SILABS GSM850 Single 8x8 mm package cmos process technology intergrated gsm/gprs transceiver including Datasheet

Aero I
A E R O ™ I TR A N S C E I V E R
FOR GSM AND GPRS WIRELESS COMMUNICATIONS
Features
Applications
„
„
Multi-band GSM/GPRS digital cellular handsets
Multi-band GSM/GPRS wireless data modems
Description
The Aero I transceiver is a complete RF front end for multi-band GSM
and GPRS wireless communications. The transmit section interfaces
between the baseband processor and the power amplifier. The receive
section interfaces between the RF band-select SAW filters and the
baseband processor. All sensitive components, such as RF/IF VCOs,
loop filters, and tuning inductors, are completely integrated into a single
compact package.
DIAG2
DIAG1
RFOG
RFOD
28
27
26
25
24
23
22
31
RXQN
1
21
RFIGN
RXIP
2
20
RFIGP
RXIN
3
19
RFIDN
TXIP
4
18
RFIDP
TXIN
5
17
RFIPN
TXQP
6
16
RFIPP
TXQN
7
15
GND
29
30
GND
GND
GND
GND
8
9
10
11
12
13
14
SDI
„
32
SCLK
„
GPRS Class 12 compliant
3-wire serial interface
2.7 V to 3.0 V operation
SEN
z
„
Si4205-BM
(For pin description see page 33)
XEN
z
GSM 850 Class 4, small MS
E-GSM 900 Class 4, small MS
DCS 1800 Class 1
PCS 1900 Class 1
SDO
z
RXQP
z
PDN
„
Quad-band support:
XOUT
„
„
XIN
„
Single 8 x 8 mm package
CMOS process technology
Integrated GSM/GPRS
transceiver including:
z Low-IF receiver
z Universal baseband interface
z Offset-PLL transmitter
z Dual RF synthesizer
Integrated VCOs, frequency
synthesizers, and tuning inductors
VDD
„
Pin Assignments
(Top View)
Ordering Information:
See page 34.
Patents pending
Functional Block Diagram
PGA
ADC
PGA
ADC
LNA
PCS
LNA
0 / 90
GSM
DCS
PCS
DAC
I
PGA
DAC
Q
XOUT
100 kHz
I
DET
PA
I
Q
PA
RF
PLL
Rev. 1.0 12/03
PGA
BASEBAND
DCS
ANTENNA SWITCH
Si4205
LNA
CHANNEL
FILTER
GSM
IF
PLL
VC-TCXO
13 or 26 MHz
XIN
AFC
Copyright © 2003 by Silicon Laboratories
Aero I
Aero I
2
Rev. 1.0
Aero I
TA B L E O F C O N T E N TS
Section
Page
Electrical Specifications . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .4
Typical Application Schematic . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 14
Bill of Materials . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 15
Functional Description . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 16
Receiver . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 17
Transmitter . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 18
Frequency Synthesizer . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 19
Serial Interface . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 20
XOUT Buffer . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 20
Control Registers . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 21
Pin Descriptions: Si4205-BM . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .33
Ordering Guide . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 34
Package Outline: Si4205-BM . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .35
Document Change List . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .36
Contact Information . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .38
Rev. 1.0
3
Aero I
Electrical Specifications
Table 1. Recommended Operating Conditions
Parameter
Ambient Temperature
DC Supply Voltage
Symbol
Test Condition
Min
Typ
Max
Unit
TA
–20
25
85
°C
VDD
2.7
2.85
3.0
V
Note: All minimum and maximum specifications are guaranteed and apply across the recommended operating conditions.
Typical values apply at 2.85 V and an operating temperature of 25 °C unless otherwise stated. Parameters are tested in
production unless otherwise stated.
Table 2. Absolute Maximum Ratings1,2
Parameter
Symbol
Value
Unit
VDD
–0.5 to 3.3
V
Input Current3
IIN
±10
mA
Input Voltage3
VIN
–0.3 to (VDD + 0.3)
V
Operating Temperature Range
TOP
–40 to 95
°C
Storage Temperature Range
TSTG
–55 to 150
°C
10
dBm
DC Supply Voltage
RF Input Level4
Notes:
1. Permanent device damage may occur if the above Absolute Maximum Ratings are exceeded. Functional operation
should be restricted to the conditions as specified in the operational sections of this data sheet. Exposure to absolute
maximum rating conditions for extended periods may affect device reliability.
2. The Si4205 device is high-performance RF integrated circuit with an ESD rating of < 2 kV. Handling and
assembly of this device should only be done at ESD-protected workstations.
3. For signals SCLK, SDI, SEN, PDN, XEN, and XIN.
4. At SAW filter output for all bands.
4
Rev. 1.0
Aero I
Table 3. DC Characteristics
(VDD = 2.7 to 3.0 V, TA = –20 to 85 °C)
Parameter
Supply Current
1
Symbol
Test Condition
Min
Typ
Max
Unit
IRX
Receive mode
—
80
111
mA
ITX
Transmit mode
—
82
107
mA
IXOUT
PDN = 0, XEN = 1
—
1
2
mA
IPDN
PDN = 0, XEN = 0,
XBUF = 0, XPD1 = 1
—
5
80
µA
High Level Input Voltage2
VIH
0.7 VDD
—
—
V
Voltage2
VIL
—
—
0.3 VDD
V
High Level Input Current2
IIH
VIH = VDD = 3.0 V
–10
—
10
µA
Low Level Input Current2
IIL
VIL = 0 V,
VDD = 3.0 V
–10
—
10
µA
High Level Output Voltage3
VOH
IOH = –500 µA
VDD–0.4
—
—
V
3
VOL
IOL = 500 µA
—
—
0.4
V
High Level Output Voltage4
VOH
IOH = –10 mA
VDD–0.4
—
—
V
Low Level Output Voltage4
VOL
IOL = 10 mA
—
—
0.4
V
Low Level Input
Low Level Output Voltage
Notes:
1. Measured with load on XOUT pin of 10 pF and fREF = 13 MHz. Limits with XEN = 1 guaranteed by characterization.
2. For pins SCLK, SDI, SEN, XEN, and PDN.
3. For pins SDO, XOUT.
4. For pins DIAG1, DIAG2.
Rev. 1.0
5
Aero I
Table 4. AC Characteristics
(VDD = 2.7 to 3.0 V, TA = –20 to 85 °C)
Symbol
Test Condition
Min
Typ
Max
Unit
SCLK Cycle Time
tCLK
Figures 1, 3
35
—
—
ns
SCLK Rise Time
tR
Figures 1, 3
—
—
50
ns
SCLK Fall Time
tF
Figures 1, 3
—
—
50
ns
SCLK High Time
tHI
Figures 1, 3
10
—
—
ns
SCLK Low Time
tLO
Figures 1, 3
10
—
—
ns
PDN Rise Time
tPR
Figure 2
—
—
10
ns
PDN Fall Time
tPF
Figure 2
—
—
10
ns
SDI Setup Time to SCLK↑
tSU
Figure 3
15
—
—
ns
SDI Hold Time from SCLK↑
tHOLD
Figure 3
10
—
—
ns
SEN↓ to SCLK↑ Delay Time
tEN1
Figure 3
10
—
—
ns
SCLK↑ to SEN↑ Delay Time
tEN2
Figures 3, 4
12
—
—
ns
SEN↑ to SCLK↑ Delay Time
tEN3
Figures 3, 4
12
—
—
ns
tW1, tW3
Figures 3, 4
10
—
—
ns
DGAIN bits only
130
—
—
µs
tW2
Option 2 only
10
—
—
ns
tCA
Figure 4
—
—
27
ns
—
—
5
pF
Parameter
SEN Pulse Width1
SCLK↓ to SDO Time
Digital Input Pin Capacitance2
XIN Input Resistance3
RXIN
10
15
20
kΩ
XIN Input Capacitance3
CXIN
7
10
14
pF
VREF
0.5
—
—
VPP
XSEL = 0, DIV2 = 0
—
13
—
MHz
XSEL = 1, DIV2 = 1
—
26
—
MHz
XIN Input
Sensitivity3
XIN Input Frequency3,4
fREF
Notes:
1. Two programming options are allowed for SEN. Either option may be used. In both cases, the SEN pulse width must be
at least 10 ns after writing all registers except after DGAIN is written. After DGAIN is written, SEN must be held high for
at least 130 µs. See “AN50: Aero Transceiver Programming Guide.”
2. For pins SCLK, SDI, SEN, XEN, and PDN.
3. For XIN pin.
4. The XSEL and DIV2 bits control internal divide-by-two circuits and do not effect the XOUT pin.
6
Rev. 1.0
Aero I
tR
SCLK
tF
80%
50%
20%
tHI
tCLK
tLO
Figure 1. SCLK Timing Diagram
tPR
tPF
80%
PDN
20%
Figure 2. PDN Timing Diagram
80%
D17
SDI 50%
D16
A0
D17
20%
tSU
tHOLD
80%
SCLK 50%
20%
tR
tEN 1
80%
SEN 50%
(option 1) 20%
tL O
tH I
tF
tEN 2
tEN 3
tCLK
tW 1
80%
SEN 50%
(option 2) 20%
tW 2
tW 3
Figure 3. Serial Interface Write Timing Diagram
80%
SDI 50%
A0
20%
80%
OD17
SDO 50%
OD16
OD0
20%
tCA
80%
SCLK 50%
20%
tEN2
tEN3
80%
SEN 50%
20%
tW1
Figure 4. Serial Interface Read Timing Diagram
Rev. 1.0
7
Aero I
Table 5. Receiver Characteristics
(VDD = 2.7 to 3.0 V, TA = –20 to 85 °C)
Parameter
1
GSM Input Frequency
DCS or PCS Input Frequency
Noise Figure at 25
Noise Figure at 85 °C
3 MHz Input
Test Condition
Min
Typ
Max
Unit
fIN
GSM 850 band
869
—
894
MHz
E-GSM 900 band
925
—
960
MHz
DCS 1800 band
1805
—
1880
MHz
PCS 1900 band
1930
—
1990
MHz
GSM 850 band
—
2.9
3.8
dB
E-GSM 900 band
—
3.0
3.9
dB
DCS 1800 band
—
3.3
4.1
dB
PCS 1900 band
—
3.7
4.5
dB
GSM 850 band
—
3.6
4.5
dB
E-GSM 900 band
—
3.7
4.6
dB
DCS 1800 band
—
4.2
5.0
dB
PCS 1900 band
—
4.9
5.7
dB
GSM 850 band
—
3.7
4.6
dB
E-GSM 900 band
—
3.8
4.7
dB
DCS 1800 band
—
4.6
5.4
dB
PCS 1900 band
—
5.2
6.0
dB
GSM input
–25
–21
—
dBm
DCS/PCS inputs
–28
–25
—
dBm
GSM input
–21
–16
—
dBm
DCS/PCS inputs
–19
–15
—
dBm
1
°C2,3
Noise Figure at 75 °C
Symbol
NF25
2,3
NF75
2,3
NF85
Desensitization2,3,4
20 MHz Input Desensitization
2,3,4
DES3
DES20
2
Input IP2
IP2
|f1,2 – f0| ≥ 6 MHz,
|f2 – f1| = 100 kHz
29
40
—
dBm
Input IP32
IP3
|f2 – f1| ≥ 800 kHz,
f0 = 2f1 – f2
–18
–12
—
dBm
Image Rejection2,4
IR
GSM Input
28
35
—
dB
DCS/PCS Inputs
28
40
—
dB
GSM Input
–28
–23
—
dBm
DCS/PCS inputs
–27
–22
—
dBm
GSM Input
–23
–18
—
dBm
DCS/PCS inputs
–23
–18
—
dBm
GSM input
3
8.5
12.5
dB
DCS/PCS inputs
10
15.5
19.5
dB
GSM input
100
104
109
dB
DCS/PCS inputs
96
102
107
dB
GSM input
—
17
—
dB
DCS/PCS inputs
—
15
—
dB
GSM input
13
17
21
dB
DCS/PCS inputs
4
8
12
dB
2,5
1 dB Input Compression
1 dB Input
Compression2,6
Minimum Voltage Gain
2,6,7
Maximum Voltage Gain
LNA Voltage
2,7
Gain3,8
LNA Gain Control Range
8
CPMAX
CPMIN
GMIN
GMAX
GLNA
∆GLNA
Rev. 1.0
Aero I
Table 5. Receiver Characteristics (Continued)
(VDD = 2.7 to 3.0 V, TA = –20 to 85 °C)
Parameter
Symbol
Analog PGA Control Range
∆GAPGA
Test Condition
Min
Typ
Max
Unit
13
16
19
dB
3.2
4.0
4.8
dB
—
63
—
dB
—
1
—
dB
DACFS[1:0] = 00
0.7
1.0
1.3
VPPD
DACFS[1:0] = 01
1.5
2.0
2.5
VPPD
DACFS[1:0] = 10
2.6
3.5
4.4
VPPD
DACCM[1:0] = 00
0.8
1.0
1.2
V
DACCM[1:0] = 01
1.05
1.25
1.45
V
DACCM[1:0] = 10
1.15
1.35
1.55
V
Differential Output Offset Voltage
—
—
16
mV
Differential Output Offset Voltage Drift9,10,11
—
—
5
mV
Baseband Gain Error9,11
—
—
1
%
—
—
1
deg
Analog PGA Step Size
∆GDPGA
Digital PGA Control Range
Digital PGA Step Size
Maximum Differential Output Voltage
Output Common Mode Voltage
9
9
9,10,11
Baseband Phase Error
9,11
9
Output Load Resistance
RL
Single-ended
10
—
—
kΩ
Output Load Capacitance9
CL
Single-ended
—
—
10
pF
CSEL = 0
—
—
22
µs
CSEL = 1
—
—
16
µs
CSEL = 0
—
—
1.5
µs
CSEL = 1
—
—
1
µs
From powerdown
—
200
220
µs
Group Delay12
Differential Group
Delay12
3,13
Powerup Settling Time
Notes:
1. GSM input pins RFIGP and RFIGN. DCS input pins RFIDP and RFIDN. PCS input pins RFIPP and RFIPN.
2. Measurement is performed with a 2:1 balun (50 Ω input, 200 Ω balanced output) and includes matching network and
PCB losses. Measured at max gain (AGAIN[2:0] =100b, LNAG[1:0] = 01b, LNAC[1:0] = 01b) unless otherwise noted.
Noise figure measurements are referred to 290 °K. Insertion loss of the balun is removed.
3. Specifications guaranteed by characterization using LQW15AN series matching inductors.
4. Input signal at balun is –102 dBm. SNR at baseband output is 9 dB.
5. AGAIN[2:0]=min=000b, LNAG[1:0] = max=01b, LNAC[1:0] =max= 01b.
6. AGAIN[2:0]=min=000b, LNAG[1:0] = min=00b, LNAC[1:0] = min=00b.
7. Voltage gain is defined as the differential rms voltage at the RXIP/RXIN pins or RXQP/RXQN pins divided by the rms
voltage at the balun input with DACFS[1:0] = 01 and CSEL = 1. Gain is 1.5 dB higher with CSEL = 0. Minimum and
maximum values do not include the variation in the DAC full scale voltage (also see Maximum Differential Output
Voltage specification).
8. Voltage gain is defined as the differential rms voltage at the LNA output divided by the rms voltage at the balun output.
9. Output pins RXIP, RXIN, RXQP, RXQN.
10. Specified as root sum square:
2
2 . Drift specification applies to dc offset
( RXIP – RXIN ) + ( RXQP – RXQN )
calibration and is guaranteed by characterization. See ZERODEL[2:0] in the register description.
11. The baseband signal path is entirely digital. Gain, phase, and offset errors at the baseband outputs are because of the
D/A converters. Offsets can be measured and calibrated out. See ZERODEL[2:0] in the register description.
12. Group delay is measured from antenna input to baseband outputs. Differential group delay is measured in-band.
13. Includes settling time of the frequency synthesizer. Settling to 5 degrees phase error measured at RXIP, RXIN, RXQP,
and RXQN pins.
Rev. 1.0
9
Aero I
Receive Path Magnitude Response (CSEL = 0)
Receive Path Magnitude Response (CSEL = 1)
0
0
−20
−20
Magnitude (dB)
Magnitude (dB)
−40
−60
−40
−80
−60
−100
−120
0
50
100
150
200
Frequency (KHz)
250
300
350
−80
400
0
50
100
150
200
Frequency (KHz)
250
300
350
400
Figure 5. Receive Path Magnitude Response (CSEL = 0 and CSEL = 1)
Receive Path Passband Magnitude Response (CSEL = 1)
2
0
0
−2
−2
−4
−4
Magnitude (dB)
Magnitude (dB)
Receive Path Passband Magnitude Response (CSEL = 0)
2
−6
−8
−6
−8
−10
−10
−12
−12
−14
−14
−16
0
10
20
30
40
50
Frequency (KHz)
60
70
80
90
100
−16
0
10
20
30
40
50
Frequency (KHz)
60
70
80
90
100
90
100
Figure 6. Receive Path Passband Magnitude Response (CSEL = 0 and CSEL = 1)
Receive Path Passband Group Delay (CSEL = 1)
20
24
19
23
18
22
17
21
16
Group Delay (uSec)
Group Delay (uSec)
Receive Path Passband Group Delay (CSEL = 0)
25
20
19
15
14
18
13
17
12
16
11
15
0
10
20
30
40
50
Frequency (KHz)
60
70
80
90
10
100
0
10
20
30
40
50
Frequency (KHz)
60
70
Figure 7. Receive Path Passband Group Delay (CSEL = 0 and CSEL = 1)
10
Rev. 1.0
80
Aero I
Table 6. Transmitter Characteristics
(VDD = 2.7 to 3.0 V, TA = –20 to 85 °C)
Parameter
Test Condition
Min
Typ
Max
Unit
GSM 850 band
824
—
849
MHz
E-GSM 900 band
880
—
915
MHz
DCS 1800 band
1710
—
1785
MHz
PCS 1900 band
1850
—
1910
MHz
I/Q Differential Input Swing3,4
0.88
—
2.2
VPPD
I/Q Input Common-Mode3
1.1
—
1.4
V
BBG[1:0] = 11b
26
30
35
kΩ
BBG[1:0] = 00b
22
25
29
kΩ
BBG[1:0] = 01b
17
20
23
kΩ
Powered down
—
Hi-Z
—
kΩ
I/Q Input Capacitance3,5
—
—
5
pF
I/Q Input Bias Current3
13
16
19
µA
RFOG Output Frequency1
RFOD Output Frequency2
I/Q Differential Input Resistance3,4
Symbol
Sideband Suppression
67.7 kHz sinusoid
—
–46
–34
dBc
Carrier Suppression
67.7 kHz sinusoid
—
–48
–33
dBc
IM3 Suppression
67.7 kHz sinusoid
—
–57
–50
dBc
—
1.9
3.0
o
—
5
10
o
Open loop
—
100
—
kHz/V
VSWR 2:1, all phases,
open loop
—
200
—
kHzPP
400 kHz offset
—
–65
–63
dBc
1.8 MHz offset
—
–70
–68
dBc
400 kHz offset
—
–65
–63
dBc
1.8 MHz offset
—
–70
–65
dBc
10 MHz offset
—
–160
–155
dBc/Hz
20 MHz offset
—
–166
–164
dBc/Hz
20 MHz offset
—
–163
–157
dBc/Hz
RFOG Output Power Level1
ZL = 50 Ω
7
9
11
dBm
RFOD Output Power Level2
ZL = 50 Ω
6
8
10
dBm
Phase Error5
TXVCO Pushing1,2
TXVCO Pulling1,2
RFOG Output Modulation Spectrum1,6
RFOD Output Modulation Spectrum2,6
RFOG Output Phase Noise1,5,7
RFOD Output Phase Noise2,5,7
Rev. 1.0
rms
PEAK
11
Aero I
Table 6. Transmitter Characteristics (Continued)
(VDD = 2.7 to 3.0 V, TA = –20 to 85 °C)
Parameter
RF Output Harmonic Suppression1,2
Powerup Settling Time5,8
Symbol
Test Condition
Min
Typ
Max
Unit
2nd harmonic
—
—
–20
dBc
3rd harmonic
—
—
–10
dBc
From powerdown
—
—
150
µs
Notes:
1. Measured at RFOG pin.
2. Measured at RFOD pin.
3. Input pins TXIP, TXIN, TXQP, and TXQN.
4. Differential Input Swing is programmable with the BBG[1:0] bits in register 04h. Program these bits to the closest
appropriate value. The I/Q Input Resistance scales inversely with the BBG[1:0] setting.
5. Specifications guaranteed by characterization.
6. Measured with pseudo-random pattern. Carrier power and noise power < 1.8 MHz measured with 30 kHz RBW. Noise
power ≥ 1.8 MHz measured with 100 kHz RBW.
7. Measured with all 1s pattern.
8. Including settling time of the frequency synthesizer. Settling time measured at the RFOD and RFOG pins to 0.1 ppm
frequency error.
12
Rev. 1.0
Aero I
Table 7. Frequency Synthesizer Characteristics
(VDD = 2.7 to 3.0 V, TA = –20 to 85 °C)
Parameter
Symbol
Test Condition
Min
Typ
Max
Unit
fRF1
GSM 850 band
1737.8
—
1787.8
MHz
E-GSM 900 band
1849.8
—
1919.8
MHz
DCS 1800 band
1804.9
—
1879.9
MHz
PCS 1900 band
1929.9
—
1989.9
MHz
GSM 850 band
1272
—
1297
MHz
E-GSM 900
1279
—
1314
MHz
DCS 1800 band
1327
—
1402
MHz
PCS 1900 band
1423
—
1483
MHz
GSM 850 band
—
896
—
MHz
E-GSM 900 band
880–895 MHz
900–915 MHz
—
798
—
MHz
E-GSM 900 band
895–900 MHz
—
790
—
MHz
DCS 1800 band
—
766
—
MHz
PCS 1900 band
—
854
—
MHz
GSM input,
RFUP = 0
—
200
—
kHz
DCS/PCS inputs,
RFUP = 1
—
100
—
kHz
—
200
—
kHz
—
500
—
kHz/V
—
400
—
kHz/V
—
300
—
kHz/V
—
400
—
kHzPP
—
100
—
kHzPP
—
100
—
kHzPP
3 MHz offset
—
–144
–138
dBc/Hz
RF2 PLL Phase Noise2
400 kHz offset
—
–126
–121
dBc/Hz
IF PLL Phase Noise2
400 kHz offset
—
–128
–123
dBc/Hz
3 MHz offset
—
–95
–83
dBc
400 kHz offset
—
–80
–75
dBc
400 kHz offset
—
–80
–70
dBc
RF1 VCO Frequency1
RF2 VCO Frequency1
fRF2
IF VCO Frequency1
fIF
RF1 PLL Phase Detector Update
Frequency
IF and RF2 PLL Phase Detector
Update Frequency
RF1 VCO Pushing2
RF2 VCO
fφ
Open Loop
Pushing2
IF VCO Pushing
2
RF1 VCO Pulling2
VSWR = 2:1,
all phases, open loop
RF2 VCO Pulling2
IF VCO Pulling
2
RF1 PLL Phase Noise
RF1 PLL Spurious
RF2 PLL
fφ
2
Spurious2
IF PLL Spurious2
2
Notes:
1. For the GSM input, the RF1 VCO is divided by two. During transmit, the IF VCO is divided by two.
2. Specifications are guaranteed by characterization.
Rev. 1.0
13
Aero I
Typical Application Schematic
RFOG
DIAG1
DIAG2
XEN
XOUT
RFOD
C1
L1
32
1
2
3
4
5
6
7
RXQN
RXIP
RXIN
TXIP
TXIN
TXQP
TXQN
RXQN
RXIP
RXIN
TXIP
TXIN
TXQP
TXQN
GND
U1
Si4205
GND
31
RFIGN
RFIGP
RFIDN
RFIDP
RFIPN
RFIPP
GND
21
20
19
18
17
16
15
GND
30
OUT+
IN
OUT-
GND
GSM900 IN
C2
C3
L2
Z2
OUT+
IN
OUT-
GND
DCS 1800 IN
C4
8
9
10
11
12
13
14
29
VDD
XIN
VDD
PDNB
SDO
SENB
SCLK
SDI
VDD
C8
RXQP
XOUT
XEN
DIAG2
DIAG1
RFOG
RFOD
28
27
26
25
24
23
22
RXQP
Z1
R1
XIN
VDD
C7
C5
L3
SDI
SCLK
SENB
PDNB
SDO
Z3
OUT+
IN
OUT-
GND
PCS 1900 IN
C6
Notes:
1. Connect pads on bottom of U1 to GND.
2. See “AN92: Aero™ I/Aero™ I+ Transceiver PCB Layout Guidelines” for details on the following:
z LNA matching network (C1–C6, L1–L3). Values should be custom tuned for a specific PCB layout and SAW filter to
optimize performance.
z Differential traces between the SAW filters (Z1–Z3) and transceiver (U1) pins 16–21.
z Detailed SAW filter requirements.
3. For the XIN input, no external ac coupling is required.
4. For optimum performance, connect pin 31 to ground plane of power amplifier through several vias close to pin.
14
Rev. 1.0
Aero I
Bill of Materials
Component
Value/Description
Supplier(s)
C1–C2
1.2 pF, ±0.1 pF, C0G
(GSM 850 and E-GSM 900)
Murata GRM36C0G series
Venkel C0402C0G500 series
C3–C4
1.2 pF, ±0.1 pF, C0G
(DCS 1800)
Murata GRM36C0G series
Venkel C0402C0G500 series
C5–C6
1.5 pF, ±0.1 pF, C0G
(PCS 1900)
Murata GRM36C0G series
Venkel C0402C0G500 series
C7
22 nF, ±20%, Z5U
C8
10 pF, ±20%, C0G
L1
24 nH, ±2%
Murata LQG15HN series (0402 size)
Murata LQW15AN series (0402 size)
L2
6.8 nH, ±0.2 nH
Murata LQG15HN series (0402 size)
Murata LQW15AN series (0402 size)
L3
5.6 nH, ±0.2 nH
Murata LQG15HN series (0402 size)
Murata LQW15AN series (0402 size)
R1
100 Ω, ±5%
U1
GSM/GPRS Transceiver
Silicon Laboratories Si4205
Z1
GSM 850 RX SAW Filter
(150 Ω balanced output)
Epcos B39881-B9001-C710 (5-pin, 1.4 x 2.0 mm)
Epcos B39881-B9004-E710 (6-pin, 1.6 x 2.0 mm)
Murata SAFEK881MFL0T00R00 (6-pin, 1.6 x 2.0 mm)
E-GSM 900 RX SAW Filter
(150 Ω balanced output)
Epcos B39941-B7820-C710 (5-pin, 1.4 x 2.0 mm)
Epcos B39941-B9017-K310 (6-pin, 1.6 x 2.0 mm)
Murata SAFEK942MFM0T00R00 (6-pin, 1.6 x 2.0 mm)
Z2
DCS 1800 RX SAW Filter
(150 Ω balanced output)
Epcos B39182-B7821-C710 (5-pin, 1.4 x 2.0 mm)
Epcos B39182-B9013-K310 (6-pin, 1.6 x 2.0 mm)
Murata SAFEK1G84FA0T00R00 (6-pin, 1.6 x 2.0 mm)
Z3
PCS 1900 RX SAW Filter
(150 Ω balanced output)
Epcos B39202-B7825-C710 (5-pin, 1.4 x 2.0 mm)
Epcos B39202-B9020-K310 (6-pin, 1.6 x 2.0 mm)
Murata SAFEK1G96FA0T00R00 (6-pin, 1.6 x 2.0 mm)
Rev. 1.0
15
Aero I
Functional Description
PGA
ADC
PGA
ADC
LNA
PCS
LNA
0 / 90
GSM
DCS
PCS
PGA
DAC
I
PGA
DAC
Q
XOUT
100 kHz
I
DET
PA
I
PA
BASEBAND
DCS
ANTENNA SWITCH
Si4205
LNA
CHANNEL
FILTER
GSM
Q
RF
PLL
IF
PLL
VC-TCXO
13 or 26 MHz
XIN
AFC
Figure 8. Aero I Transceiver Block Diagram
The Aero I transceiver is the industry’s most integrated
RF front end for multi-band GSM/GPRS digital cellular
handsets and wireless data modems. The highly
integrated solution eliminates the IF SAW filter, external
low noise amplifiers (LNAs) for three bands, transmit
and RF voltage controlled oscillator (VCO) modules,
and more than 70 other discrete components found in
conventional designs.
compatible with any supplier’s baseband subsystem.
The high level of integration obtained through highperformance packaging and fine line CMOS process
technology results in a solution with 50% less area and
80% fewer components than competing solutions. A
triple-band GSM transceiver using the Aero I
transceiver can be implemented with 15 components in
less than 1.2 cm2 of board area. This level of integration
is an enabling force in lowering the cost, simplifying the
design and manufacturing, and shrinking the form factor
in next-generation GSM/GPRS voice and data
terminals.
The unique integer-N PLL architecture produces a
transient response that is superior in speed to
fractional-N architectures without suffering the high
phase noise or spurious modulation effects often
associated with those designs. This fast transient
response makes the Aero I transceiver well suited to
GPRS multi-slot applications where channel switching
and settling times are critical.
The receive section uses a digital low-IF architecture
that avoids the difficulties associated with direct
conversion while delivering lower solution cost and
reduced complexity. The baseband interface is
16
The transmit section is a complete up-conversion path
from the baseband subsystem to the power amplifier,
and uses an offset phase-locked loop (PLL) with a fully
integrated transmit VCO. The frequency synthesizer
uses Silicon Laboratories’ proven technology, which
includes integrated RF and IF VCOs, varactors, and
loop filters.
While conventional solutions use BiCMOS or other
bipolar process technologies, the Aero I transceiver
employs 100% CMOS process. This brings the dramatic
cost savings and extensive manufacturing capacity of
CMOS to the GSM market.
Rev. 1.0
Aero I
Receiver
LNA
DCS
LNA
PCS
LNA
RXBAND[1:0] 0/90
LNAC[1:0]
LNAG[1:0]
RF
PLL
PGA
ADC
PGA
ADC
AGAIN[2:0]
100 kHz CSEL
PGA
DAC
I
PGA
DAC
Q
BASEBAND
GSM
CHANNEL
FILTER
Si4205
DGAIN[5:0]
DACCM[1:0]
DACFS[1:0]
ZERODEL[2:0]
NRF1[15:0]
RFUP
Figure 9. Receiver Block Diagram
The Aero I transceiver uses a low-IF receiver
architecture which allows for the on-chip integration of
the channel selection filters, eliminating the external RF
image reject filters and the IF SAW filter required in
conventional superheterodyne architectures. Compared
to a direct-conversion architecture, the low-IF
architecture has a much greater degree of immunity to
dc offsets, which can arise from RF local oscillator
(RFLO) self-mixing, 2nd-order distortion of blockers,
and device 1/f noise. This relaxes the common-mode
balance requirements on the input SAW filters, and
simplifies PC board design and manufacturing.
Three differential-input LNAs are integrated. The GSM
input supports the GSM 850 (869–894 MHz) or EGSM 900 (925–960 MHz) bands. The DCS input
supports the DCS 1800 (1805–1880 MHz) band. The
PCS input supports the PCS 1900 (1930–1990 MHz)
band. For quad-band designs, SAW filters for the
GSM 850 and E-GSM 900 bands should be connected
to a balanced combiner which drives the GSM input for
both bands.
The LNA inputs are matched to the 150 Ω balancedoutput SAW filters through external LC matching
networks. The LNA gain is controlled with the
LNAG[1:0] and LNAC[1:0] bits in register 05h.
A quadrature image-reject mixer downconverts the RF
signal to a 100 kHz intermediate frequency (IF) with the
RFLO from the frequency synthesizer. The RFLO
frequency is between 1737.8 to 1989.9 MHz, and is
internally divided by 2 for GSM 850 and E-GSM 900
modes. The mixer output is amplified with an analog
programmable gain amplifier (PGA), which is controlled
with the AGAIN[2:0] bits in register 05h. The quadrature
IF signal is digitized with high resolution A/D converters
(ADCs).
The ADC output is downconverted to baseband with a
digital 100 kHz quadrature LO signal. Digital decimation
and IIR filters perform channel selection to remove
blocking and reference interference signals. The
response of the IIR filter is programmable to a high
selectivity setting (CSEL = 0) or a low selectivity setting
(CSEL = 1). The low selectivity filter has a flatter group
delay response which may be desirable where the final
channelization filter is in the baseband chip. After
channel selection, the digital output is scaled with a
digital PGA, which is controlled with the DGAIN[5:0] bits
in register 05h.
The LNAG[1:0], LNAC[1:0], AGAIN[2:0] and DGAIN[5:0]
bits must be set to provide a constant amplitude signal
to the baseband receive inputs. See “AN51: Aero
Transceiver AGC Strategy” for more details.
DACs drive a differential analog signal onto the RXIP,
RXIN, RXQP, and RXQN pins to interface to standard
analog-input baseband ICs. No special processing is
required in the baseband for offset compensation or
extended dynamic range. The receive and transmit
baseband I/Q pins can be multiplexed together into a 4wire interface. The common mode level at the receive I
and Q outputs is programmable with the DACCM[1:0]
bits, and the full scale level is programmable with the
DACFS[1:0] bits in register 12h.
Rev. 1.0
17
Aero I
Transmitter
NIF[15:0]
PDIB
RF
PLL
IF
PLL
y2
REG
GSM
DCS/PCS
PA
PA
FIF[3:0]
RFOG
BBG[1:0]
SWAP
TXIP
I
REG
RFOD
Si4205
TXIN
I
DET
y1, 2
TXQP
BASEBAND
NRF2[15:0]
PDRB
Q
TXBAND[1:0]
TXQN
Figure 10. Transmitter Block Diagram
The transmit (TX) section consists of an I/Q baseband
upconverter, an offset phase-locked loop (OPLL) and
two output buffers that can drive external power
amplifiers (PA), one for the GSM 850 (824 to 849 MHz)
and E-GSM 900 (880 to 915 MHz) bands and one for
the DCS 1800 (1710 to 1785 MHz) and PCS 1900
(1850 to 1910 MHz) bands. The OPLL requires no
external duplexer to attenuate transmitter noise or
spurious signals in the receive band, saving both cost
and power. Additionally, the output of the transmit VCO
(TXVCO) is a constant-envelope signal that reduces the
problem of spectral spreading caused by non-linearity in
the PA.
low-side injection is used for the DCS 1800 and
PCS 1900 bands. The I and Q signals are automatically
swapped when switching bands. Therefore, there is no
need for the customer to externally swap the I and Q
signals. However, for additional layout flexibility, the
SWAP bit in register 03h can be used to manually
exchange the I and Q signals.
Low-pass filters before the OPLL phase detector reduce
the harmonic content of the quadrature modulator and
feedback mixer outputs. The cutoff frequency of the
filters is programmable with the FIF[3:0] bits in register
04h, and should be set to the recommended settings
detailed in the register description.
A quadrature mixer upconverts the differential in-phase
(TXIP, TXIN) and quadrature (TXQP, TXQN) signals
with the IFLO to generate a SSB IF signal that is filtered
and used as the reference input to the OPLL. The IFLO
frequency is generated between 766 and 896 MHz and
internally divided by 2 to generate the quadrature LO
signals for the quadrature modulator, resulting in an IF
between 383 and 448 MHz. For the E-GSM 900 band,
two different IFLO frequencies are required for spur
management. Therefore, the IF PLL must be
programmed per channel in the E-GSM 900 band. The
IFLO frequencies are defined in Table 7 on page 13.
The OPLL consists of a feedback mixer, a phase
detector, a loop filter, and a fully integrated TXVCO. The
TXVCO is centered between the DCS 1800 and
PCS 1900 bands, and its output is divided by 2 for the
GSM 850 and E-GSM 900 bands. The RFLO frequency
is generated between 1272 and 1483 MHz. To allow a
single VCO to be used for the RFLO, high-side injection
is used for the GSM 850 and E-GSM 900 bands, and
18
Rev. 1.0
Aero I
Frequency Synthesizer
Si4205
XIN
y1, 2
y65,
y130
XOUT
DIV2
RFUP
XEN
PDN
Power
Control
SCLK
Serial
I/O
RF2
Self
Tune
RF PLL
PDIB
PDRB
SDI
SDO
RF1
I
DET
IF PLL
Self
Tune
SDOSEL[4:0]
SEN
To
RX/TX
NRF1[15:0]
NRF2[15:0]
yN
yN
NIF[15:0]
I
DET
To TX
Figure 11. Frequency Synthesizer Block Diagram
The Aero I transceiver integrates two complete PLLs
including VCOs, varactors, resonators, loop filters,
reference and VCO dividers, and phase detectors. The
RF PLL uses two multiplexed VCOs. The RF1 VCO is
used for receive mode, and the RF2 VCO is used for
transmit mode. The IF PLL is used only during transmit
mode. All VCO tuning inductors are also integrated.
The IF and RF output frequencies are set by
programming the N-Divider registers, NRF1, NRF2 and
NIF. Programming the N-Divider register for either RF1
or RF2 automatically selects the proper VCO. The
output frequency of each PLL is as follows:
f OUT = N × f φ
The DIV2 bit in register 31h controls a programmable
divider at the XIN pin to allow either a 13 or 26 MHz
reference frequency. For receive mode, the RF1 PLL
phase detector update rate (fφ) should be programmed
fφ = 100 kHz for DCS 1800 or PCS 1900 bands, and
fφ = 200 kHz for GSM 850 and E-GSM 900 bands. For
transmit mode, the RF2 and IF PLL phase detector
update rates are always fφ =200 kHz.
Rev. 1.0
19
Aero I
Serial Interface
XOUT Buffer
A three-wire serial interface is provided to allow an
external system controller to write the control registers
for dividers, receive path gain, powerdown settings, and
other controls. The serial control word is 24 bits in
length, comprised of an 18-bit data field and a 6-bit
address field as shown in Figure 12.
The Aero I transceiver contains a reference clock buffer
to drive the baseband input. The clock signal from the
VC-TCXO is capacitively coupled to the XIN pin. The
clock signal is not divided with the XSEL control.
Last bit
clocked in
D D D D D D D D D D D D D D D D D D A A A A A A
17 16 15 14 13 12 11 10 9 8 7 6 5 4 3 2 1 0 5 4 3 2 1 0
Data Field
Address
Field
Figure 12. Serial Interface Format
The XOUT buffer is a CMOS driver stage with
approximately 250 Ω of series resistance. This buffer is
enabled when the XEN hardware control (pin 26 on the
Si4205) is set high, independent of the PDN control pin.
To achieve complete powerdown during sleep, the XEN
pin must be set low, the XBUF bit in Register 12 must
be set to zero, and the XPD1 bit in Register 11 must be
set to one. During normal operation, these bits should
be set to their default values.
All registers must be written when the PDN pin is
asserted (low), except for register 22h. All serial
interface pins should be held at a constant level during
receive and transmit bursts to minimize spurious
emissions. This includes stopping the SCLK clock. A
timing diagram for the serial interface is shown in
Figure 3 on page 7.
When the serial interface is enabled (i.e., when SEN is
low), data and address bits on the SDI pin are clocked
into an internal shift register on the rising edge of SCLK.
Data in the shift register is then transferred on the rising
edge of SEN into the internal data register addressed in
the address field. The internal shift register ignores any
leading bits before the 24 required bits. The serial
interface is disabled when SEN is high.
Optionally, registers can be read as illustrated in
Figure 4 on page 7. The serial output data appears on
the SDO pin after writing the revision register with the
address to be read. Writing to any of the registers
causes the function of SDO to revert to its previously
programmed function.
20
Rev. 1.0
Aero I
Control Registers
Table 8. Register Summary
Master Registers
Bit
Reg
Name
01h
Reset
0
0
0
0
0
0
0
02h
Mode
0
0
0
0
0
0
03h
Config
0
0
0
0
DIAG[1:0]
04h
Transmit
0
0
0
0
0
05h
Receive
0
0
0
0
11h
Config
0
0
0
0
12h
DAC Config
0
0
0
0
0
0
19h
Reserved
0
0
0
0
0
0
20h
RX Master #1
21h
RX Master #2
0
22h
RX Master #3
0
23h
TX Master #1
24h
TX Master #2
31h
Config
0
0
0
32h
Powerdown
0
0
0
33h
RF1 N Divider
0
0
NRF1[15:0]
34h
RF2 N Divider
0
0
NRF2[15:0]
35h
IF N Divider
0
0
NIF[15:0]
3Ah
Reserved
0
0
0
0
0
0
0
0
0
0
3Eh
Reserved
0
0
0
0
0
0
0
0
0
3Fh
Reserved
0
0
0
0
0
0
0
0
0
D17 D16 D15 D14 D13 D12 D11 D10
D9
D8
D7
D6
D5
D4
D3
D2
D1
D0
0
0
0
0
0
0
0
0
0
0
RESET
0
0
0
0
0
0
0
0
0
AUTO
SWAP
0
0
0
0
0
1
0
0
1
BBG[1:0]
0
0
0
0
0
DPDS[2:0]
RXBAND[1:0]
FIF[3:0]
DGAIN[5:0]
0
XPD1
1
XSEL
0
0
1
XBUF
0
ZDBS
0
0
0
0
0
RXBAND[1:0]
AGAIN[2:0]
1
0
1
ZERODEL[2:0]
0
0
LNAC[1:0]
LNAG[1:0]
0
0
0
DACCM[1:0]
0
0
0
CSEL
DACFS[1:0]
0
0
NRF1[15:0]
DPDS[2:0]
0
TXBAND[1:0]
MODE[1:0]
0
0
LNAC[1:0]
LNAG[1:0]
0
0
0
0
AGAIN[2:0]
0
TXBAND[1:0]
0
0
0
DGAIN[5:0]
0
DGAIN[5:0]
NRF2[15:0]
FIF[3:0]
NIF[13:0]
SDOSEL[3:0]
0
0
0
0
0
0
0
0
0
0
RFUP
DIV2
0
0
1
0
0
0
0
0
0
0
0
0
PDIB
PDRB
0
0
0
0
1
0
0
1
0
0
0
0
0
1
1
1
1
0
0
0
0
1
0
0
0
0
Notes:
1. Any register not listed here is reserved and should not be written. Writing to reserved registers may result in
unpredictable behavior.
2. Master registers 20h to 24h simplify programming the Aero I to support initiation of receive (RX) and transmit (TX)
operations with only two register writes.
3. See “AN50: Aero Transceiver Programming Guide” for detailed instructions on register programming.
Rev. 1.0
21
Aero I
Register 01h. Reset
Bit
D17 D16 D15 D14 D13 D12 D11 D10
Name
0
0
0
0
Bit
Name
17:1
Reserved
0
RESET
0
0
0
0
D9
D8
D7
D6
D5
D4
D3
D2
D1
D0
0
0
0
0
0
0
0
0
0
RESET
Function
Program to zero.
Chip Reset.
0 = Normal operation (default).
1 = Reset all registers to default values.
Note: See “Control Registers” on page 21 for more details. This register must be
written to 0 twice after a reset operation. This bit does not reset registers
31h to 35h.
Register 02h. Mode Control
Bit
D17 D16 D15 D14 D13 D12 D11 D10
Name
0
0
0
0
Bit
Name
17:3
Reserved
2
AUTO
1:0
MODE[1:0]
0
0
0
D9
D8
D7
D6
D5
D4
D3
D2
0
0
0
0
0
0
0
AUTO
0
D0
MODE[1:0]
Function
Program to zero.
Automatic Mode Select.
0 = Manual. Mode is controlled by MODE[1:0] bits (default).
1 = Automatic. Last register write to NRF1 implies RX mode; Last register
write to NRF2 implies TX mode. MODE[1:0] bits are ignored.
Transmit/Receive/Cal Mode Select.
00 = Receive mode (default).
01 = Transmit mode.
10 = Calibration mode.
11 = Reserved.
Note: These bits are valid only when AUTO = 0.
Note: Calibration must be performed each time the power supply is applied. To initiate the calibration mode, set
MODE[1:0] = 10 and pulse the PDN pin high for at least 150 µs.
22
D1
Rev. 1.0
Aero I
Register 03h. Configuration
Bit
D17 D16 D15 D14 D13 D12 D11 D10
Name
0
0
0
0
DIAG[1:0]
SWAP
D9
D8
0
0
0
D7
D6
TXBAND[1:0]
D5
D4
RXBAND[1:0]
Bit
Name
17:14
Reserved
Program to zero.
13:12
DIAG[1:0]
DIAG1/DIAG2 Output Select.
DIAG1
DIAG2
00 =
LOW
LOW (default)
01 =
LOW
HIGH
10 =
HIGH
LOW
11 =
HIGH
HIGH
D3
D2
D1
D0
0
0
1
0
Function
Note: These pins can be used to control antenna switch functions. These bits
must be programmed with the PDN pin is zero. The DIAG1/DIAG2 pins
are held at the desired value regardless of the state of the PDN pin.
11
SWAP
Transmit I/Q Swap.
0 = Normal (default).
1 = Swap I and Q for TXIP, TXIN, TXQP and TXQN pins.
10:8
Reserved
7:6
TXBAND[1:0]
Transmit Band Select.
00 = GSM 850 or E-GSM 900 (default).
01 = DCS 1800.
10 = PCS 1900.
11 = Reserved.
5:4
RXBAND[1:0]
Receive Band Select.
00 = GSM input (default).
01 = DCS input.
10 = PCS input.
11 = Reserved.
3:2
Reserved
Program to zero.
1
Reserved
Program to one.
0
Reserved
Program to zero.
Program to zero.
Rev. 1.0
23
Aero I
Register 04h. Transmit Control
Bit
D17 D16 D15 D14 D13 D12 D11 D10
Name
0
0
0
0
0
0
0
D9
1
D8
BBG[1:0]
D7
D6
D5
FIF[3:0]
D4
D3
D2
D1
D0
0
0
0
0
Bit
Name
Function
17:11
Reserved
Program to zero.
10
Reserved
Program to one.
9:8
BBG[1:0]
TX Baseband Input Full Scale Differential Input Voltage.
10 = Reserved.
11 = 2.0 VPPD.
00 = 1.6 VPPD (default).
01 = 1.2 VPPD.
Note: Refer to Table 6 for minimum and maximum values. Set this register to the
nearest value.
7:4
FIF[3:0]
TX IF Filter Cutoff Frequency.
0111 = Use for GSM 850, E-GSM 900 and PCS 1900 bands.
0110 = Use for DCS 1800 band.
Note: Use the recommended setting for each band. Other settings reserved.
3:0
24
Reserved
Program to zero.
Rev. 1.0
Aero I
Register 05h. Receive Gain
Bit
D17 D16 D15 D14 D13 D12 D11 D10
Name
0
0
0
0
Bit
Name
17:14
Reserved
13:8
DGAIN[5:0]
D9
D8
D7
DGAIN[5:0]
0
D6
D5
AGAIN[2:0]
D4
D3
D2
LNAC[1:0]
D1
D0
LNAG[1:0]
Function
Program to zero.
Digital PGA Gain Control.
00h = 0 dB (default).
01h = 1 dB.
...
3Fh = 63 dB.
Note: See “AN51: Aero Transceiver AGC Strategy” for details on setting the gain
registers.
7
Reserved
6:4
AGAIN[2:0]
Program to zero.
Analog PGA Gain Control.
000 = 0 dB (default).
001 = 4 dB.
010 = 8 dB.
011 = 12 dB.
100 = 16 dB.
101 = Reserved.
110 = Reserved.
111 = Reserved.
Note: See “AN51: Aero Transceiver AGC Strategy” for details on setting the gain
registers.
3:2
LNAC[1:0]
LNA Bias Current Control.
00 = Minimum current (default).
01 = Maximum current.
10 = Reserved.
11 = Reserved.
Note: Program these bits to the same value as LNAG[1:0].
1:0
LNAG[1:0]
LNA Gain Control.
00 = Minimum gain (default).
01 = Maximum gain.
10 = Reserved.
11 = Reserved.
Notes:
1. Program these bits to the same value as LNAC[1:0].
2. See “AN51: Aero Transceiver AGC Strategy” for details on setting the gain
registers.
Rev. 1.0
25
Aero I
Register 11h. Configuration
Bit
D17 D16 D15 D14 D13 D12 D11 D10
Name
0
0
0
0
DPDS[2:0]
D9
D8
D7
D6
D5
D4
D3
D2
D1
D0
1
XSEL
0
1
0
1
0
0
0
CSEL
XPD1
Bit
Name
Function
17:14
Reserved
Program to zero.
13:11
DPDS[2:0]
Data Path Delayed Start.
111= Use for GSM 850 and GSM 900 bands.
011= Use for DCS 1800 and PCS 1900 bands (default).
Note: Use the recommended setting for each band. Other settings reserved.
10
XPD1
Reference Buffer Powerdown.
0 = Reference buffer automatically enabled (default).
1 = Reference buffer disabled.
Note: This bit should be set to 0 during normal operation. To achieve lowest
powerdown current (IPDN), this bit should be set to 1. The XBUF bit in
Register 12h must also be set appropriately.
9
Reserved
8
XSEL
Program to one.
Reference Frequency Select.
0 = No divider. XIN = 13 MHz (default).
1 = Divide XIN by 2. XIN = 26 MHz.
Note: The internal clock should always be 13 MHz.
26
7
Reserved
Program to zero.
6
Reserved
Program to one.
5
Reserved
Program to zero.
4
Reserved
Program to one.
3:1
Reserved
Program to zero.
0
CSEL
Digital IIR Coefficient Select.
0 = High selectivity filter (default).
1 = Low selectivity filter.
Rev. 1.0
Aero I
Register 12h. DAC Configuration
Bit
D17 D16 D15 D14 D13 D12 D11 D10
Name
0
0
0
0
0
0
0
1
D9
D8
D7
XBUF
0
ZDBS
Bit
Name
17:11
Reserved
Program to zero.
10
Reserved
Program to one.
9
XBUF
D6
D5
D4
ZERODEL[2:0]
D3
D2
DACCM[1:0]
D1
D0
DACFS[1:0]
Function
Reference Buffer Power Control.
0 = Reference buffer disabled.
1 = Reference buffer automatically enabled (default).
Note: This bit should be set to 1 during normal operation. To achieve the lowest
powerdown current (IPDN), this bit should be set to 0. The XPD1 bit in
Register 11h must also be set appropriately.
8
Reserved
7
ZDBS
6:4
ZERODEL[2:0]
Program to zero.
ZERODEL Band Select.
0 = Use ZERODEL[2:0] settings corresponding to DCS/PCS column
(default).
1 = Use RXBAND[1:0] to determine ZERODEL[2:0] delay setting (GSM
or DCS/PCS).
RX Output Zero Delay.
Code
GSM
000:
90 µs
001:
110 µs
010:
130 µs
011:
140 µs
100:
150 µs
101:
160 µs
110:
180 µs
111:
Reserved
DCS/PCS
130 µs
150 µs
170 µs
180 µs
190 µs
200 µs
220 µs
(default)
Note: DAC input is forced to zero after PDN is deasserted. This feature can be
used by the baseband processor to cancel the Si4205 DAC dc offset.
Offsets induced on channels due to 13 MHz harmonics will not be
included in the calibrated value.
3:2
DACCM[1:0]
RX Output Common Mode Voltage.
00 = 1.0 V.
01 = 1.25 V (default).
10 = 1.35 V.
11 = Reserved.
1:0
DACFS[1:0]
RX Output Differential Full Scale Voltage.
00 = 1.0 VPPD
01 = 2.0 VPPD (default).
10 = 3.5 VPPD
11 = Reserved.
Rev. 1.0
27
Aero I
Register 19h. Reserved
Bit
Name
D17 D16 D15 D14 D13 D12 D11 D10
0
0
0
0
Bit
Name
17:0
Reserved
0
0
0
D9
D8
D7
D6
D5
D4
D3
D2
D1
D0
0
0
0
0
0
0
0
0
0
0
D4
D3
D2
D1
D0
0
Function
Program to zero.
Register 20h. RX Master #1
Bit
D17 D16 D15 D14 D13 D12 D11 D10
D9
D8
Name RXBAND[1:0]
D7
D6
D5
NRF1[15:0]
Notes:
1. See registers 03h and 33h for bit definitions.
2. When this register is written, the PDIB bit will be automatically set to 0, the PDRB bit will be set to 1 and the RFUP bit is
set as a function of RXBAND[1:0].
Register 21h. RX Master #2
Bit
Name
D17 D16 D15 D14 D13 D12 D11 D10
0
LNAC[1:0]
DPDS[2:0]
D9
LNAG[1:0]
D8
D7
AGAIN[2:0]
D6
D5
D4
0
D3
D2
D1
D0
D1
D0
DGAIN[5:0]
Note: See registers 05h and 11h for bit definitions.
Register 22h. RX Master #3
Bit
Name
D17 D16 D15 D14 D13 D12 D11 D10
0
0
0
0
0
0
0
0
D9
D8
D7
D6
0
0
0
0
Notes:
1. See register 05h for bit definitions.
2. The DGAIN[5:0] in register 22h can be changed without powering down.
28
Rev. 1.0
D5
D4
D3
D2
DGAIN[5:0]
Aero I
Register 23h. TX Master #1
Bit
D17 D16 D15 D14 D13 D12 D11 D10
D9
Name TXBAND[1:0]
D8
D7
D6
D5
D4
D3
D2
D1
D0
D3
D2
D1
D0
NRF2[15:0]
Notes:
1. See registers 03h and 34h for bit definitions.
2. When this register is written, the PDIB bit is automatically set to 1, and the PDRB bit is set to 1.
Register 24h. TX Master #2
Bit
Name
D17 D16 D15 D14 D13 D12 D11 D10
D9
D8
D7
D6
D5
D4
NIF[13:0]
FIF[3:0]
Note: See registers 04h and 35h for bit definitions.
Rev. 1.0
29
Aero I
Register 31h. Main Configuration
Bit
Name
D17 D16 D15 D14 D13 D12 D11 D10
0
0
0
Bit
Name
17:15
Reserved
14:11
SDOSEL[3:0]
SDOSEL[3:0]
D9
D8
D7
D6
D5
D4
D3
D2
D1
D0
0
0
0
0
0
RFUP
DIV2
0
0
1
0
Function
Program to zero.
SDO Output Control Register.
The mux_output table is as follows:
0000 Connected to the Output Shift Register (default).
0001 Force the Output to Low.
0010 Reference Clock.
0011 Lock Detect (LDETB) Signal from Phase Detectors.
1111 High Impedance.
Notes:
1. SDO is high-impedance when PDN = 0.
2. SDO is Serial Data Output when in register read mode.
10:5
Reserved
4
RFUP
Program to zero.
RF PLL Update Rate (RF1 VCO only).
0 = 200 kHz update rate (Receive GSM modes).
1 = 100 kHz update rate (Receive DCS and PCS modes).
Note: This bit is set to 1 when register 20h D[17:16] = 01b or 10b (DCS 1800 or
PCS 1900 receive modes) and is set to 0 when D[17:16] = 00b or 11b
(GSM 850 or GSM 900 modes).
30
3
DIV2
Input Clock Frequency.
0 = No divider. XIN = 13 MHz.
1 = Divide XIN by 2. XIN = 26 MHz.
2:1
Reserved
Program to zero.
0
Reserved
Program to one.
Rev. 1.0
Aero I
Register 32h. Powerdown
Bit
D17 D16 D15 D14 D13 D12 D11 D10
Name
0
0
0
0
Bit
Name
17:2
Reserved
1
PDIB
0
0
0
D9
D8
D7
D6
D5
D4
D3
D2
D1
D0
0
0
0
0
0
0
0
0
PDIB
PDRB
0
Function
Program to zero.
Powerdown IF PLL.
0 = IF synthesizer powered down.
1 = IF synthesizer powered up when the PDN pin is high.
Notes:
1. The IF PLL is only used in transmit mode. Powerdown for receive mode.
2. This bit is set to 0 when register 20h is written (receive mode).
3. This bit is set to 1 when register 23h is written (transmit mode).
0
PDRB
Powerdown RF PLL.
0 = RF synthesizer powered down.
1 = RF synthesizer powered up when the PDN pin is high.
Notes:
1. This bit is set to 1 when register 20h is written (receive mode).
2. This bit is set to 1 when register 23h is written (transmit mode).
Register 33h. RF1 N Divider
Bit
Name
D17 D16 D15 D14 D13 D12 D11 D10
0
D9
D8
D7
D6
D5
D4
D3
D2
D1
D0
D5
D4
D3
D2
D1
D0
NRF1[15:0]
0
Bit
Name
17:16
Reserved
Program to zero.
Function
15:0
NRF1[15:0]
N Divider for RF PLL (RF1 VCO).
Used for receive mode.
Register 34h. RF2 N Divider
Bit
Name
D17 D16 D15 D14 D13 D12 D11 D10
0
D9
D8
D7
D6
NRF2[15:0]
0
Bit
Name
Function
17:16
Reserved
Program to zero.
15:0
NRF2[15:0]
N Divider for RF PLL (RF2 VCO).
Used for transmit mode.
Rev. 1.0
31
Aero I
Register 35h. IF N Divider
Bit
Name
D17 D16 D15 D14 D13 D12 D11 D10
0
D9
D8
D7
D6
D5
D4
D3
D2
D1
D0
NIF[15:0]
0
Bit
Name
Function
17:16
Reserved
Program to zero.
15:0
NIF[15:0]
N Divider for IF Synthesizer.
Used for transmit mode.
Register 3Ah. Reserved
Bit
Name
D17 D16 D15 D14 D13 D12 D11 D10
0
0
0
0
0
0
Bit
17:4
Name
Reserved
Program to zero.
3
Reserved
Program to one.
2:1
Reserved
Program to zero.
0
Reserved
Program to one.
0
0
D9
D8
D7
D6
D5
D4
D3
D2
D1
D0
0
0
0
0
0
0
1
0
0
1
Function
Register 3Eh. Reserved
Bit
Name
D17 D16 D15 D14 D13 D12 D11 D10
0
0
0
0
0
0
Bit
17:4
Name
Reserved
Program to zero.
3:0
Reserved
Program to one.
0
0
D9
D8
D7
D6
D5
D4
D3
D2
D1
D0
0
0
0
0
0
0
1
1
1
1
Function
Register 3Fh. Reserved
Bit
Name
32
D17 D16 D15 D14 D13 D12 D11 D10
0
0
0
0
0
0
Bit
17:5
Name
Reserved
Program to zero.
4
Reserved
Program to one.
3:0
Reserved
Program to zero.
0
0
D9
D8
D7
D6
D5
D4
D3
D2
D1
D0
0
0
0
0
0
1
0
0
0
0
Function
Rev. 1.0
Aero I
RXQN
1
RXIP
2
XO U T
XE N
DI A G 2
DI A G 1
R F OG
RFOD
32
R XQ P
Pin Descriptions: Si4205-BM
28
27
26
25
24
23
22
GND
GND
31
21
RFIGN
20
RFIGP
RFIDN
RXIN
3
19
TXIP
4
18
RFIDP
17
RFIPN
16
RFIPP
15
GND
9
10
11
12
13
14
SDI
8
SEN
29
SC L K
7
GND
SD O
TXQN
GND
PD N
6
XI N
5
VD D
TXIN
TXQP
30
Pin Number(s)
Name
Description
1, 28
RXQN, RXQP
Receive Q output (differential).
2, 3
RXIP, RXIN
Receive I output (differential).
4, 5
TXIP, TXIN
Transmit I input (differential).
6, 7
TXQP, TXQN
Transmit Q input (differential).
8
XIN
Reference frequency input from crystal oscillator.
9, 32
VDD
Supply voltage.
10
PDN
Powerdown input (active low).
11
SDO
Serial data output.
12
SEN
Serial enable input (active low).
13
SCLK
Serial clock input.
14
SDI
Serial data input.
15, 29–31
GND
Ground. Connect to ground plane on PCB.
16, 17
RFIPP, RFIPN
PCS LNA input (differential).
Use for PCS 1900 band.
18, 19
RFIDP, RFIDN
DCS LNA input (differential).
Use for DCS 1800 band.
20, 21
RFIGP, RFIGN
GSM LNA input (differential).
Used for GSM 850 or E-GSM 900 bands.
22
RFOD
DCS and PCS transmit output to power amplifier.
Used for DCS 1800 and PCS 1900 bands.
23
RFOG
GSM transmit output to power amplifier.
Used for GSM 850 and E-GSM 900 bands.
24, 25
DIAG1, DIAG2
Diagnostic output.
Can be used as digital outputs to control antenna switch functions.
26
XEN
XOUT pin enable.
27
XOUT
Clock output to baseband.
Rev. 1.0
33
Aero I
Ordering Guide
Part Number
Si4205-BM
Description
Operating
Temperature
Tri-band Transceiver
GSM 850 or E-GSM 900, DCS 1800, PCS 1900
–20 to 85 °C
Note: Add an “R” at the end of the part number to denote tape and reel option; 2500 quantity per
reel.
34
Rev. 1.0
Aero I
Package Outline: Si4205-BM
Figure 13. 32-Pin Land Grid Array (LGA)
Notes:
1. Dimensions in mm.
2. Approximate device weight is 196 mg.
Rev. 1.0
35
Aero I
Document Change List
Revision 0.9 to Revision 1.0
„
„
This document corresponds to Aero I (Si4205),
revision F.
Table 3 on page 5 updated.
z
„
Table 4 on page 6 updated.
z
z
„
„
z
„
„
Added Note 1.
Clarified register writes for DGAIN bits.
Figure 3 on page 7 updated.
z Added SEN programming option.
Table 5 on page 8 updated.
z
„
Updated Supply Current specification for powerdown
mode.
Updated 20 MHz GSM band desensitization
specification.
Updated Voltage Gain specification.
"Bill of Materials‚" on page 15 updated.
"Ordering Guide‚" on page 34 updated.
"Package Outline: Si4205-BM‚" on page 35
updated.
z
Added Note 1.
Rev. 1.0
36
Aero I
Notes:
Rev. 1.0
37
Aero I
Contact Information
Silicon Laboratories Inc.
4635 Boston Lane
Austin, Texas 78735
Tel:1+ (512) 416-8500
Fax:1+ (512) 416-9669
Toll Free:1+ (877) 444-3032
Email: [email protected]
Internet: www.silabs.com
The information in this document is believed to be accurate in all respects at the time of publication but is subject to change without notice.
Silicon Laboratories assumes no responsibility for errors and omissions, and disclaims responsibility for any consequences resulting from
the use of information included herein. Additionally, Silicon Laboratories assumes no responsibility for the functioning of undescribed features or parameters. Silicon Laboratories reserves the right to make changes without further notice. Silicon Laboratories makes no warranty, representation or guarantee regarding the suitability of its products for any particular purpose, nor does Silicon Laboratories assume
any liability arising out of the application or use of any product or circuit, and specifically disclaims any and all liability, including without
limitation consequential or incidental damages. Silicon Laboratories products are not designed, intended, or authorized for use in applications intended to support or sustain life, or for any other application in which the failure of the Silicon Laboratories product could create a
situation where personal injury or death may occur. Should Buyer purchase or use Silicon Laboratories products for any such unintended
or unauthorized application, Buyer shall indemnify and hold Silicon Laboratories harmless against all claims and damages.
Silicon Laboratories, Silicon Labs, and Aero are trademarks of Silicon Laboratories Inc.
Other products or brand names mentioned herein are trademarks or registered trademarks of their respective holder.
38
Rev. 1.0
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