.2, 2011-07-22
Page
Subjects (major changes since last revision)
1
Title updated
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of Epcos AG. FLEXGO™ of Microsoft Corporation. FlexRay™ is licensed by FlexRay Consortium.
HYPERTERMINAL™ of Hilgraeve Incorporated. IEC™ of Commission Electrotechnique Internationale. IrDA™
of Infrared Data Association Corporation. ISO™ of INTERNATIONAL ORGANIZATION FOR
STANDARDIZATION. MATLAB™ of MathWorks, Inc. MAXIM™ of Maxim Integrated Products, Inc.
MICROTEC™, NUCLEUS™ of Mentor Graphics Corporation. Mifare™ of NXP. MIPI™ of MIPI Alliance, Inc.
MIPS™ of MIPS Technologies, Inc., USA. muRata™ of MURATA MANUFACTURING CO., MICROWAVE
OFFICE™ (MWO) of Applied Wave Research Inc., OmniVision™ of OmniVision Technologies, Inc.
Openwave™ Openwave Systems Inc. RED HAT™ Red Hat, Inc. RFMD™ RF Micro Devices, Inc. SIRIUS™ of
Sirius Satellite Radio Inc. SOLARIS™ of Sun Microsystems, Inc. SPANSION™ of Spansion LLC Ltd.
Symbian™ of Symbian Software Limited. TAIYO YUDEN™ of Taiyo Yuden Co. TEAKLITE™ of CEVA, Inc.
TEKTRONIX™ of Tektronix Inc. TOKO™ of TOKO KABUSHIKI KAISHA TA. UNIX™ of X/Open Company
Limited. VERILOG™, PALLADIUM™ of Cadence Design Systems, Inc. VLYNQ™ of Texas Instruments
Incorporated. VXWORKS™, WIND RIVER™ of WIND RIVER SYSTEMS, INC. ZETEX™ of Diodes Zetex
Limited.
Last Trademarks Update 2011-02-24
Application Note AN251, Rev. 1.3
3 / 24
2011-09-13
BGA915N7
Highly Linear LNA for Global Navigation Satellite Systems
GPS/GNSS/Galileo/COMPASS
Table of Content, List of Figures and Tables
Table of Content
1
BGA915N7 GPS Front-End LNA for High Performance Integrated Solution ............................... 6
2
Introduction ........................................................................................................................................ 7
3
Application Circuit ........................................................................................................................... 10
4
Typical Measurement Results ......................................................................................................... 11
5
Measured Graphs for Galileo, GPS and GLONASS bands .......................................................... 13
6
Miscellaneous Measured Graphs ................................................................................................... 19
7
Evaluation Board .............................................................................................................................. 21
8
Authors .............................................................................................................................................. 23
Application Note AN251, Rev. 1.3
4 / 24
2011-09-13
BGA915N7
Highly Linear LNA for Global Navigation Satellite Systems
GPS/GNSS/Galileo/COMPASS
Table of Content, List of Figures and Tables
List of Figures
Figure 1
Figure 2
Figure 3
Figure 4
Figure 5
Figure 6
Figure 7
Figure 8
Figure 9
Figure 10
Figure 11
Figure 12
Figure 13
Figure 14
Figure 15
Figure 16
Figure 17
Figure 18
Figure 19
Figure 20
Figure 21
Figure 22
BGA915N7 in TSNP-7-6 Package (1.40mm x 1.26mm x 0.38mm) ..................................................... 6
Block diagram of the BGA915N7 for GNSS High Bands 1559-1615MHz applications ....................... 9
BGA915N7 application circuit ............................................................................................................ 10
Power gain of BGA915N7 for Galileo, GPS and GLONASS bands .................................................. 13
Narrowband power gain of BGA915N7 for Galileo, GPS and GLONASS bands .............................. 13
Input matching of BGA915N7 for Galileo, GPS and GLONASS bands ............................................. 14
Output matching of BGA915N7 for Galileo, GPS and GLONASS bands .......................................... 14
Reverse isolation of BGA915N7 for Galileo, GPS and GLONASS bands ......................................... 15
Noise figure of BGA915N7 for Galileo, GPS and GLONASS bands ................................................. 15
Input 1 dB compression point of BGA915N7 at supply voltage of 1.8V for Galileo, GPS and
GLONASS bands ............................................................................................................................... 16
Input 1 dB compression point of BGA915N7 at supply voltage of 2.8V for Galileo, GPS and
GLONASS bands ............................................................................................................................... 16
Carrier and intermodulation products of BGA915N7 for GPS band at Vcc=1.8V .............................. 17
Carrier and intermodulation products of BGA915N7 for GPS band at Vcc=2.8V .............................. 17
Carrier and intermodulation products of BGA915N7 for GLONASS band at Vcc=1.8V .................... 18
Carrier and intermodulation products of BGA915N7 for GLONASS band at Vcc=2.8V .................... 18
Stability factor k of BGA915N7 upto 10GHz ...................................................................................... 19
Stability factor µ1 of BGA915N7 upto 10GHz .................................................................................... 19
Stability factor µ2 of BGA915N7 upto 10GHz .................................................................................... 20
Input and output matching for Galileo, GPS and GLONASS bands with Vcc=1.8V .......................... 20
Input and output matching for Galileo, GPS and GLONASS bands with Vcc=2.8V .......................... 21
Populated PCB picture of BGA915N7 ............................................................................................... 21
PCB layer stack .................................................................................................................................. 22
List of Tables
Table 1
Table 2
Table 3
Table 4
Table 5
Pin Definition ........................................................................................................................................ 9
Switching Mode .................................................................................................................................... 9
Bill-of-Materials................................................................................................................................... 10
Electrical Characteristics (at room temperature), Vcc = Vpon = 1.8 V .............................................. 11
Electrical Characteristics (at room temperature), Vcc = Vpon = 2.8 V .............................................. 12
Application Note AN251, Rev. 1.3
5 / 24
2011-09-13
BGA915N7
Highly Linear LNA for Global Navigation Satellite Systems
GPS/GNSS/Galileo/COMPASS
BGA915N7 GPS Front-End LNA for High Performance Integrated Solution
1
BGA915N7 GPS Front-End LNA for High Performance Integrated
Solution
1.1
Features
• High gain: 15.5 dB
• High out-of-band input 3rd-order intercept point: +10 dBm
• High input 1dB compression point: -5 dBm
• Low noise figure: 0.7 dB
• Low current consumption: 4.4 mA
• Operating frequency: 1550-1615 MHz
• Supply voltage: 1.5 V to 3.6 V
• Digital on/off switch (1V logic high level)
• Very small TSNP-7-6 leadless package
• B7HF Silicon Germanium technology
• RF output internally matched to 50 Ω
• Only three external SMD components necessary
• 2 kV HBM ESD protection (including AI-pin)
• Pb-free (RoHS compliant) package
Figure 1
BGA915N7 in TSNP-7-6 Package (1.40mm x 1.26mm x 0.38mm)
1.2
Applications
- Global Positioning System (GPS)
- GLONASS (Russian GNSS)
- Galileo (European GNSS)
- COMPASS (Chinese Beidou Navigation System)
Application Note AN251, Rev. 1.3
6 / 24
2011-09-13
BGA915N7
Highly Linear LNA for Global Navigation Satellite Systems
GPS/GNSS/Galileo/COMPASS
Introduction
2
Introduction
The BGA915N7 is a front-end Low Noise Amplifier (LNA) for Global Navigation Satellite
Systems (GNSS) applications. It is based on Infineon Technologies’ B7HF SiliconGermanium (SiGe:C) technology, enabling a cost-effective solution in a very small TSNP-7-6
package with ultra low noise figure, high gain, high linearity and low current consumption
over a wide range of supply voltages from 3.6 V down to 1.5 V. The GNSS satellites are at an
orbit altitude of more than 20,000 km away from earth’s surface and transmit power in the
range of +47 dBm. After taking losses (atmospheric, antenna etc.) into account, the received
signal strength at the GNSS device input is very low in the range of -130 dBm. The ability of
the GNSS device to receive such a low signal strength and provide meaningful information to
the end-user depends strongly on the noise figure of the GNSS receive chain. This ability
which is called receiver sensitivity can be improved by using a low-noise amplifier with low
noise figure and high gain at the input of the receiver chain. The improved sensitivity results
in a shorter Time-To-First-Fix (TTFF), which is the time required for a GNSS receiver to
acquire satellite signals and navigation data, and calculate a position and also improved
coverage area. Noise figure of the LNA defines the overall noise figure of the GNSS receiver
system. This is where BGA915N7 excels by providing noise figure as low as 0.7 dB and high
gain of 15.5 dB, thereby improving the receiver sensitivity significantly.
The ever growing demand to integrate more and more functionality into one device leads to
many challenges when transmitter/receiver has to work simultaneously without degrading the
performance of each other. In today’s smart-phones a GNSS receiver simultaneously coexists with transceivers in the GSM/EDGE/UMTS/LTE bands. These 3G/4G transceivers
transmit high power in the range of +24 dBm which due to insufficient isolation couple to the
GNSS receiver. The cellular signals can mix to produce Intermodulation products exactly in
the GNSS receiver frequency band. For example, GSM 1712.5 MHz mixes with UMTS 1850
MHz to produce third-order-product exactly at GPS 1575 MHz. To quantify the effect,
BGA915N7 shows out-of-band input IP3 at GPS of +10.6 dBm as a result of frequency
mixing between GSM 1713 MHz and UMTS 1851 MHz with power levels of -20 dBm.
BGA915N7 has a high in-band input 3rd order intercept point (IIP3) of +0.37 dBm, so that it is
especially suitable for the GPS function in mobile phones.
Application Note AN251, Rev. 1.3
7 / 24
2011-09-13
BGA915N7
Highly Linear LNA for Global Navigation Satellite Systems
GPS/GNSS/Galileo/COMPASS
Introduction
BGA915N7 also offers sufficient rejection at 787.76MHz, which is band-13 of upcoming LTE
and whose 2nd harmonic is at GPS frequency, to meet specifications of 2nd harmonic of band13 without any additional circuitry. BGA915N7 has input referred band-13 second harmonic
level of -48.5 dBm when the input signal of 787.76 MHz at -25 dBm is applied.
The output of the BGA915N7 is internally matched to 50 Ω, and a DC blocking capacitor is
integrated on-chip, thus no external component is required at the output. Depending on the
application, three or four external components on the input side are required.
The device also integrates an on-chip ESD protection which can resist until 2 kV (referenced
to Human Body Model). The integrated power on/off feature provides for low power
consumption and increased stand-by time for GNSS handsets. Moreover, the low
consumption (4.4 mA) makes the device suitable for portable technology like GNSS receivers
and mobiles phones.
The Internal circuit diagram of the BGA915N7 is presented in Figure 2. Table 1 show the pin
assignment of BGA915N7. Table 2 shows the truth table to turn on/off BGA915N7 by
applying different voltage to the PON pin.
Application Note AN251, Rev. 1.3
8 / 24
2011-09-13
BGA915N7
Highly Linear LNA for Global Navigation Satellite Systems
GPS/GNSS/Galileo/COMPASS
Introduction
Figure 2
Table 1
Block diagram of the BGA915N7 for GNSS High Bands 1559-1615MHz applications
Pin Definition
Pin
Symbol
Comment
1
DEG
Emitter degneration
2
AI
Amplifier Input
3
BIAS
Collector to Base bias
4
AO
Amplifier Output
5
VCC
Voltage supply
6
PON
Power On/Off mode
7
VSS
Grounding
Table 2
Mode
Switching Mode
Symbol
ON/OFF Control Voltage
Min
Max
On
PON, on
1.0V
VCC
Off
PON, off
0
0.4
Application Note AN251, Rev. 1.3
9 / 24
2011-09-13
BGA915N7
Highly Linear LNA for Global Navigation Satellite Systems
GPS/GNSS/Galileo/COMPASS
Application Circuit
3
Application Circuit
3.1
Schematic Diagram
Figure 3
BGA915N7 application circuit
Table 3
Symbol
1
Bill-of-Materials
Value
Unit
Package
Manufacturer
Comment
C1 (optional)
1
µF
0402
Various
RF bypass for low frequencies
C2 (optional)
33
pF
0402
Various
DC block
C3
1
pF
0402
Various
Input matching
L1
82
nH
0402
Murata LQW series
Bias feed, RF choke
self resonance frequency @ 1.575 GHz
L2
7.3
nH
0402
Murata LQW series Input matching / noise matching
TSNP-7-6
Infineon
N1
M1
BGA915N7
2
~ 0.55
nH
SiGe LNA
Microstrip line for gain setting
1
This application circuit is implemented using high-Q inductors. For application with low-Q inductors please refer to
application note AN253
2
Total board inductance = inductance of the microstrip line (~500pH) + inductance of via (~50pH)
Please refer to application note AN258 for more details on “realization of small inductor values on a PCB by using
microstriplines”.
Application Note AN251, Rev. 1.3
10 / 24
2011-09-13
BGA915N7
Highly Linear LNA for Global Navigation Satellite Systems
GPS/GNSS/Galileo/COMPASS
Typical Measurement Results
4
Typical Measurement Results
Table 4 and Table 5 show typical measurement results of the application circuit shown in
Figure 3. The values given in this table include losses of the board and the SMA connectors if
not otherwise stated.
Table 4
Electrical Characteristics (at room temperature), Vcc = Vpon = 1.8 V
Parameter
Symbol
Value
Unit
DC Voltage
Vcc
1.8
V
DC Current
Icc
4.6
mA
Frequency
System
Sys
Galileo/COMPASS
GPS
GLONASS
Frequency
Range
Freq
1559-1593
1575
1602-1615
MHz
Gain
G
15.5
15.4
15.2
dB
Noise Figure
NF
0.76
0.77
0.76
dB
Input Return
Loss
RLin
11.1
11.3
11.4
dB
Output Return
Loss
RLout
15.9
16.6
16.8
dB
Reverse
Isolation
IRev
20.2
20.1
19.9
dB
Comment/Test
Condition
PCB and SMA
connectors of 0.05dB
losses substracted
fgalileo = 1559 MHz
Input P1dB
IP1dB
-7.5
-7.2
dBm
-6.4
fgps = 1575 MHz
f GLONASS = 1615 MHz
Output P1dB
OP1dB
LTE band-13
nd
2 Harmonic
H2 – input
referred
Input IP3
In-band
7.0
7.2
dBm
7.8
dBm
-48.2
fIN = 787.76 MHz
PIN = -25 dBm
f1gal/gps = 1575 MHz
f2gal/gps = 1576MHz
IIP3
-0.13
-0.03
1.06
dBm
f1GLONASS =1609 MHz
f2GLONASS =1610 MHz
Input power= -30dBm
Output IP3
In-band
Input IP3
out-of-band
Stability
OIP3
15.5
15.5
IIP3o
16.4
dBm
11
dBm
f1 = 1713 MHz
f2 = 1851 MHz
Input power= -20dBm
k
Application Note AN251, Rev. 1.3
>1
11 / 24
--
Unconditionnally
Stable from 0 to
10GHz
2011-09-13
BGA915N7
Highly Linear LNA for Global Navigation Satellite Systems
GPS/GNSS/Galileo/COMPASS
Table 5
Electrical Characteristics (at room temperature), Vcc = Vpon = 2.8 V
Parameter
Symbol
Value
Unit
DC Voltage
Vcc
2.8
V
DC Current
Icc
4.7
mA
Frequency
System
Sys
Galileo/COMPASS
GPS
Glonass
Frequency
Range
Freq
1559-1593
1575
1602-1615
MHz
Gain
G
15.6
15.5
15.3
dB
Noise Figure
NF
0.77
0.76
0.76
dB
Input Return
Loss
RLin
11.7
12.0
12.2
dB
Output Return
Loss
RLout
15.3
16.2
17.4
dB
Reverse
Isolation
IRev
20.6
20.5
20.2
dB
Comment/Test
Condition
PCB and SMA
connectors of 0.05dB
losses substracted
fgalileo = 1559 MHz
Input P1dB
IP1dB
-4.6
-4.4
-3.6
dBm
fgps = 1575 MHz
f GLONASS = 1615 MHz
Output P1dB
OP1dB
LTE band-13
nd
2 Harmonic
H2 – input
referred
Input IP3
In-band
10.0
10.1
10.7
dBm
dBm
-48.5
fIN = 787.76 MHz
PIN = -25 dBm
f1gal/gps = 1575 MHz
f2gal/gps = 1576MHz
IIP3
0.37
0.37
1.23
dBm f1GLONASS =1609 MHz
f2GLONASS =1610 MHz
Input power= -30dBm
Output IP3
In-band
Input IP3
out-of-band
Stability
OIP3
IIP3o
k
Application Note AN251, Rev. 1.3
15.9
15.9
10.6
>1
12 / 24
16.6
dBm
f1 = 1713 MHz
dBm f2 = 1851 MHz
Input power= -20dBm
--
Unconditionnally
Stable from 0 to
10GHz
2011-09-13
BGA915N7
Highly Linear LNA for Global Navigation Satellite Systems
GPS/GNSS/Galileo/COMPASS
Measured Graphs for Galileo, GPS and GLONASS bands
5
Measured Graphs for Galileo, GPS and GLONASS bands
Gain
20
1559 MHz
15.5 dB
15
1575 MHz
15.44 dB
10
S21 (dB)
1559 MHz
15.56 dB
Gain at Vcc=1.8V
1575 MHz
15.5 dB
Gain at Vcc=2.8V
1615 MHz
15.32 dB
1615 MHz
15.23 dB
5
0
-5
-10
-15
-20
0
Figure 4
500 1000 1500 2000 2500 3000 3500 4000 4500 5000 5500 6000
Frequency (MHz)
Power gain of BGA915N7 for Galileo, GPS and GLONASS bands
Narrowband gain
16
Gain at Vcc=1.8V
1559 MHz
15.556 dB
15.8
1575 MHz
15.502 dB
15.6
1615 MHz
15.324 dB
Gain at Vcc=2.8V
S21 (dB)
15.4
1559 MHz
15.498 dB
15.2
1575 MHz
15.438 dB
15
1615 MHz
15.234 dB
14.8
14.6
14.4
14.2
14
1500
Figure 5
1525
1550
1575
1600
1625
Frequency (MHz)
1650
1675
1700
Narrowband power gain of BGA915N7 for Galileo, GPS and GLONASS bands
Application Note AN251, Rev. 1.3
13 / 24
2011-09-13
BGA915N7
Highly Linear LNA for Global Navigation Satellite Systems
GPS/GNSS/Galileo/COMPASS
Measured Graphs for Galileo, GPS and GLONASS bands
Input matching
0
S11 at Vcc=1.8V
S11 at Vcc=2.8V
S11 (dB)
-5
1575 MHz
-11.3 dB
1559 MHz
-11.05 dB
-10
1615 MHz
-11.35 dB
1559 MHz
-11.7 dB
1575 MHz
-11.99 dB
-15
1615 MHz
-12.15 dB
-20
0
Figure 6
500 1000 1500 2000 2500 3000 3500 4000 4500 5000 5500 6000
Frequency (MHz)
Input matching of BGA915N7 for Galileo, GPS and GLONASS bands
Output matching
0
S22 at Vcc=1.8V
S22 at Vcc=2.8V
S22 (dB)
-5
-10
1559 MHz
-15.86 dB
1575 MHz
-16.56 dB
-15
1615 MHz
-16.84 dB
1559 MHz
-15.28 dB
1575 MHz
-16.21 dB
1615 MHz
-17.39 dB
-20
0
Figure 7
500 1000 1500 2000 2500 3000 3500 4000 4500 5000 5500 6000
Frequency (MHz)
Output matching of BGA915N7 for Galileo, GPS and GLONASS bands
Application Note AN251, Rev. 1.3
14 / 24
2011-09-13
BGA915N7
Highly Linear LNA for Global Navigation Satellite Systems
GPS/GNSS/Galileo/COMPASS
Measured Graphs for Galileo, GPS and GLONASS bands
Isolation
-10
S12 at Vcc=1.8V
-15
1575 MHz
-20.08 dB
1559 MHz
-20.17 dB
-20
S12 (dB)
S12 at Vcc=2.8V
1615 MHz
-19.9 dB
-25
1615 MHz
-20.24 dB
1575 MHz
1559 MHz -20.45 dB
-20.56 dB
-30
-35
-40
-45
0
Figure 8
500 1000 1500 2000 2500 3000 3500 4000 4500 5000 5500 6000
Frequency (MHz)
Reverse isolation of BGA915N7 for Galileo, GPS and GLONASS bands
Noise figure
1
NF at Vcc=1.8V
NF at Vcc=2.8V
NF (dB)
0.9
0.8
0.7
1559 MHz
0.759
1559 MHz
0.765
1575 MHz
0.774
1615 MHz
0.756
1575 MHz
0.76
1615 MHz
0.755
0.6
0.5
1559
Figure 9
1567
1575
1583
1591
Frequency (MHz)
1599
1607
1615
Noise figure of BGA915N7 for Galileo, GPS and GLONASS bands
Application Note AN251, Rev. 1.3
15 / 24
2011-09-13
BGA915N7
Highly Linear LNA for Global Navigation Satellite Systems
GPS/GNSS/Galileo/COMPASS
Measured Graphs for Galileo, GPS and GLONASS bands
Compression point at 1dB with Vcc=1.8V
20
P1dB at Vcc=1.8V Galileo (1559MHz)
P1dB at Vcc=1.8V GPS (1575MHz)
P1dB at Vcc=1.8V GLONASS (1615MHz)
Gain (dB)
18
-25 dBm
15.55 dB
-25 dBm
15.32 dB
16
14
-6.38 dBm
14.3 dB
-25 dBm
15.3 dB
-7.524 dBm
14.55 dB
-7.214 dBm
14.32 dB
12
10
-25
Figure 10
-20
-15
-10
Power (dBm)
-5
0
Input 1 dB compression point of BGA915N7 at supply voltage of 1.8V for Galileo, GPS and
GLONASS bands
Compression point at 1dB with Vcc=2.8V
20
P1dB at Vcc=2.8V Galileo (1559MHz)
P1dB at Vcc=2.8V GPS (1575MHz)
P1dB at Vcc=2.8V GLONASS (1615MHz)
Gain (dB)
18
-25 dBm
15.6 dB
16
-3.646 dBm
14.39 dB
-25 dBm
15.41 dB
14
-4.641 dBm
14.6 dB
-25 dBm
15.39 dB
-4.386 dBm
14.41 dB
12
10
-25
Figure 11
-20
-15
-10
Power (dBm)
-5
0
Input 1 dB compression point of BGA915N7 at supply voltage of 2.8V for Galileo, GPS and
GLONASS bands
Application Note AN251, Rev. 1.3
16 / 24
2011-09-13
BGA915N7
Highly Linear LNA for Global Navigation Satellite Systems
GPS/GNSS/Galileo/COMPASS
Measured Graphs for Galileo, GPS and GLONASS bands
Intermodulation for GPS band
0
-10
1576 MHz
-14.32
1575 MHz
-14.28
-20
Power (dBm)
-30
-40
-50
-60
1577 MHz
-73.78
-70
-80
-90
-100
1573
Figure 12
1574
1575
1576
Frequency (MHz)
1577
1578
Carrier and intermodulation products of BGA915N7 for GPS band at Vcc=1.8V
Intermodulation for GPS band
0
-10
1575 MHz
-14.23
1576 MHz
-14.27
-20
Power (dBm)
-30
-40
-50
-60
1577 MHz
-74.62
-70
-80
-90
-100
1573
Figure 13
1574
1575
1576
Frequency (MHz)
1577
1578
Carrier and intermodulation products of BGA915N7 for GPS band at Vcc=2.8V
Application Note AN251, Rev. 1.3
17 / 24
2011-09-13
BGA915N7
Highly Linear LNA for Global Navigation Satellite Systems
GPS/GNSS/Galileo/COMPASS
Measured Graphs for Galileo, GPS and GLONASS bands
Intermodulation for GLONASS band
0
-10
1610 MHz
-14.53
1609 MHz
-14.46
-20
Power (dBm)
-30
-40
-50
-60
-70
1611 MHz
-76.1
-80
-90
-100
1607
Figure 14
1608
1609
1610
Frequency (MHz)
1611
1612
Carrier and intermodulation products of BGA915N7 for GLONASS band at Vcc=1.8V
Intermodulation for GLONASS band
0
-10
1610 MHz
-14.46
1609 MHz
-14.39
-20
Power (dBm)
-30
-40
-50
-60
1611 MHz
-76.43
-70
-80
-90
-100
1607
Figure 15
1608
1609
1610
Frequency (MHz)
1611
1612
Carrier and intermodulation products of BGA915N7 for GLONASS band at Vcc=2.8V
Application Note AN251, Rev. 1.3
18 / 24
2011-09-13
BGA915N7
Highly Linear LNA for Global Navigation Satellite Systems
GPS/GNSS/Galileo/COMPASS
Miscellaneous Measured Graphs
6
Miscellaneous Measured Graphs
Stability K factor
3
Stability K factor at Vcc=1.8V
Stability K factor at Vcc=2.8V
2
1575 MHz
1.13
1
1575 MHz
1.106
0
100
Figure 16
2100
4100
6100
Frequency (MHz)
8100
10000
Stability factor k of BGA915N7 upto 10GHz
Stability Mu1 factor
3
Stability Mu1 factor at Vcc=1.8V
Stability Mu1 factor at Vcc=2.8V
1575 MHz
1.642
2
1
1575 MHz
1.509
0
100
Figure 17
2100
4100
6100
Frequency (MHz)
8100
10000
Stability factor µ1 of BGA915N7 upto 10GHz
Application Note AN251, Rev. 1.3
19 / 24
2011-09-13
BGA915N7
Highly Linear LNA for Global Navigation Satellite Systems
GPS/GNSS/Galileo/COMPASS
Miscellaneous Measured Graphs
Stability Mu2 factor
3
Stability Mu2 factor at Vcc=1.8V
Stability Mu2 factor at Vcc=2.8V
2
1575 MHz
1.349
1
1575 MHz
1.276
0
100
Figure 18
2100
4100
6100
Frequency (MHz)
8100
10000
Stability factor µ2 of BGA915N7 upto 10GHz
0.8
1.0
Input and Output matching with Vcc=1.8V
Swp Max
1615MHz
2.
0
6
0.
Input
Output
0.
4
0
3.
10.0
10.0
1615 MHz
r 0.815933
x -0.187204
2
-0.
-4
.0
-5.
0
-3
.0
.0
-2
-1.0
-0.8
-0
.6
.4
-0
Figure 19
5.0
5.0
4.0
3.0
2.0
1.0
0.8
0.6
0
0.2
0.2
1559 MHz
r 0.733601
x -0.0844743
0
4.
1615 MHz
r 1.1184
x 0.582512
-10.0
0.4
1559 MHz
r 0.791711
x 0.475553
Swp Min
1559MHz
Input and output matching for Galileo, GPS and GLONASS bands with Vcc=1.8V
Application Note AN251, Rev. 1.3
20 / 24
2011-09-13
BGA915N7
Highly Linear LNA for Global Navigation Satellite Systems
GPS/GNSS/Galileo/COMPASS
Evaluation Board
0.8
1.0
Input and Output matching with Vcc=2.8V
Swp Max
1615MHz
Output
2.
0
6
0.
Input
0.
4
0
3.
10.0
5.0
10.0
4.0
3.0
2.0
1.0
0.8
0.6
0.4
0.2
5.0
1615 MHz
r 1.09257
x 0.524272
1615 MHz
r 0.804721
x -0.147024
-10.0
0.2
1559 MHz
r 0.710489
x -0.0552515
0
0
4.
1559 MHz
r 0.785904
x 0.426873
2
-0.
-4
.0
-5.
0
-3
.0
.0
-2
-1.0
-0.8
-0
.6
.4
-0
Swp Min
1559MHz
Figure 20
Input and output matching for Galileo, GPS and GLONASS bands with Vcc=2.8V
7
Evaluation Board
Figure 21
Populated PCB picture of BGA915N7
Application Note AN251, Rev. 1.3
21 / 24
2011-09-13
BGA915N7
Highly Linear LNA for Global Navigation Satellite Systems
GPS/GNSS/Galileo/COMPASS
Evaluation Board
Vias
Rogers 4003C, 0.2mm
Copper
35µm
Figure 22
FR4, 0.8mm
PCB layer stack
Application Note AN251, Rev. 1.3
22 / 24
2011-09-13
BGA915N7
Highly Linear LNA for Global Navigation Satellite Systems
GPS/GNSS/Galileo/COMPASS
Authors
8
Authors
Anthony Thomas, Engineer of Business Unit “RF and Protection Devices”.
Jagjit Singh Bal, Engineer of Business Unit “RF and Protection Devices”.
Dr. Chih-I Lin, Senior staff engineer of Business Unit “RF and Protection Devices”.
Application Note AN251, Rev. 1.3
23 / 24
2011-09-13
w w w . i n f i n e o n . c o m
Published by Infineon Technologies AG
AN251