bgm1043n7 front-end module for global navigation satellite

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RF and Protection Devices BGM1043N7 Application Note AN294 Revision: Rev. 1.0 2012-07-23 Front-End Module for Global Navigation Satellite Systems (GNSS) Applications with higher LTE Band-13 rejection using 0402 components

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Page 1: BGM1043N7 Front-End Module for Global Navigation Satellite

RF and Protect ion Devices

BGM1043N7

Appl icat ion Note AN294 Revision: Rev. 1.0

2012-07-23

Front-End Module for Global Navigat ion Satel l i te Systems (GNSS) Appl icat ions with higher LTE Band-13 reject ion using 0402 components

Page 2: BGM1043N7 Front-End Module for Global Navigation Satellite

Edition 2012-07-23

Published by Infineon Technologies AG 81726 Munich, Germany

© 2012 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.

Page 3: BGM1043N7 Front-End Module for Global Navigation Satellite

BGM1043N7 Low-Noise FEM for GPS Applications

Application Note AN294, Rev. 1.0 2012-07-23 3 / 23

Application Note AN294

Revision History: 2012-07-23

Previous Revision: None

Page Subjects (major changes since last revision)

Trademarks of Infineon Technologies AG

AURIX™, C166™, CanPAK™, CIPOS™, CIPURSE™, EconoPACK™, CoolMOS™, CoolSET™, CORECONTROL™, CROSSAVE™, DAVE™, DI-POL™, EasyPIM™, EconoBRIDGE™, EconoDUAL™, EconoPIM™, EconoPACK™, EiceDRIVER™, eupec™, FCOS™, HITFET™, HybridPACK™, I²RF™, ISOFACE™, IsoPACK™, MIPAQ™, ModSTACK™, my-d™, NovalithIC™, OptiMOS™, ORIGA™, POWERCODE™, PRIMARION™, PrimePACK™, PrimeSTACK™, PRO-SIL™, PROFET™, RASIC™, ReverSave™, SatRIC™, SIEGET™, SINDRION™, SIPMOS™, SmartLEWIS™, SOLID FLASH™, TEMPFET™, thinQ!™, TRENCHSTOP™, TriCore™.

Other Trademarks

Advance Design System™ (ADS) of Agilent Technologies, AMBA™, ARM™, MULTI-ICE™, KEIL™, PRIMECELL™, REALVIEW™, THUMB™, µVision™ of ARM Limited, UK. AUTOSAR™ is licensed by AUTOSAR development partnership. Bluetooth™ of Bluetooth SIG Inc. CAT-iq™ of DECT Forum. COLOSSUS™, FirstGPS™ of Trimble Navigation Ltd. EMV™ of EMVCo, LLC (Visa Holdings Inc.). EPCOS™ 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. 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 2011-11-11

Page 4: BGM1043N7 Front-End Module for Global Navigation Satellite

BGM1043N7 Low-Noise FEM for GPS Applications

List of Content, Figures and Tables

Application Note AN294, Rev. 1.0 2012-07-23 4 / 23

Table of Content

1 BGM1043N7 GPS and GLONASS Front-End Module ..................................................................... 5

2 Introduction ........................................................................................................................................ 6

3 Description .......................................................................................................................................... 8

4 Application Circuit and Block Diagram ........................................................................................... 9

5 Measurement Results ...................................................................................................................... 10

6 Measured Graphs for GPS and GLONASS Bands ........................................................................ 12

7 Miscellaneous Measured Graphs ................................................................................................... 18

8 Evaluation Board and Layout Information .................................................................................... 21

9 Authors .............................................................................................................................................. 22

List of Figures

Figure 1 BGM1043N7 in TSNP-7-10 Package................................................................................................... 5 Figure 2 RF System Overview: Mobile Phone ................................................................................................... 6 Figure 3 GNSS system with integrated GNSS FEM BGM1043N7 for mobile/portable and personal navigation

devices ................................................................................................................................................. 7 Figure 4 Block Diagram of BGM1043N7 ............................................................................................................ 8 Figure 5 Schematic diagram of the BGM1043N7 application circuit .................................................................. 9 Figure 6 Wideband Insertion Power Gain of BGM1043N7 .............................................................................. 12 Figure 7 Narrowband Insertion Power Gain of BGM1043N7 for GPS and GLONASS bands ......................... 12 Figure 8 Input Matching of BGM1043N7 for GPS and GLONASS bands ....................................................... 13 Figure 9 Output Matching of BGM1043N7 for GPS and GLONASS bands ..................................................... 13 Figure 10 Reverse Isolation of BGM1043N7 for GPS and GLONASS bands ................................................... 14 Figure 11 Noise Figure of BGM1043N7 for GPS and GLONASS bands ........................................................... 14 Figure 12 Input 1dB Compression Point of BGM1043N7 at supply voltage of 1.8V for GPS band ................... 15 Figure 13 Input 1dB Compression Point of BGM1043N7 at supply voltage of 2.8V for GPS band ................... 15 Figure 14 Carrier and intermodulation products of BGM1043N7 for GPS band at Vcc=1.8V ........................... 16 Figure 15 Carrier and intermodulation products of BGM1043N7 for GPS band at Vcc=2.8V ........................... 16 Figure 16 Carrier and intermodulation products of BGM1043N7 for GLONASS band at Vcc=1.8V ................. 17 Figure 17 Carrier and intermodulation products of BGM1043N7 for GLONASS band at Vcc=2.8V ................. 17 Figure 18 Input and Output Matching of BGM1043N7 for GPS and GLONASS bands with Vcc=1.8V ............ 18 Figure 19 Input and Output Matching of BGM1043N7 for GPS and GLONASS bands with Vcc=2.8V ............ 18 Figure 20 Stability Factor K of BGM1043N7 upto 10 GHz ................................................................................. 19 Figure 21 Stability Factor µ1 of BGM1043N7 upto 10 GHz ............................................................................... 19 Figure 22 Stability Factor µ2 of BGM1043N7 upto 10 GHz ............................................................................... 20 Figure 23 Picture of Evaluation Board for BGM1043N7 .................................................................................... 21 Figure 24 PCB Layer Information ....................................................................................................................... 21

List of Tables

Table 1 Pin Assignment of BGM1043N7 .......................................................................................................... 9 Table 2 Bill-of-Materials ..................................................................................................................................... 9 Table 3 Electrical Characteristics (at room temperature), Vcc = Vpon = 1.8 V .............................................. 10 Table 4 Electrical Characteristics (at room temperature), Vcc = Vpon = 2.8 V .............................................. 11

Page 5: BGM1043N7 Front-End Module for Global Navigation Satellite

BGM1043N7 Low-Noise FEM for GPS Applications

BGM1043N7 GPS and GLONASS Front-End Module

Application Note AN294, Rev. 1.0 2012-07-23 5 / 23

1 BGM1043N7 GPS and GLONASS Front-End Module

1.1 Features

Operating frequency: 1575.42 MHz and 1598.06-

1605.38 MHz

High Gain: 15.1 dB

Low Noise Figure (GPS): 1.5 dB

Low current consumption: 4.0 mA

Out-of-band rejection in cellular bands: > 43 dBc

Input compression point in cellular bands: 30 dBm

Supply voltage: 1.5 V to 3.6 V

Tiny TSNP-7-10 leadless package (2.3 x 1.7 x 0.73 mm3)

RF output internally matched to 50 Ω

IEC ESD contact discharge of RF input pin: 6 kV

Only 3 external SMD parts

RoHS compliant package (Pb-free)

Figure 1 BGM1043N7 in TSNP-7-10 Package

1.2 Applications

- GPS (Global Positioning System) working in the L1 band at 1575.42 MHz

- GLONASS (Globalnaya Navigatsionnaya Sputnikovaya Sistema) working in the L1 band from 1598.06 MHz to 1605.38 MHz

Page 6: BGM1043N7 Front-End Module for Global Navigation Satellite

BGM1043N7 Low-Noise FEM for GPS Applications

Introduction

Application Note AN294, Rev. 1.0 2012-07-23 6 / 23

2 Introduction

Global Navigation Satellite System or GNSS receiver, as we know, works on the reception of location based

information from satellite signals. There are several standards worldwide like GPS, GLONASS, Galileo and

COMPASS Bei Du. However, the power levels of the satellite signals received, can be lower than -130 dBm.

This poses a challenge on the sensitivity of the GNSS receiver. Along with this, the ever growing disturbing or

jamming signals in the adjacent cellular bands makes the design of the receiver front-end even more difficult.

The rapidly growing market for GNSS systems is driving the design of advanced and high-performance GNSS

receivers. A simple overview of the GNSS RF system in a mobile phone or other handheld devices is shown in

Figure 2.

Figure 2 RF System Overview: Mobile Phone

GNSS receivers for mobile or handheld applications are always under the threat of high power cellular signals.

Due to the coexistence of GNSS and Cellular services, there is a strong coupling of the DCS/PCS and Cellular

signals to the GNSS receiver. The performance of a standard integrated GNSS receiver chip cannot meet the

specifications required for the present systems. An external RF front-end is essential to achieve this required

performance. The most important prerequisites for the front-end of a GNSS receiver are low noise figure and

sufficient amplification of the desired signal together with high attenuation of the jamming signals.

Blocking Signal ESD

protection

Int.

LNA

GNSS

Receiver IC

GNSS Signal < -130dBm

Tx Signal

Satellite GNSS

signal

GNSS RF

Front-end

module

Tranceiver moduleGSM800/GSM900/

DCS/PCS1800/

UMTS/

WLAN

Mobile Phone / Handheld device

Page 7: BGM1043N7 Front-End Module for Global Navigation Satellite

BGM1043N7 Low-Noise FEM for GPS Applications

Application Note AN294, Rev. 1.0 2012-07-23 7 / 23

2.1 Systems overview of a GNSS receiver

Several configurations can be adopted for a GNSS receiver chain. In all configurations, as mentioned earlier, a

RF front-end like BGM1043N7 is placed between the antenna and the GNSS receiver chip. Mobile/portable

devices as well as personal navigation devices request decreasing form factor used by the implementation of

the GNSS function in the devices. BGM1043N7 supports the designers to minimize the area in the front-end.

Such a configuration is shown in Figure 3. The BGM1043N7 can also be used for the active antenna module.

Figure 3 GNSS system with integrated GNSS FEM BGM1043N7 for mobile/portable and personal navigation devices

BPF

GNSS Receiver

IC

Embedded ANT

LNA

BGM1043N7

Page 8: BGM1043N7 Front-End Module for Global Navigation Satellite

BGM1043N7 Low-Noise FEM for GPS Applications

Description

Application Note AN294, Rev. 1.0 2012-07-23 8 / 23

3 Description

The BGM1043N7 is a combination of a low-insertion-loss pre-filter with Infineon’s high performance low noise

amplifier (LNA) for Global Positioning System (GPS) and Globalnaya Navigatsionnaya Sputnikovaya Sistema

(GLONASS) applications. Both, GPS and GLONASS frequency bands, can be used at the same time. Through

the low insertion loss of the filter, the BGM1043N7 provides 15.1 dB gain, 1.5 dB noise figure and high linearity

performance. In addition BGM1043N7 provides very high out-of-band attenuation in conjunction with a high

input compression point. It can withstand IEC61000-4-2 ESD contact discharge at the RF input as high as 6 kV

in the application circuit shown in Figure 5. Its current consumption is as low as 4.0 mA. It operates over the 1.5

V to 3.6 V supply voltage range.

Figure 4 Block Diagram of BGM1043N7

Page 9: BGM1043N7 Front-End Module for Global Navigation Satellite

BGM1043N7 Low-Noise FEM for GPS Applications

Application Circuit and Block Diagram

Application Note AN294, Rev. 1.0 2012-07-23 9 / 23

4 Application Circuit and Block Diagram

The BGM1043N7 is internally matched at the output to 50 Ohm. The LNA bias circuitry is also integrated on

chip. Therefore, only three external components are required in the application. The application schematic is

shown in Figure 5 and the function of the external passives is listed in Table 2.

4.1 Application Schematic

Figure 5 Schematic diagram of the BGM1043N7 application circuit

Table 1 Pin Assignment of BGM1043N7

Pin No. Symbol Function

1 VCC Power Supply

2 PON Power ON/OFF

3 RFIN RF Input

4 SO Pre-Filter Output

5 AI LNA Input

6 RFOUT RF Output

7 GND DC and RF ground

Table 2 Bill-of-Materials

Symbol Value Unit Size Manufacturer Comment

C1 1.0 µF 0402 Various Supply filtering

C3 6.2 pF 0402 Various 787MHz Optimization

L1 5.8 nH 0402 Murata LQW Series Matching/ESD protection Inductor

L2 7.5 nH 0402 Murata LQW Series Matching Inductor

L3 7.3 nH 0402 Murata LQW Series 787MHz Optimization

Q1 BGM1043N7 TSNP-7-10 Infineon GPS/GLONASS FEM

Q1 BGM1043N7

(Topview)

RFOUT

SO

L2

7.5 nH

AI7 GND

1

2

3

6

5

4

VCC

C1

1 µF

PON

L1

5.8 nH

RFIN

L3

7.3 nH

C3

6.2 pF

Page 10: BGM1043N7 Front-End Module for Global Navigation Satellite

BGM1043N7 Low-Noise FEM for GPS Applications

Measurement Results

Application Note AN294, Rev. 1.0 2012-07-23 10 / 23

5 Measurement Results

Measurement results of the BGM1043N7 are presented in this section. The measurements are performed on

the Infineon application board at room temperature. The performances of the BGM1043N7 are here provided for

the voltage of 1.8V (Table 3) and 2.8V (Table 4). The data exclude PCB and SMA connector losses, unless

otherwise mentioned.

Table 3 Electrical Characteristics (at room temperature), Vcc = Vpon = 1.8 V

Parameter Symbol Value Unit Comment/Test Condition

DC Voltage Vcc 1.8 V

DC Current Icc 4.0 mA

Navigation System Sys GPS GLONASS

Frequency Range Freq 1575.42 1598-1606 MHz

Gain G 14.7 14.2 dB

Noise Figure NF 1.56 1.87 dB PCB and SMA connectors of 0.1 dB losses substracted

Input Return Loss RLin 12.3 15.4 dB

Output Return Loss RLout 24.3 24.0 dB

Reverse Isolation IRev 21.4 21.9 dB

Input P1dB IP1dB -8.38 -7.2 dBm fgps = 1575.42 MHz

f GLONASS = 1605 MHz

Output P1dB OP1dB 5.32 6.0 dBm

Input IP3

In-band IIP3 -6.8 -5.5 dBm

Output IP3

In-band OIP3 7.9 8.7 dBm

f1gps = 1575 MHz, f2gps = 1576MHz

f1GLONASS =1602 MHz, f2GLONASS =1603 MHz

P1IN = P2IN = -30 dBm

Rejection 750MHz1) Rej750M 70.1 dBc f = 750 MHz

Rejection 900MHz1) Rej900M 52.3 dBc f = 806 MHz - 928 MHz

Rejection 1800MHz1)

Rej1800M 43.0

dBc f = 1710 MHz - 1980 MHz

Rejection 2400MHz1)

Rej2400M 49.8

dBc f = 2400 MHz - 2500 MHz

Input P1dB IP1dB900M 29.0 dBm f = 900 MHz

Input P1dB IP1dB1710M 31.5 dBm f = 1710 MHz

LTE band-13 2nd

Harmonic

H2 -83.8 dBm fIN = 787.76 MHz, PIN = +15 dBm;

fH2 = 1575.52 MHz

Input IP3

out-of-band IIP3OOB 63.5 dBm

f1 = 1712.7 MHz, f2 = 1850 MHz

P1IN = +10 dBm, P2IN = +10 dBm;

fIIP3 = 1575.4 MHz

Stability k >1 -- Unconditionnally Stable from 0 to 10GHz

1) Rejection is defined as following: [Gain at 1575.42 MHz] – [Attenuation@stopband frequency]

Page 11: BGM1043N7 Front-End Module for Global Navigation Satellite

BGM1043N7 Low-Noise FEM for GPS Applications

Measurement Results

Application Note AN294, Rev. 1.0 2012-07-23 11 / 23

Table 4 Electrical Characteristics (at room temperature), Vcc = Vpon = 2.8 V

Parameter Symbol Value Unit Comment/Test Condition

DC Voltage Vcc 2.8 V

DC Current Icc 4.1 mA

Navigation System Sys GPS GLONASS

Frequency Range Freq 1575.42 1598-1606 MHz

Gain G 14.8 14.3 dB

Noise Figure NF 1.57 1.9 dB PCB and SMA connectors of 0.12 dB losses substracted

Input Return Loss RLin 12.8 16.5 dB

Output Return Loss RLout 23.3 23.2 dB

Reverse Isolation IRev 21.8 22.3 dB

Input P1dB IP1dB -6.47 -5.2 dBm fgps = 1575.42 MHz

f GLONASS = 1605 MHz

Output P1dB OP1dB 7.33 8.1 dBm

Input IP3

In-band IIP3 -6.7 -5.4 dBm

Output IP3

In-band OIP3 8.1 8.9 dBm

f1gps = 1575 MHz, f2gps = 1576MHz

f1GLONASS =1602 MHz, f2GLONASS =1603 MHz

Input power= -30 dBm

Rejection 750MHz1) Rej750M 70.2 dBc f = 750 MHz

Rejection 900MHz1) Rej900M 52.4 dBc f = 806 MHz - 928 MHz

Rejection 1800MHz1)

Rej1800M 43.0

dBc f = 1710 MHz - 1980 MHz

Rejection 2400MHz1)

Rej2400M 49.9

dBc f = 2400 MHz - 2500 MHz

Input P1dB IP1dB900M 30.0 dBm f = 900 MHz

Input P1dB IP1dB1710M 32.0 dBm f = 1710 MHz

LTE band-13 2nd

Harmonic

H2 -84.0 dBm fIN = 787.76 MHz, PIN = +15 dBm;

fH2 = 1575.52 MHz

Input IP3

out-of-band IIP3OOB 63.6 dBm

f1 = 1712.7 MHz, f2 = 1850 MHz

P1IN = +10 dBm, P2IN = +10 dBm;

fIIP3 = 1575.4 MHz

Stability k >1 -- Unconditionnally Stable from 0 to 10GHz

1)

Rejection is defined as following: [Gain at 1575.42 MHz] – [Attenuation@stopband frequency]

Page 12: BGM1043N7 Front-End Module for Global Navigation Satellite

BGM1043N7 Low-Noise FEM for GPS Applications

Measured Graphs for GPS and GLONASS Bands

Application Note AN294, Rev. 1.0 2012-07-23 12 / 23

6 Measured Graphs for GPS and GLONASS Bands

Figure 6 Wideband Insertion Power Gain of BGM1043N7

Figure 7 Narrowband Insertion Power Gain of BGM1043N7 for GPS and GLONASS bands

0 500 1000 1500 2000 2500 3000 3500 4000 4500 5000 5500 6000

Frequency (MHz)

Gain

-70

-60

-50

-40

-30

-20

-10

0

10

20

S2

1 (

dB

)

787.76 MHz-64.8 dB

1575.4 MHz14.8 dB

Gain at Vcc=1.8V

Gain at Vcc=2.8V

1500 1525 1550 1575 1600 1625 1650

Frequency (MHz)

Narrowband gain

13

13.6

14.2

14.8

15.4

16

S2

1 (

dB

)

1605.4 MHz14.2 dB

1605.4 MHz14.3 dB

1575.4 MHz14.8 dB

1575.4 MHz14.7 dB

Gain at Vcc=1.8V

Gain at Vcc=2.8V

Page 13: BGM1043N7 Front-End Module for Global Navigation Satellite

BGM1043N7 Low-Noise FEM for GPS Applications

Measured Graphs for GPS and GLONASS Bands

Application Note AN294, Rev. 1.0 2012-07-23 13 / 23

Figure 8 Input Matching of BGM1043N7 for GPS and GLONASS bands

Figure 9 Output Matching of BGM1043N7 for GPS and GLONASS bands

1500 1525 1550 1575 1600 1625 1650

Frequency (MHz)

Input matching

-35

-30

-25

-20

-15

-10

-5

0

S1

1 (

dB

)

1605.4 MHz-16.5 dB

1605.4 MHz-15.4 dB

1575.4 MHz-12.8 dB

1575.4 MHz-12.3 dB

S11 at Vcc=1.8V

S11 at Vcc=2.8V

1500 1525 1550 1575 1600 1625 1650

Frequency (MHz)

Output matching

-35

-30

-25

-20

-15

-10

-5

0

S2

2 (

dB

)

1605.4 MHz-23.2 dB

1605.4 MHz-24 dB

1575.4 MHz-23.3 dB

1575.4 MHz-24.3 dB

S22 at Vcc=1.8V

S22 at Vcc=2.8V

Page 14: BGM1043N7 Front-End Module for Global Navigation Satellite

BGM1043N7 Low-Noise FEM for GPS Applications

Measured Graphs for GPS and GLONASS Bands

Application Note AN294, Rev. 1.0 2012-07-23 14 / 23

Figure 10 Reverse Isolation of BGM1043N7 for GPS and GLONASS bands

Figure 11 Noise Figure of BGM1043N7 for GPS and GLONASS bands

1500 1525 1550 1575 1600 1625 1650

Frequency (MHz)

Isolation

-27

-25

-23

-21

-19

-17

S1

2 (

dB

)

1605.4 MHz-22.3 dB

1605.4 MHz-21.9 dB

1575.4 MHz-21.8 dB

1575.4 MHz-21.4 dB

S12 at Vcc=1.8V

S12 at Vcc=2.8V

1559 1567 1575 1583 1591 1599 1607 1615

Frequency (MHz)

Noise figure

1

1.2

1.4

1.6

1.8

2

2.2

2.4

2.6

2.8

3

NF

(d

B)

1605.4 MHz1.87

1605.4 MHz1.9

1575.4 MHz1.56

1575.4 MHz1.57

NF at Vcc=1.8V

NF at Vcc=2.8V

Page 15: BGM1043N7 Front-End Module for Global Navigation Satellite

BGM1043N7 Low-Noise FEM for GPS Applications

Measured Graphs for GPS and GLONASS Bands

Application Note AN294, Rev. 1.0 2012-07-23 15 / 23

Figure 12 Input 1dB Compression Point of BGM1043N7 at supply voltage of 1.8V for GPS band

Figure 13 Input 1dB Compression Point of BGM1043N7 at supply voltage of 2.8V for GPS band

-30 -25 -20 -15 -10 -5 0

Power (dBm)

Compression point at 1dB with Vcc=1.8V

10

11

12

13

14

15

16

Ga

in (

dB

)

-8.38 dBm13.7 dB

-30 dBm14.7 dB

-30 -25 -20 -15 -10 -5 0

Power (dBm)

Compression point at 1dB with Vcc=2.8V

10

11

12

13

14

15

16

Ga

in (

dB

)

-6.47 dBm13.8 dB

-30 dBm14.8 dB

Page 16: BGM1043N7 Front-End Module for Global Navigation Satellite

BGM1043N7 Low-Noise FEM for GPS Applications

Measured Graphs for GPS and GLONASS Bands

Application Note AN294, Rev. 1.0 2012-07-23 16 / 23

Figure 14 Carrier and intermodulation products of BGM1043N7 for GPS band at Vcc=1.8V

Figure 15 Carrier and intermodulation products of BGM1043N7 for GPS band at Vcc=2.8V

1573 1574 1575 1576 1577 1578

Frequency (MHz)

Intermodulation for GPS band

-90

-80

-70

-60

-50

-40

-30

-20

-10

0

Po

we

r (d

Bm

)

1577 MHz-62.45

1574 MHz-63.62

1576 MHz-15.55

1575 MHz-15.48

1573 1574 1575 1576 1577 1578

Frequency (MHz)

Intermodulation for GPS band

-90

-80

-70

-60

-50

-40

-30

-20

-10

0

Po

we

r (d

Bm

)

1574 MHz-63.63

1577 MHz-62.58

1576 MHz-15.46

1575 MHz-15.39

Page 17: BGM1043N7 Front-End Module for Global Navigation Satellite

BGM1043N7 Low-Noise FEM for GPS Applications

Measured Graphs for GPS and GLONASS Bands

Application Note AN294, Rev. 1.0 2012-07-23 17 / 23

Figure 16 Carrier and intermodulation products of BGM1043N7 for GLONASS band at Vcc=1.8V

Figure 17 Carrier and intermodulation products of BGM1043N7 for GLONASS band at Vcc=2.8V

1600 1601 1602 1603 1604 1605

Frequency (MHz)

Intermodulation for GLONASS band

-90

-80

-70

-60

-50

-40

-30

-20

-10

0

Po

we

r (d

Bm

)

1601 MHz-65.18

1602 MHz-15.72

1604 MHz-64.63

1603 MHz-15.78

1600 1601 1602 1603 1604 1605

Frequency (MHz)

Intermodulation for GLONASS band

-90

-80

-70

-60

-50

-40

-30

-20

-10

0

Po

we

r (d

Bm

)

1604 MHz-64.74

1602 MHz-15.61

1603 MHz-15.67

1601 MHz-65.05

Page 18: BGM1043N7 Front-End Module for Global Navigation Satellite

BGM1043N7 Low-Noise FEM for GPS Applications

Miscellaneous Measured Graphs

Application Note AN294, Rev. 1.0 2012-07-23 18 / 23

7 Miscellaneous Measured Graphs

Figure 18 Input and Output Matching of BGM1043N7 for GPS and GLONASS bands with Vcc=1.8V

Figure 19 Input and Output Matching of BGM1043N7 for GPS and GLONASS bands with Vcc=2.8V

0 1.0

1.0

-1.0

10.0

10.0

-10.0

5.0

5.0

-5.0

2.0

2.0

-2.0

3.0

3.0

-3.0

4.0

4.0

-4.0

0.2

0.2

-0.2

0.4

0.4

-0.4

0.6

0.6

-0.6

0.8

0.8

-0.8

Input and Output matching with Vcc=1.8VSwp Max

1615MHz

Swp Min

1559MHz

1605.4 MHzr 1.29x -0.32

1605.4 MHzr 1.04x -0.00977

1575.4 MHzr 0.98x 0.0959

1575.4 MHzr 1.13x -0.529

Input

Output

0 1.0

1.0

-1.0

10.0

10.0

-10.0

5.0

5.0

-5.0

2.0

2.0

-2.0

3.0

3.0

-3.0

4.0

4.0

-4.0

0.2

0.2

-0.2

0.4

0.4

-0.4

0.6

0.6

-0.6

0.8

0.8

-0.8

Input and Output matching with Vcc=2.8VSwp Max

1615MHz

Swp Min

1559MHz

1605.4 MHzr 1.28x -0.285

1605.4 MHzr 1.03x 0.0419

1575.4 MHzr 0.958x 0.139

1575.4 MHzr 1.16x -0.501

Input

Output

Page 19: BGM1043N7 Front-End Module for Global Navigation Satellite

BGM1043N7 Low-Noise FEM for GPS Applications

Miscellaneous Measured Graphs

Application Note AN294, Rev. 1.0 2012-07-23 19 / 23

Figure 20 Stability Factor K of BGM1043N7 upto 10 GHz

Figure 21 Stability Factor µ1 of BGM1043N7 upto 10 GHz

0 1000 2000 3000 4000 5000 6000 7000 8000 9000 10000

Frequency (MHz)

Stability K factor

0

1

2

3

4

5

1575.4 MHz1.24

Stability K factor at Vcc=1.8V

Stability K factor at Vcc=2.8V

0 1000 2000 3000 4000 5000 6000 7000 8000 9000 10000

Frequency (MHz)

Stability Mu1 factor

0

1

2

3

4

5

1575.4 MHz1.64

Stability Mu1 factor at Vcc=1.8V

Stability Mu1 factor at Vcc=2.8V

Page 20: BGM1043N7 Front-End Module for Global Navigation Satellite

BGM1043N7 Low-Noise FEM for GPS Applications

Miscellaneous Measured Graphs

Application Note AN294, Rev. 1.0 2012-07-23 20 / 23

Figure 22 Stability Factor µ2 of BGM1043N7 upto 10 GHz

0 1000 2000 3000 4000 5000 6000 7000 8000 9000 10000

Frequency (MHz)

Stability Mu2 factor

0

1

2

3

1575.4 MHz1.42

Stability Mu2 factor at Vcc=1.8V

Stability Mu2 factor at Vcc=2.8V

Page 21: BGM1043N7 Front-End Module for Global Navigation Satellite

BGM1043N7 Low-Noise FEM for GPS Applications

Evaluation Board and Layout Information

Application Note AN294, Rev. 1.0 2012-07-23 21 / 23

8 Evaluation Board and Layout Information

In this application note, the following PCB is used:

PCB Marking: BGM1032N7 V3.0 M110416

PCB material: FR4

Figure 23 Picture of Evaluation Board for BGM1043N7

Figure 24 PCB Layer Information

Copper

35µm

FR4, 0.2mm

FR4, 0.8mm

Vias

Page 22: BGM1043N7 Front-End Module for Global Navigation Satellite

BGM1043N7 Low-Noise FEM for GPS Applications

Authors

Application Note AN294, Rev. 1.0 2012-07-23 22 / 23

9 Authors

Jagjit Singh Bal, Senior Application Engineer of Business Unit “RF and Protection Devices”

Dr. Chih-I Lin, Senior Staff Engineer of Business Unit “RF and Protection Devices”

Page 23: BGM1043N7 Front-End Module for Global Navigation Satellite

w w w . i n f i n e o n . c o m

Published by Infineon Technologies AG AN294