ADAS3022SCPZ-EP [ADI]

16-Bit, 1 MSPS, 8 Channel Data Acquisition System;
ADAS3022SCPZ-EP
型号: ADAS3022SCPZ-EP
厂家: ADI    ADI
描述:

16-Bit, 1 MSPS, 8 Channel Data Acquisition System

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16-Bit, 1 MSPS, 8-Channel  
Data Acquisition System  
ADAS3022  
Data Sheet  
and buffer; and a 16-bit charge redistribution analog-to-digital  
converter (ADC) with successive approximation register (SAR)  
architecture. The ADAS3022 can resolve eight single-ended  
inputs or four fully differential inputs up to ±24.576 V when  
using 15 V supplies. In addition, the device can accept the  
commonly used bipolar differential, bipolar single-ended,  
pseudo bipolar, or pseudo unipolar input signals, as shown in  
Table 1, thus enabling the use of almost any direct sensor  
interface.  
FEATURES  
Ease of use—16-bit, 1 MSPS complete data acquisition system  
High impedance, 8-channel input: >500 MΩ  
Differential input voltage range: 24.576 V maximum  
High input common-mode rejection: >100 dB  
User-programmable input ranges  
Channel sequencer with individual channel gains  
On-chip 4.096 V reference and buffer  
Auxiliary input—direct interface to PulSAR ADC inputs  
No latency or pipeline delay (SAR architecture)  
Serial 4-wire, 1.8 V to 5 V SPI-/SPORT-compatible interface  
LFCSP package (6 mm × 6 mm)  
The ADAS3022 simplifies design challenges by eliminating  
signal buffering, level shifting, amplification/attenuation,  
common-mode rejection, settling time, and any other analog  
signal conditioning challenge while allowing a smaller form  
factor, faster time to market, and lower cost.  
−40°C to +85°C industrial temperature range  
APPLICATIONS  
Multichannel data acquisition and system monitoring  
Process control  
Power line monitoring  
Table 1. Typical Input Range Selection  
Signal  
Input Range, VIN (V)  
Differential  
1 V  
Automated test equipment  
Instrumentation  
1.28 V  
2.5 V  
5 V  
10 V  
2.56 V  
10.24 V  
20.48 V  
GENERAL DESCRIPTION  
The ADAS3022 is a complete 16-bit, 1 MSPS, successive approxi-  
mation–based analog-to-digital data acquisition system, which is  
manufactured on Analog Devices, Inc., proprietary iCMOS® high  
voltage industrial process technology. The device integrates an  
8-channel, low leakage multiplexer; a high impedance program-  
mable gain instrumentation amplifier (PGIA) stage with high  
common-mode rejection; a precision, low drift 4.096 V reference  
Single Ended1  
0 V to 1 V  
0 V to 2.5 V  
0 V to 5 V  
0 V to 10 V  
0.64 V  
1.28 V  
2.56 V  
5.12 V  
1 See Figure 59 and Figure 60 in the Analog Inputs section for more information.  
FUNCTIONAL BLOCK DIAGRAM  
AVDD  
DVDD  
VIO  
RESET  
PD  
VDDH  
DIFF TO  
COM  
DIFF  
PAIR  
ADAS3022  
CNV  
LOGIC/  
INTERFACE  
IN0/IN1  
BUSY  
IN0  
IN1  
CS  
IN2  
IN2/IN3  
IN4/IN5  
IN6/IN7  
IN3  
SCK  
DIN  
SDO  
PulSAR  
ADC  
PGIA  
MUX  
IN4  
IN5  
IN6  
IN7  
TEMP  
SENSOR  
COM  
AUX+  
BUF  
REFIN  
REF  
AUX–  
VSSH  
AGND  
DGND  
REFx  
Figure 1.  
Rev. A  
Document Feedback  
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Tel: 781.329.4700 ©2012–2013 Analog Devices, Inc. All rights reserved.  
Technical Support  
www.analog.com  
 
 
 
 
 
 
ADAS3022  
Data Sheet  
TABLE OF CONTENTS  
Features .............................................................................................. 1  
Typical Application Connection Diagram.............................. 24  
Analog Inputs.............................................................................. 25  
Voltage Reference Output/Input .............................................. 28  
Power Supply............................................................................... 29  
Conversion Modes ..................................................................... 30  
Digital Interface .............................................................................. 31  
Conversion Control ................................................................... 31  
Reset and Power-Down (PD) Inputs ....................................... 32  
Serial Data Interface................................................................... 32  
General Considerations............................................................. 33  
General Timing........................................................................... 34  
Configuration Register .............................................................. 36  
Channel Sequencer Details ....................................................... 37  
Outline Dimensions....................................................................... 39  
Ordering Guide .......................................................................... 39  
Applications....................................................................................... 1  
General Description ......................................................................... 1  
Functional Block Diagram .............................................................. 1  
Revision History ............................................................................... 2  
Specifications..................................................................................... 3  
Timing Specifications .................................................................. 7  
Absolute Maximum Ratings............................................................ 9  
ESD Caution.................................................................................. 9  
Pin Configuration and Function Descriptions........................... 10  
Typical Performance Characteristics ........................................... 12  
Terminology .................................................................................... 20  
Theory of Operation ...................................................................... 22  
Overview...................................................................................... 22  
ADAS3022 Operation................................................................ 22  
Transfer Function ....................................................................... 23  
REVISION HISTORY  
1/13—Rev. 0 to Rev. A  
Removed Endnote 3 and Added TA = 25°C to Gain Error Test  
Conditions/Comments, Table 2...................................................... 3  
Changes to REF1 and REF2 Description..................................... 11  
Added Figure 25 to Figure 28; Renumbered Sequentially ........ 15  
Changes to Figure 29...................................................................... 15  
Added Figure 30.............................................................................. 16  
Changes to Figure 33, Figure 34, and Figure 35 ......................... 16  
Changes to Figure 36 and Figure 37............................................. 17  
Changes to Figure 50...................................................................... 19  
Changes to Figure 54...................................................................... 24  
Changes to Figure 56...................................................................... 25  
Changes to Figure 57, Figure 58, Figure 59, and Figure 60....... 26  
Changes to Voltage Reference Output/Input Section, Figure 62,  
and Figure 63................................................................................... 28  
Changes to Core Supplies Section................................................ 29  
11/12—Revision 0: Initial Version  
Rev. A | Page 2 of 40  
 
Data Sheet  
ADAS3022  
SPECIFICATIONS  
VDDH = 15 V 5%, VSSH = −15 V 5%, AVDD = DVDD = 5 V 5%, VIO = 1.8 V to AVDD, internal reference, VREF = 4.096 V,  
fS = 1 MSPS. All specifications TMIN to TMAX, unless otherwise noted.  
Table 2.  
Parameter  
Test Conditions/Comments  
Min  
Typ  
Max  
Unit1  
RESOLUTION  
16  
Bits  
ANALOG INPUTS—IN[7:0], COM  
Operating Input Voltage Range  
Differential Input Voltage Range, VIN  
VIN  
VIN+ − VIN−  
−VSSH + 2.5  
VDDH − 2.5  
V
PGIA gain = 0.16, VIN = 49.15 V p-p  
PGIA gain = 0.2, VIN = 40.96 V p-p  
PGIA gain = 0.4, VIN = 20.48 V p-p  
PGIA gain = 0.8, VIN = 10.24 V p-p  
PGIA gain = 1.6, VIN = 5.12 V p-p  
PGIA gain = 3.2, VIN = 2.56 V p-p  
PGIA gain = 6.4, VIN = 1.28 V p-p  
−6VREF  
−5VREF  
−2.5VREF  
−1.25VREF  
−0.625VREF  
−0.3125VREF  
−0.1563VREF  
+6VREF  
+5VREF  
+2.5VREF  
+1.25VREF  
+0.625VREF  
+0.3125VREF  
+0.1563VREF  
V
V
V
V
V
V
V
Channel Off Leakage  
Channel On Leakage  
Common-Mode Voltage Range2  
0.6  
0.02  
nA  
nA  
VIN+, VIN−; full-scale differential inputs  
PGIA gain = 0.4  
PGIA gain = 0.8  
PGIA gain = 1.6  
PGIA gain = 3.2  
−5.12  
−7.68  
−8.96  
−9.60  
−9.92  
+5.12  
+7.68  
+8.96  
+9.60  
+9.92  
V
V
V
V
V
PGIA gain = 6.4  
ANALOG INPUTS—AUX+, AUX−  
Differential Input Voltage Range  
THROUGHPUT  
−VREF  
+VREF  
V
Conversion Rate  
One channel/one pair  
Two channels/two pairs  
Four channels/four pairs  
Eight channels  
0
0
0
0
1000  
500  
250  
125  
520  
kSPS  
kSPS  
kSPS  
kSPS  
ns  
Transient Response  
DC ACCURACY  
Full-scale step  
No Missing Codes  
Integral Linearity Error  
16  
−2  
−3  
−5  
−0.9  
−0.9  
−0.9  
Bits  
LSB  
LSB  
LSB  
LSB  
LSB  
LSB  
PGIA gain = 0.16, 0.2, 0.4, 0.8, 1.6  
PGIA gain = 3.2  
PGIA gain = 6.4  
PGIA gain = 0.16, 0.2, 0.4, 0.8, 1.6  
PGIA gain = 3.2  
PGIA gain = 6.4  
0.6  
1.0  
1.5  
0.6  
0.75  
0.75  
+2  
+3  
+5  
+1.0  
+1.25  
+1.25  
Differential Linearity Error  
Transition Noise  
External reference  
PGIA gain = 0.16, 0.2, 0.4, 0.8, 1.6  
PGIA gain = 3.2  
5
7
LSB  
LSB  
PGIA gain = 6.4  
11  
LSB  
Gain Error  
Gain Error Temperature Drift  
Offset Error  
External reference, all PGIA gains, TA = 25°C  
External reference, all PGIA gains  
External reference, TA = 25°C  
PGIA gain = 0.16, 0.2, 0.4, 0.8  
PGIA gain = 1.6  
−9  
+9  
0.1  
LSB  
ppm/°C  
−3.0  
−4.0  
−7.5  
−12.5  
+0.2  
+0.2  
+0.2  
+0.2  
+3.0  
+4.0  
+7.5  
+12.5  
LSB  
LSB  
LSB  
LSB  
PGIA gain = 3.2  
PGIA gain = 6.4  
Rev. A | Page 3 of 40  
 
ADAS3022  
Data Sheet  
Parameter  
Test Conditions/Comments  
External reference  
Min  
Typ  
Max  
Unit1  
Offset Error Temperature Drift  
PGIA gain = 0.16, 0.2, 0.4, 0.8  
PGIA gain = 1.6  
PGIA gain = 3.2  
0.1  
0.2  
0.4  
0.8  
0.5  
1.0  
2.0  
4.0  
ppm/°C  
ppm/°C  
ppm/°C  
ppm/°C  
PGIA gain = 6.4  
Total Unadjusted Error  
External reference, TA = 25°C  
PGIA gain = 0.16, 0.2, 0.4, 0.8, 1.6, 3.2  
PGIA gain = 6.4  
−9  
−15  
+9  
+15  
LSB  
LSB  
AC ACCURACY3  
Signal-to-Noise Ratio (SNR)  
fIN = 10 kHz  
PGIA gain = 0.16  
PGIA gain = 0.2  
PGIA gain = 0.4  
PGIA gain = 0.8  
PGIA gain = 1.6  
PGIA gain = 3.2  
PGIA gain = 6.4  
fIN = 10 kHz  
90.0  
90.0  
89.5  
89.0  
88.0  
86.0  
83.0  
91.5  
91.5  
91.5  
91.0  
89.7  
86.8  
84.5  
dB  
dB  
dB  
dB  
dB  
dB  
dB  
Signal-to-Noise-and-Distortion  
(SINAD)  
PGIA gain = 0.16  
PGIA gain = 0.2  
PGIA gain = 0.4  
PGIA gain = 0.8  
PGIA gain = 1.6  
88.0  
88.0  
88.5  
88.5  
87.5  
85.5  
82.5  
90.0  
90.0  
91.0  
90.5  
89.5  
86.5  
84.0  
dB  
dB  
dB  
dB  
dB  
dB  
dB  
PGIA gain = 3.2  
PGIA gain = 6.4  
Dynamic Range  
fIN = 10 kHz, −60 dB input  
PGIA gain = 0.16  
PGIA gain = 0.2  
91.0  
91.0  
90.5  
90.0  
89.0  
86.0  
83.5  
92.0  
92.0  
91.5  
91.0  
90.0  
87.0  
85.0  
−100  
101  
dB  
dB  
dB  
dB  
dB  
dB  
dB  
dB  
dB  
dB  
PGIA gain = 0.4  
PGIA gain = 0.8  
PGIA gain = 1.6  
PGIA gain = 3.2  
PGIA gain = 6.4  
Total Harmonic Distortion  
Spurious-Free Dynamic Range  
Channel-to-Channel Crosstalk  
Common-Mode Rejection Ratio  
(CMRR)  
fIN = 10 kHz, all PGIA gains  
fIN = 10 kHz, all PGIA gains  
fIN = 10 kHz, all channels inactive  
fIN = 2 kHz  
−120  
PGIA gain = 0.16, 0.2, 0.4, 0.8  
PGIA gain = 1.6  
PGIA gain = 3.2  
PGIA gain = 6.4  
−40 dBFS  
90.0  
90.0  
90.0  
90.0  
110.0  
105.0  
98.0  
98.0  
8
dB  
dB  
dB  
dB  
−3 dB Input Bandwidth  
AUXILIARY ADC INPUT CHANNEL  
DC Accuracy  
MHz  
External reference  
Integral Nonlinearity Error  
Differential Nonlinearity Error  
Gain Error  
−1.5  
−0.8  
−2.5  
−5  
0.5  
0.6  
0.2  
0.2  
+1.5  
+1.0  
+2.5  
+5  
LSB  
LSB  
LSB  
LSB  
Offset Error  
Rev. A | Page 4 of 40  
Data Sheet  
ADAS3022  
Parameter  
Test Conditions/Comments  
Min  
Typ  
Max  
Unit1  
AC Performance  
Internal reference  
Signal-to-Noise Ratio (SNR)  
Signal-to-Noise-and-Distortion  
(SINAD)  
90.0  
89.5  
93.0  
92.5  
dB  
dB  
Total Harmonic Distortion  
Spurious-Free Dynamic Range  
(SFDR)  
−105  
110  
dB  
dB  
INTERNAL REFERENCE  
REFx Output Voltage  
REFx Output Current  
REFx Temperature Drift  
TA = 25°C  
TA = 25°C  
REFEN = 1  
REFEN = 0  
AVDD = 5 V 5%  
4.088  
4.096  
250  
5
4.104  
2.505  
V
µA  
ppm/°C  
ppm/°C  
1
REFx Line Regulation  
Internal Reference  
Buffer Only  
REFIN Output Voltage4  
Turn-On Settling Time  
EXTERNAL REFERENCE  
Voltage Range  
20  
4
2.500  
100  
µV/V  
µV/V  
V
TA = 25°C  
CREFIN, CREF1, CREF2 = 10 µF and 0.1 µF  
2.495  
4.000  
ms  
REFx input  
REFIN input (buffered)  
VREF = 4.096 V  
4.096  
2.5  
100  
4.104  
2.505  
V
V
µA  
Current Drain  
TEMPERATURE SENSOR  
Output Voltage  
Temperature Sensitivity  
TA = 25 °C  
275  
800  
mV  
µV/°C  
DIGITAL INPUTS  
Logic Levels  
VIL  
VIH  
VIL  
VIH  
IIL  
IIH  
VIO > 3 V  
VIO > 3 V  
VIO ≤ 3 V  
VIO ≤ 3 V  
−0.3  
0.7 × VIO  
−0.3  
0.9 × VIO  
−1  
−1  
+0.3 × VIO  
VIO + 0.3  
+0.1 × VIO  
VIO + 0.3  
+1  
V
V
V
V
µA  
µA  
+1  
DIGITAL OUTPUTS5  
Data Format  
VOL  
VOH  
Twos complement  
0.4  
ISINK = +500 µA  
ISOURCE = −500 µA  
PD = 0  
V
V
VIO − 0.3  
POWER SUPPLIES  
VIO  
1.8  
AVDD + 0.3  
5.25  
5.25  
15.75  
−14.25  
3.5  
3.5  
4.0  
5.5  
9.5  
V
V
V
V
AVDD  
4.75  
4.75  
14.25  
−15.75  
5
5
15  
DVDD  
VDDH6  
VSSH6  
IVDDH  
VDDH > input voltage + 2.5 V  
VSSH < input voltage − 2.5 V  
PGIA gain = 0.16  
PGIA gain = 0.2  
PGIA gain = 0.4  
PGIA gain = 0.8  
PGIA gain = 1.6  
PGIA gain = 3.2  
PGIA gain = 6.4  
−15  
3.0  
3.0  
3.5  
5.0  
8.5  
15.5  
15.5  
100  
V
mA  
mA  
mA  
mA  
mA  
mA  
mA  
µA  
17.5  
17.5  
All PGIA gains, PD = 1  
Rev. A | Page 5 of 40  
ADAS3022  
Data Sheet  
Parameter  
Test Conditions/Comments  
PGIA gain = 0.16  
PGIA gain = 0.2  
PGIA gain = 0.4  
PGIA gain = 0.8  
PGIA gain = 1.6  
PGIA gain = 3.2  
PGIA gain = 6.4  
All PGIA gains, PD = 1  
PGIA gain = 6.4, reference buffer enabled  
Min  
Typ  
−2.5  
−2.5  
−3.0  
−4.5  
−8.0  
−15  
−15  
10  
Max  
Unit1  
mA  
mA  
mA  
mA  
mA  
mA  
mA  
µA  
IVSSH  
−3.0  
−3.0  
−3.5  
−5.5  
−9.5  
−17.5  
−17.5  
IAVDD  
18  
16  
21.0  
19.0  
mA  
mA  
All other PGIA gains, reference buffer  
enabled  
PGIA gain = 6.4, reference buffer disabled  
All other PGIA gains, reference buffer  
disabled  
14  
12  
17.5  
16.0  
mA  
mA  
All PGIA gains, PD = 1  
All PGIA gains, PD = 0  
All PGIA gains, PD = 1  
VIO = 3.3 V, PD = 0  
PD = 1  
100  
2.5  
10  
0.30  
10  
µA  
mA  
µA  
mA  
µA  
IDVDD  
IVIO  
3.5  
1.2  
Power Supply Sensitivity  
At TA = 25°C  
External reference  
PGIA gain = 0.16, 0.2, 0.4, 0.8; VDDH/VSSH 5%  
PGIA gain = 3.2, VDDH/VSSH 5%  
PGIA gain = 6.4, VDDH/VSSH 5%  
PGIA gain = 0.16, AVDD/DVDD 5%  
PGIA gain = 0.2, AVDD/DVDD 5%  
PGIA gain = 0.4, AVDD/DVDD 5%  
PGIA gain = 0.8, AVDD/DVDD 5%  
PGIA gain = 1.6, AVDD/DVDD 5%  
PGIA gain = 3.2, AVDD/DVDD 5%  
PGIA gain = 6.4, AVDD/DVDD 5%  
0.5  
1.0  
2.0  
0.6  
0.8  
1.0  
1.5  
2.0  
3.5  
7.0  
LSB  
LSB  
LSB  
LSB  
LSB  
LSB  
LSB  
LSB  
LSB  
LSB  
TEMPERATURE RANGE  
Specified Performance  
TMIN to TMAX  
−40  
+85  
°C  
1 LSB means least significant bit and changes depending on the voltage range. See the Programmable Gain section for the LSB size.  
2 The common-mode voltage (VCM) range for a PGIA gain of 0.16 or 0.2 is 0 V.  
3 All ac accuracy specifications expressed in decibels are referred to a full-scale input FSR and tested with an input signal at 0.5 dB below full scale, unless otherwise specified.  
4 This is the output from the internal band gap reference.  
5 There is no pipeline delay. Conversion results are available immediately after a conversion is complete.  
6 The differential input common-mode voltage (VCM) range changes according to the maximum input range selected and the high voltage power supplies (VDDH and  
VSSH). Note that the specified operating input voltage of any input pin requires 2.5 V of headroom from the VDDH and VSSH supplies; therefore, (VSSH + 2.5 V) ≤  
INx/COM ≤ (VDDH − 2.5 V).  
Rev. A | Page 6 of 40  
 
Data Sheet  
ADAS3022  
TIMING SPECIFICATIONS  
VDDH = 15 V 5ꢀ% VSSH = −15 V 5ꢀ% ꢁVDD = DVDD = 5 V 5ꢀ% VꢂO = 1.8 V to ꢁVDD% internal reference% VREF = 4.096 V%  
fS = 1 MSPS. ꢁll specifications TMꢂN to TMꢁX% unless otherwise noted.  
Table 3.  
Parameter  
Symbol  
Min  
Typ  
Max  
Unit  
Time Between Conversions  
Warp Mode,1 CMS = 0  
tCYC  
1
1000  
μs  
μs  
Normal Mode (Default), CMS = 1  
Conversion Time: CNV Rising Edge to Data Available  
Warp Mode, CMS = 0  
1.1  
tCONV  
825  
925  
ns  
ns  
ns  
ns  
ns  
ns  
ns  
Normal Mode (Default), CMS = 1  
Auxiliary ADC Input Channel Acquisition Time  
CNV Pulse Width  
1000  
tACQ  
tCH  
600  
10  
CNV High to Hold Time (Aperture Delay)  
CNV High to Busy Delay  
Safe Data Access Time During Conversion  
Quiet Conversion Time (BUSY High)  
Warp Mode, CMS = 0  
tAD  
2
tCBD  
tDDC  
tQUIET  
520  
500  
400  
500  
ns  
ns  
Normal Mode (Default), CMS = 1  
Data Access During Quiet Conversion Time  
Warp Mode, CMS = 0  
tDDCA  
200  
300  
ns  
ns  
ns  
ns  
ns  
ns  
Normal Mode (Default), CMS = 1  
SCK Period  
tSCK  
15  
5
SCK Low Time  
tSCKL  
tSCKH  
tSDOH  
tSDOD  
SCK High Time  
5
SCK Falling Edge to Data Valid  
SCK Falling Edge to Data Valid Delay  
VIO > 4.5 V  
4
12  
18  
24  
25  
37  
ns  
ns  
ns  
ns  
ns  
VIO > 3.0 V  
VIO > 2.7 V  
VIO > 2.3 V  
VIO > 1.8 V  
CS  
tEN  
/RESET/PD Low to SDO  
VIO > 4.5 V  
15  
16  
18  
23  
28  
25  
ns  
ns  
ns  
ns  
ns  
ns  
ns  
ns  
ns  
ns  
VIO > 3.0 V  
VIO > 2.7 V  
VIO > 2.3 V  
VIO > 1.8 V  
CS  
tDIS  
/RESET/PD High to SDO High Impedance  
DIN Valid Setup Time from SCK Rising Edge  
DIN Valid Hold Time from SCK Rising Edge  
tDINS  
tDINH  
tCCS  
tRH  
4
4
5
5
CS  
CNV Rising to  
RESET/PD High Pulse  
1 Exceeding the maximum time has an effect on the accuracy of the conversion (see the Conversion Modes section).  
I
500µA  
OL  
70% VIO  
30% VIO  
tDELAY  
tDELAY  
1.4V  
TO SDO  
1
1
2V OR VIO – 0.5V  
2V OR VIO – 0.5V  
C
L
50pF  
2
2
0.8V OR 0.5V  
0.8V OR 0.5V  
1
500µA  
I
2V IF VIO > 2.5V; VIO – 0.5V IF VIO < 2.5V.  
0.8V IF VIO > 2.5V; 0.5V IF VIO < 2.5V.  
OH  
2
Figure 3. Voltage Levels for Timing  
Figure 2. Load Circuit for Digital Interface Timing  
Rev. A | Page 7 of 40  
 
 
ADAS3022  
Data Sheet  
tACQ  
EOC  
tCYC  
SOC  
SOC  
EOC  
tQUIET  
NOTE 2  
tDDC  
NOTE 1  
tDAC  
NOTE 1  
POWER  
UP  
CONVERSION (n – 1)  
UNDEFINED  
ACQUISITION (n)  
UNDEFINED  
CONVERSION (n)  
UNDEFINED  
ACQUISITION (n + 1)  
UNDEFINED  
CONVERSION (n + 1)  
UNDEFINED  
PHASE  
CNV  
BUSY  
tDDCA  
NOTE 2  
NOTE 5  
tAD  
NOTE 4  
CS  
X
1
16/32  
NOTE 3  
1
16  
SCK  
CFG  
INVALID  
CFG (n + 2)  
CFG (n + 2)  
CFG (n + 3)  
CFG (n + 3)  
DIN  
DATA  
INVALID  
DATA (n – 1)  
INVALID  
DATA (n – 1)  
INVALID  
DATA (n)  
INVALID  
DATA (n)  
INVALID  
SDO  
EOC  
EOC  
EOC  
ACQUISITION  
(n + 4)  
CONVERSION  
(n + 2)  
ACQUISITION  
(n + 3)  
CONVERSION  
(n + 3)  
CONVERSION  
(n + 4)  
ACQUISITION  
(n + 2)  
PHASE  
CNV  
BUSY  
CS  
1
1
16  
16  
1
SCK  
CFG (n + 4)  
CFG (n + 4)  
CFG (n + 5)  
CFG (n + 5)  
CFG (n + 6)  
CFG (n + 6)  
DIN  
DATA (n + 1)  
INVALID  
DATA (n + 1)  
INVALID  
SDO  
DATA (n + 2)  
DATA (n + 2)  
DATA (n + 3)  
DATA (n + 3)  
NOTES  
1. DATA ACCESS CAN OCCUR DURING A CONVERSION (tDDC), AFTER A CONVERSION (tDAC), OR BOTH DURING AND AFTER A CONVERSION.  
THE CONVERSION RESULT AND THE CFG REGISTER ARE UPDATED AT THE END OF A CONVERSION (EOC).  
2. DATA ACCESS CAN ALSO OCCUR UP TO tDDCA WHILE BUSY IS ACTIVE (SEE THE DIGITAL INTERFACE SECTION FOR DETAILS). ALL OF THE BUSY  
TIME CAN BE USED TO ACQUIRE DATA.  
3. A TOTAL OF 16 SCK FALLING EDGES IS REQUIRED FOR A CONVERSION RESULT. AN ADDITIONAL 16 EDGES ARE REQUIRED TO  
READ BACK THE CFG RESULT ASSOCIATED WITH THE CURRENT CONVERSION.  
4. CS CAN BE HELD LOW OR CONNECTED TO CNV. CS WITH FULL INDEPENDENT CONTROL IS SHOWN IN THIS FIGURE.  
5. FOR OPTIMAL PERFORMANCE, DATA ACCESS SHOULD NOT OCCUR DURING THE SAMPLING EDGE. A MINIMUM TIME  
OF THE APERTURE DELAY (tAD) SHOULD ELAPSE PRIOR TO DATA ACCESS.  
Figure 4. General Timing Diagram  
Rev. A | Page 8 of 40  
Data Sheet  
ADAS3022  
ABSOLUTE MAXIMUM RATINGS  
Table 4.  
Parameter  
Stresses above those listed under Absolute Maximum Ratings  
may cause permanent damage to the device. This is a stress  
rating only; functional operation of the device at these or any  
other conditions above those indicated in the operational  
section of this specification is not implied. Exposure to absolute  
maximum rating conditions for extended periods may affect  
device reliability.  
Rating  
Analog Inputs/Outputs  
INx, COM to AGND  
AUX+, AUX− to AGND  
REFx to AGND  
REFIN to AGND  
REFN to AGND  
VSSH − 0.3 V to VDDH + 0.3 V  
−0.3 V to AVDD + 0.3 V  
AGND − 0.3 V to AVDD + 0.3 V  
AGND −0.3 V to +2.7 V  
0.3 V  
Ground Voltage Differences  
AGND, RGND, DGND  
Supply Voltages  
ESD CAUTION  
0.3 V  
VDDH to AGND  
VSSH to AGND  
−0.3 V to +16.5 V  
+0.3 V to −16.5 V  
−0.3 V to +7 V  
AVDD, DVDD, VIO to AGND  
ACAP, DCAP, RCAP to GND  
Digital Inputs/Outputs  
CNV, DIN, SCK, RESET, PD, CS  
to DGND  
−0.3 V to +2.7 V  
−0.3 V to VIO + 0.3 V  
SDO, BUSY to DGND  
Internal Power Dissipation  
Junction Temperature  
Storage Temperature Range  
θJA Thermal Impedance  
θJC Thermal Impedance  
−0.3 V to VIO + 0.3 V  
2 W  
125°C  
−65°C to +125°C  
44.1°C/W  
0.28°C/W  
Rev. A | Page 9 of 40  
 
 
 
ADAS3022  
Data Sheet  
PIN CONFIGURATION AND FUNCTION DESCRIPTIONS  
PIN 1  
IN0  
IN1  
IN2  
IN3  
AUX+  
IN4  
IN5  
IN6  
IN7  
COM 10  
1
2
3
4
5
6
7
8
9
30 NC  
29 NC  
INDICATOR  
28 AVDD  
27 DVDD  
26 ACAP  
25 DCAP  
24 AGND  
23 AGND  
22 DGND  
21 DGND  
ADAS3022  
TOP VIEW  
(Not to Scale)  
NOTES  
1. NC = NO CONNECT. THIS PIN IS NOT INTERNALLY CONNECTED.  
2. THE EXPOSED PADDLE SHOULD BE CONNECTED TO VSSH.  
Figure 5. Pin Configuration  
Table 5. Pin Function Descriptions  
Pin No.  
1 to 4  
5
6 to 9  
10  
Mnemonic Type1 Description  
IN0 to IN3  
AUX+  
AI  
AI  
AI  
AI  
Input Channel 0 to Input Channel 3.  
Auxiliary Input Channel Positive Input.  
Input Channel 4 to Input Channel 7.  
IN4 to IN7  
COM  
IN[7:0] Common Channel Input. The IN[7:0] input channels can be referenced to a common point. The  
maximum voltage on this pin is 10.24 V for all PGIA gains except for a PGIA gain of 0.16, in which case  
the maximum voltage on this pin is 12.228 V. AUX+ and AUX− are not referenced to COM.  
11  
12  
13  
CS  
DI  
DI  
DI  
Chip Select. Active low signal. Enables the digital interface for writing and reading data. Use this pin  
when sharing the serial bus. For a dedicated ADAS3022 serial interface, CS can be tied to DGND or CNV  
to simplify the interface.  
Data Input. Serial data input used for writing the 16-bit configuration word (CFG) that is latched on SCK  
rising edges. CFG is an internal register that is updated on the rising edge of the end of a conversion, which is  
the falling edge of BUSY. The configuration register can be written to during and after a conversion.  
DIN  
RESET  
Asynchronous Reset. A low-to-high transition resets the ADAS3022. The current conversion, if active, is  
aborted and CFG is reset to the default state.  
14, 29, 30  
15  
NC  
PD  
NC  
DI  
No Connect. This pin is not connected internally.  
Power-Down. A low-to-high transition powers down the ADAS3022, minimizing the bias current. Note  
that this pin must be held high until the user is ready to power on the device; after powering on the  
device, the user must wait 100 ms until the reference is enabled and then wait for the completion of  
two dummy conversions before the device is ready to convert. See the Power-Down Mode section for  
more information.  
16  
17  
SCK  
VIO  
DI  
P
Serial Clock Input. The DIN and SDO data sent to and from the ADAS3022 are synchronized with SCK.  
Digital Interface Supply. Nominally, this supply should be at the same voltage as the supply of the host  
interface: 1.8 V, 2.5 V, 3.3 V, or 5 V.  
18  
19  
SDO  
DO  
DO  
Serial Data Output. The conversion result is output on this pin and is synchronized to SCK falling edges.  
The conversion result is output in twos complement format.  
Busy Output. An active high signal on this pin indicates that a conversion is in process. Reading or  
writing data during the quiet conversion phase (tQUIET) may cause incorrect bit decisions.  
BUSY  
20  
CNV  
DI  
P
P
Convert Input. A conversion is initiated on the rising edge of this pin.  
Digital Ground. Connect these pins to the system digital ground plane.  
Analog Ground. Connect these pins to the system analog ground plane.  
Internal 2.5 V Digital Regulator Output. Decouple this internally regulated output using a 10 μF  
capacitor and a 0.1 μF local capacitor.  
21, 22  
23, 24  
25  
DGND  
AGND  
DCAP  
P
26  
ACAP  
P
Internal 2.5 V Analog Regulator Output. This regulator supplies power to the internal ADC core and all  
of the supporting analog circuits with the exception of the internal reference. Decouple this internally  
regulated output using a 10 μF capacitor and a 0.1 μF local capacitor.  
Rev. A | Page 10 of 40  
 
Data Sheet  
ADAS3022  
Pin No.  
27  
28  
Mnemonic Type1 Description  
DVDD  
AVDD  
RCAP  
P
P
P
Digital 5 V Supply. Decouple this supply using a 10 μF capacitor and a 0.1 μF local capacitor.  
Analog 5 V Supply. Decouple this supply using a 10 μF capacitor and a 0.1 μF local capacitor.  
Internal 2.5 V Analog Regulator Output. This regulator supplies power to the internal reference.  
Decouple this pin using a 1 μF capacitor connected to RCAP and a 0.1 μF local capacitor.  
31  
32  
REFIN  
AI/O  
Internal 2.5 V Band Gap Reference Output, Reference Buffer Input, or Reference Power-Down Input. See  
the Voltage Reference Input/Output section for more information.  
33, 34  
REF1, REF2 AI/O  
Reference Input/Output. Regardless of the reference method, these pins need individual decoupling  
using external 10 μF ceramic capacitors connected as close to REF1, REF2, and REFN as possible. See  
the Voltage Reference Output/Input section for more information. REF1 and REF2 must be tied  
together externally.  
35  
36, 37  
RGND  
REFN  
P
P
Reference Supply Ground. Connect this pin to the system analog ground plane.  
Reference Input/Output Ground. Connect the 10 μF capacitors on REF1 and REF2 to these pins, and  
connect these pins to the system analog ground plane.  
38  
39  
40  
VSSH  
P
High Voltage Analog Negative Supply. Nominally, the supply of this pin should be −15 V. Decouple this  
pin using a 10 μF capacitor and a 0.1 μF local capacitor.  
High Voltage Analog Positive Supply. Nominally, the supply of this pin should be +15 V. Decouple this  
pin using a 10 μF capacitor and a 0.1 μF local capacitor.  
Auxiliary Input Channel Negative Input.  
Exposed Paddle. The exposed paddle should be connected to VSSH.  
VDDH  
P
AUX−  
EPAD  
AI  
1AI = analog input, AI/O = analog input/output, DI = digital input, DO = digital output, and P = power.  
Rev. A | Page 11 of 40  
 
ADAS3022  
Data Sheet  
TYPICAL PERFORMANCE CHARACTERISTICS  
VDDH = 15 V, VSSH = −15 V, AVDD = DVDD = 5 V, VIO = 1.8 V to AVDD, unless otherwise noted.  
2.0  
1.00  
0.75  
0.50  
0.25  
0
GAIN = 0.16, 0.2, 0.4, 0.8, 1.6  
INL MAX = 0.649  
INL MIN = –0.592  
FOR ALL GAINS  
1.5  
1.0  
0.5  
0
–0.5  
–1.0  
–1.5  
–2.0  
–0.25  
–0.50  
–0.75  
–1.00  
0
8192 16384 24576 32768 40960 49152 57344 65536  
CODE  
0
8192 16384 24576 32768 40960 49152 57344 65536  
CODE  
Figure 6. Integral Nonlinearity vs. Code,  
PGIA Gain = 0.16, 0.2, 0.4, 0.8, and 1.6  
Figure 9. Differential Nonlinearity vs. Code for All PGIA Gains  
400,000  
2.0  
1.5  
GAIN = 3.2  
INL MAX = 1.026  
INL MIN = –0.948  
GAIN = 0.16, 0.2, 0.4, 0.8, 1.6  
350,000  
300,000  
250,000  
200,000  
150,000  
100,000  
50,000  
0
300,200  
1.0  
0.5  
0
152,600  
–0.5  
–1.0  
–1.5  
–2.0  
52,300  
6,400  
600  
0
8192 16384 24576 32768 40960 49152 57344 65536  
CODE  
CODE IN HEX  
Figure 7. Integral Nonlinearity vs. Code, PGIA Gain = 3.2  
Figure 10. Histogram of a DC Input at Code Center,  
PGIA Gain = 0.16, 0.2, 0.4, 0.8, and 1.6  
2.0  
1.5  
400,000  
350,000  
300,000  
250,000  
200,000  
150,000  
100,000  
50,000  
0
GAIN = 6.4  
INL MAX = 0.558  
INL MIN = –1.319  
GAIN = 3.2  
1.0  
0.5  
213,200  
0
–0.5  
–1.0  
–1.5  
–2.0  
129,000  
118,400  
25,500  
1,600  
22,700  
1,400  
0
8192 16384 24576 32768 40960 49152 57344 65536  
CODE  
CODE IN HEX  
Figure 8. Integral Nonlinearity vs. Code, PGIA Gain = 6.4  
Figure 11. Histogram of a DC Input at Code Center, PGIA Gain = 3.2  
Rev. A | Page 12 of 40  
 
Data Sheet  
ADAS3022  
400,000  
100  
90  
80  
70  
60  
50  
40  
30  
20  
10  
0
EXTERNAL REFERENCE  
GAIN = 6.4  
S = 1000kSPS  
GAIN = 6.4  
350,000  
300,000  
250,000  
200,000  
150,000  
100,000  
50,000  
0
f
157,300  
151,900  
82,000  
75,100  
21,700  
18,400  
2,400  
300  
200  
100  
0
0.4 0.8 1.2 1.6 2.0 2.4 2.8 3.2 3.6 4.0  
OFFSET DRIFT (ppm/°C)  
CODE IN HEX  
Figure 15. Offset Drift, PGIA Gain = 6.4  
Figure 12. Histogram of a DC Input at Code Center, PGIA Gain = 6.4  
100  
120  
100  
80  
60  
40  
20  
0
112  
EXTERNAL REFERENCE  
fS = 1000kSPS  
EXTERNAL 2.5V REFERENCE  
INTERNAL BUFFER  
GAIN = 0.16, 0.2, 0.4, 0.8, 1.6  
S = 1000kSPS  
90  
80  
70  
60  
50  
40  
30  
20  
10  
0
f
72  
23  
2
0
0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1.0  
OFFSET DRIFT (ppm/°C)  
0
1
2
3
4
5
6
7
8
9
10  
REFERENCE BUFFER DRIFT (ppm/°C)  
Figure 13. Offset Drift, PGIA Gain = 0.16, 0.2, 0.4, 0.8, and 1.6  
Figure 16. Reference Buffer Drift, External Reference  
100  
120  
100  
80  
60  
40  
20  
0
EXTERNAL REFERENCE  
GAIN = 3.2  
fS = 1000kSPS  
INTERNAL 2.5V REFERENCE  
INTERNAL BUFFER  
90  
80  
70  
60  
50  
40  
30  
20  
10  
0
fS = 1000kSPS  
46  
38  
35  
30  
15 15  
11  
10  
6
2
1
0
1
2
3
4
5
6
7
8
9
10 11 12 13 14 15  
0
0.2 0.4 0.6 0.8 1.0 1.2 1.4 1.6 1.8 2.0  
OFFSET DRIFT (ppm/°C)  
REFERENCE BUFFER DRIFT (ppm/°C)  
Figure 14. Offset Drift, PGIA Gain = 3.2  
Figure 17. Reference Buffer Drift, Internal Reference  
Rev. A | Page 13 of 40  
ADAS3022  
Data Sheet  
0
0
–20  
GAIN = 0.16  
fS = 1000kSPS  
GAIN = 0.8  
fS = 1000kSPS  
–20  
fIN = 10.1kHz  
fIN = 10.1kHz  
–40  
–40  
SNR = 91.7dB  
SINAD = 89.2dB  
THD = –92.5dB  
SFDR = 92.5dB  
SNR = 90.7dB  
SINAD = 90.6dB  
THD = –107dB  
SFDR = 106dB  
–60  
–60  
–80  
–80  
–100  
–120  
–140  
–160  
–100  
–120  
–140  
–160  
–180  
–180  
0
100  
200  
300  
400  
500  
0
100  
200  
300  
400  
500  
FREQUENCY (kHz)  
FREQUENCY (kHz)  
Figure 18. 10 kHz FFT, PGIA Gain = 0.16  
Figure 21. 10 kHz FFT, PGIA Gain = 0.8  
0
–20  
0
–20  
GAIN = 0.2  
fS = 1000kSPS  
GAIN = 1.6  
fS = 1000kSPS  
fIN = 10.1kHz  
fIN = 10.1kHz  
–40  
–40  
SNR = 91.4dB  
SINAD = 89.9dB  
THD = –94.7dB  
SFDR = 94.8dB  
SNR = 89.8dB  
SINAD = 89.7dB  
THD = –106dB  
SFDR = 107dB  
–60  
–60  
–80  
–80  
–100  
–120  
–140  
–160  
–100  
–120  
–140  
–160  
–180  
–180  
0
100  
200  
300  
400  
500  
0
100  
200  
300  
400  
500  
FREQUENCY (kHz)  
FREQUENCY (kHz)  
Figure 19. 10 kHz FFT, PGIA Gain = 0.2  
Figure 22. 10 kHz FFT, PGIA Gain = 1.6  
0
–20  
0
–20  
GAIN = 0.4  
fS = 1000kSPS  
GAIN = 3.2  
fS = 1000kSPS  
fIN = 10.1kHz  
fIN = 10.1kHz  
–40  
–40  
SNR = 91.2dB  
SINAD = 91.0dB  
THD = –103dB  
SFDR = 104dB  
SNR = 87.6dB  
SINAD = 87.5dB  
THD = –105dB  
SFDR = 106dB  
–60  
–60  
–80  
–80  
–100  
–120  
–140  
–160  
–100  
–120  
–140  
–160  
–180  
–180  
0
100  
200  
300  
400  
500  
0
100  
200  
300  
400  
500  
FREQUENCY (kHz)  
FREQUENCY (kHz)  
Figure 20. 10 kHz FFT, PGIA Gain = 0.4  
Figure 23. 10 kHz FFT, PGIA Gain = 3.2  
Rev. A | Page 14 of 40  
Data Sheet  
ADAS3022  
0
–55  
–60  
GAIN = 0.4, –0.5dBFS  
GAIN = 0.8, –0.5dBFS  
GAIN = 1.6, –0.5dBFS  
GAIN = 3.2, –0.5dBFS  
GAIN = 0.4, –10dBFS  
GAIN = 0.8, –10dBFS  
GAIN = 1.6, –10dBFS  
GAIN = 3.2, –10dBFS  
GAIN = 6.4  
fS = 1000kSPS  
fIN = 10.1kHz  
SNR = 85.7dB  
SINAD = 85.6dB  
THD = –101dB  
SFDR = 103dB  
–20  
–65  
–70  
–40  
–75  
–60  
–80  
–85  
–80  
–90  
–100  
–120  
–140  
–160  
–95  
–100  
–105  
–110  
–115  
–120  
–125  
–180  
0
1
10  
100  
1000  
100  
200  
300  
400  
500  
1000  
1000  
FREQUENCY (kHz)  
FREQUENCY (kHz)  
Figure 24. 10 kHz FFT, PGIA Gain = 6.4  
Figure 27. THD vs. Frequency  
100  
95  
90  
85  
80  
75  
70  
–60  
–70  
INTERNAL REFERENCE  
CHANNEL 4 TO COM, SEQUENCER DISABLED  
VIN = –0.5dBFS ON CHANNELS 0 TO 3, 5 TO 7  
fS = 1000kSPS  
–80  
–90  
–100  
–110  
–120  
–130  
–140  
GAIN = 0.4, –0.5dBFS  
GAIN = 0.8, –0.5dBFS  
GAIN = 1.6, –0.5dBFS  
GAIN = 3.2, –0.5dBFS  
GAIN = 0.4, –10dBFS  
GAIN = 0.8, –10dBFS  
GAIN = 1.6, –10dBFS  
GAIN = 3.2, –10dBFS  
1
10  
100  
0
20  
40  
60  
80  
100 120 140 160 180 200  
FREQUENCY (kHz)  
FREQUENCY (kHz)  
Figure 25. SNR vs. Frequency  
Figure 28. Crosstalk vs. Frequency  
100  
95  
90  
85  
80  
75  
70  
65  
60  
55  
50  
130  
120  
110  
100  
90  
GAIN = 0.16  
GAIN = 0.20  
GAIN = 0.40  
GAIN = 0.80  
GAIN = 1.60  
GAIN = 3.20  
GAIN = 6.40  
GAIN = 0.4, –0.5dBFS  
GAIN = 0.8, –0.5dBFS  
GAIN = 1.6, –0.5dBFS  
GAIN = 3.2, –0.5dBFS  
GAIN = 0.4, –10dBFS  
GAIN = 0.8, –10dBFS  
GAIN = 1.6, –10dBFS  
GAIN = 3.2, –10dBFS  
80  
COMMON-MODE AMPLITUDE = 20.48V p-p  
INTERNAL REFERENCE  
fS = 1000kSPS  
70  
60  
1
10  
100  
1
10  
100  
1k  
10k  
100k  
FREQUENCY (Hz)  
FREQUENCY (kHz)  
Figure 26. SINAD vs. Frequency  
Figure 29. CMRR vs. Frequency  
Rev. A | Page 15 of 40  
ADAS3022  
Data Sheet  
20  
18  
16  
14  
12  
10  
–50  
PSRR VDDH  
PSRR VSSH  
GAIN = 0.2  
GAIN = 1.6  
GAIN = 0.4  
GAIN = 3.2  
GAIN = 0.8  
GAIN = 6.4  
AVDD, GAIN = 0.2  
AVDD, GAIN = 3.2  
AVDD, GAIN = 1.6  
AVDD, GAIN = 6.4  
–55  
–60  
–65  
–70  
–75  
–80  
–85  
–90  
–95  
–100  
0.01  
0.1  
1
10  
100  
10  
100  
THROUGHPUT (kSPS)  
1000  
FREQUENCY (kHz)  
Figure 30. PSRR vs. Frequency  
Figure 33. AVDD Current vs. Throughput, Internal Reference  
15  
14  
13  
12  
11  
10  
9
19  
18  
17  
16  
15  
14  
13  
GAIN = 0.2  
GAIN = 1.6  
GAIN = 0.4  
GAIN = 3.2  
GAIN = 0.8  
GAIN = 6.4  
GAIN = 0.2  
GAIN = 1.6  
GAIN = 0.4  
GAIN = 3.2  
GAIN = 0.8  
GAIN = 6.4  
10  
100  
THROUGHPUT (kSPS)  
1000  
4.7  
4.8  
4.9  
5.0  
AVDD SUPPLY (V)  
5.1  
5.2  
5.3  
Figure 34. AVDD Current vs. Throughput, External Reference  
Figure 31. AVDD Current vs. Supply, Internal Reference  
4.5  
4.0  
3.5  
3.0  
2.5  
2.0  
1.5  
1.0  
0.5  
15  
14  
13  
12  
11  
10  
GAIN = 0.2  
GAIN = 1.6  
GAIN = 0.4  
GAIN = 3.2  
GAIN = 0.8  
GAIN = 6.4  
GAIN = 0.2  
GAIN = 1.6  
GAIN = 0.4  
GAIN = 3.2  
GAIN = 0.8  
GAIN = 6.4  
10  
100  
THROUGHPUT (kSPS)  
1000  
4.7  
4.8  
4.9  
5.0  
AVDD SUPPLY (V)  
5.1  
5.2  
5.3  
Figure 35. DVDD Current vs. Throughput  
Figure 32. AVDD Current vs. Supply, External Reference  
Rev. A | Page 16 of 40  
Data Sheet  
ADAS3022  
0
–2  
18  
fS = 1000kSPS  
GAIN = 0.2  
GAIN = 1.6  
GAIN = 0.4  
GAIN = 3.2  
GAIN = 0.8  
GAIN = 6.4  
15  
12  
9
–4  
–6  
–8  
–10  
–12  
–14  
–16  
–18  
–20  
6
3
GAIN = 0.2  
GAIN = 1.6  
GAIN = 0.4  
GAIN = 3.2  
GAIN = 0.8  
GAIN = 6.4  
0
10  
100  
THROUGHPUT (kSPS)  
1000  
–50 –40 –30 –20 –10  
0
10 20 30 40 50 60 70 80 90  
TEMPERATURE (°C)  
Figure 36. VDDH Current vs. Throughput  
Figure 39. VSSH Current vs. Temperature  
19.5  
19.0  
18.5  
18.0  
17.5  
17.0  
16.5  
16.0  
0
–3  
GAIN = 0.2  
GAIN = 1.6  
GAIN = 0.4  
GAIN = 3.2  
GAIN = 0.8  
GAIN = 6.4  
fS = 1000kSPS  
–6  
–9  
–12  
–15  
–18  
GAIN = 0.2  
GAIN = 1.6  
GAIN = 0.4  
GAIN = 3.2  
GAIN = 0.8  
GAIN = 6.4  
10  
100  
THROUGHPUT (kSPS)  
1000  
–50 –40 –30 –20 –10  
0
10 20 30 40 50 60 70 80 90  
TEMPERATURE (°C)  
Figure 37. VSSH Current vs. Throughput  
Figure 40. AVDD Current vs. Temperature  
20  
18  
16  
14  
12  
10  
8
1.0  
0.9  
0.8  
0.7  
0.6  
0.5  
0.4  
0.3  
0.2  
0.1  
0
GAIN = 0.2  
GAIN = 1.6  
GAIN = 0.4  
GAIN = 3.2  
GAIN = 0.8  
GAIN = 6.4  
VIO = 3.3V  
fS = 1000kSPS  
GAIN = 0.2  
GAIN = 1.6  
GAIN = 0.4  
GAIN = 3.2  
GAIN = 0.8  
GAIN = 6.4  
fS = 1000kSPS  
6
4
2
0
–50 –40 –30 –20 –10  
0
10 20 30 40 50 60 70 80 90  
–50 –40 –30 –20 –10  
0
10 20 30 40 50 60 70 80 90  
TEMPERATURE (°C)  
TEMPERATURE (°C)  
Figure 38. VDDH Current vs. Temperature  
Figure 41. DVDD Current vs. Temperature  
Rev. A | Page 17 of 40  
ADAS3022  
Data Sheet  
5
4
4.00  
GAIN = 0.2  
GAIN = 1.6  
GAIN = 0.4  
GAIN = 3.2  
GAIN = 0.8  
GAIN = 6.4  
GAIN = 0.16  
GAIN = 0.2  
GAIN = 0.4  
GAIN = 0.8  
GAIN = 1.6  
GAIN = 3.2  
GAIN = 6.4  
fS = 1000kSPS  
fS = 1000kSPS  
EXTERNAL REFERENCE  
3.75  
3.50  
3.25  
3.00  
2.75  
2.50  
2.25  
2.00  
3
2
1
0
–1  
–2  
–3  
–4  
–5  
–50 –40 –30 –20 –10  
0
10 20 30 40 50 60 70 80 90  
–50 –40 –30 –20 –10  
0
10 20 30 40 50 60 70 80 90  
TEMPERATURE (°C)  
TEMPERATURE (°C)  
Figure 45. Gain Error vs. Temperature  
Figure 42. VIO Current vs. Temperature  
12  
8
100  
98  
96  
94  
92  
90  
88  
86  
84  
82  
80  
fS = 1000kSPS  
GAIN = 0.16  
GAIN = 0.16  
GAIN = 0.2  
GAIN = 0.4  
GAIN = 0.8  
GAIN = 1.6  
GAIN = 3.2  
GAIN = 6.4  
fS = 1000kSPS  
GAIN = 0.2  
GAIN = 0.4  
GAIN = 0.8  
GAIN = 1.6  
GAIN = 3.2  
GAIN = 6.4  
EXTERNAL REFERENCE  
4
0
–4  
–8  
–12  
–50 –40 –30 –20 –10  
0
10 20 30 40 50 60 70 80 90  
–50 –40 –30 –20 –10  
0
10 20 30 40 50 60 70 80 90  
TEMPERATURE (°C)  
TEMPERATURE (°C)  
Figure 46. Offset Error vs. Temperature  
Figure 43. SNR vs. Temperature  
5
4
–80  
–85  
GAIN = 0.16  
fS = 1000kSPS  
EXTERNAL REFERENCE  
GAIN = 0.2  
GAIN = 0.4  
GAIN = 0.8  
GAIN = 1.6  
GAIN = 3.2  
GAIN = 6.4  
3
–90  
2
GAIN ERROR  
–95  
1
0
–100  
–105  
–110  
–115  
–120  
OFFSET ERROR  
–1  
–2  
–3  
–4  
–5  
–50 –40 –30 –20 –10  
0
10 20 30 40 50 60 70 80 90  
–50 –40 –30 –20 –10  
0
10 20 30 40 50 60 70 80 90  
TEMPERATURE (°C)  
TEMPERATURE (°C)  
Figure 47. Offset and Gain Errors of the AUX ADC Channel Pair vs. Temperature  
Figure 44. THD vs. Temperature  
Rev. A | Page 18 of 40  
Data Sheet  
ADAS3022  
5600  
5400  
5200  
5000  
4800  
4600  
4400  
4200  
4000  
3800  
3600  
3400  
32  
28  
24  
20  
16  
12  
8
25  
20  
15  
10  
5
T
= 25°C  
A
INTERNAL REFERENCE  
4
0
0
–50 –40 –30 –20 –10  
0
10 20 30 40 50 60 70 80 90  
0
100 200 300 400 500 600 700 800 900 1000  
THROUGHPUT (kSPS)  
TEMPERATURE (°C)  
Figure 48. Temperature Sensor Output Code vs. Temperature  
Figure 50. Temperature Sensor Output Error vs. Throughput  
0.5  
0
–0.5  
–1.0  
–1.5  
–2.0  
–2.5  
–3.0  
–0.5dBFS  
–3.5  
GAIN = 0.2  
GAIN = 0.8  
GAIN = 3.2  
GAIN = 0.4  
GAIN = 1.6  
GAIN = 6.4  
–4.0  
–4.5  
10  
100  
1k  
10k  
FREQUENCY (Hz)  
Figure 49. Large Signal Frequency Response vs. Gain  
Rev. A | Page 19 of 40  
ADAS3022  
Data Sheet  
TERMINOLOGY  
Operating Input Voltage Range  
Differential Nonlinearity (DNL) Error  
Operating input voltage range is the maximum input voltage  
range, including the common-mode voltage, allowed on the  
input channels IN[7:0] and COM.  
In an ideal ADC, code transitions are 1 LSB apart. DNL is the  
maximum deviation from this ideal value. It is often specified in  
terms of resolution for which no missing codes are guaranteed.  
Differential Input Voltage Range  
Offset Error  
Differential input voltage range is the maximum differential  
full-scale input range. The value changes according to the  
programmable gain setting.  
Offset error is the deviation of the actual MSB transition from  
the ideal MSB transition point. The ideal MSB transition occurs  
at an input level ½ LSB above analog ground.  
Channel Off Leakage  
Channel off leakage is the leakage current with the channel off.  
Gain Error  
The last transition (from 111 … 10 to 111 … 11) for an analog  
voltage should occur 1½ LSB below the nominal full scale. The  
gain error is the deviation expressed in LSB (or as a percentage  
of the full-scale range) of the actual level of the last transition  
from the ideal level after the offset error is removed. Closely  
related to this parameter is the full-scale error (also expressed in  
LSB or as a percentage of the full-scale range), which includes  
the effects of the offset error.  
Channel On Leakage  
Channel on leakage is the leakage current with the channel on.  
Charge Injection  
Charge injection is a measure of the glitch impulse that is  
transferred through the analog input pin into the source when  
the sample is taken and/or the multiplexer is switched.  
Total Unadjusted Error (TUE)  
Common-Mode Rejection Ratio (CMRR)  
TUE is the deviation of each code from an ideal transfer function  
and is a combination of all error contributors, including non-  
linearity, offset error, and gain error. TUE for the ADAS3022 is  
expressed as the maximum deviation in LSB or as a percentage  
of the full-scale range.  
CMRR is the ratio of the amplitude of a signal referred to input in  
the converted result to the amplitude of the modulation common  
to a pair of inputs and is expressed in decibels. CMRR is a measure  
of the ability of the ADAS3022 to reject signals, such as power  
line noise, that are common to the inputs. This specification is  
for a 2 kHz sine wave of 20.48 V p-p applied to both channels of  
an input pair.  
Aperture Delay  
Aperture delay is a measure of the acquisition performance. It is  
the time between the rising edge of the CNV input and the point  
at which the input signal is held for a conversion.  
Transient Response  
Transient response is a measure of the time required for the  
ADAS3022 to properly acquire the input after a full-scale step  
function is applied to the system.  
Dynamic Range  
Dynamic range is the ratio of the rms value of the full-scale signal  
to the total rms noise measured with the inputs shorted together.  
The value for the dynamic range is expressed in decibels.  
Least Significant Bit (LSB)  
LSB is the smallest increment that can be represented by a  
converter. For a fully differential input ADC with N bits of  
resolution, the LSB expressed in volts is  
Signal-to-Noise Ratio (SNR)  
SNR is the ratio of the rms value of the actual input signal to the  
rms sum of all other spectral components below the Nyquist  
frequency, excluding harmonics and dc. The value for SNR is  
expressed in decibels.  
2VREF  
LSB (V) =  
2N  
Integral Nonlinearity (INL) Error  
Signal-to-Noise-and-Distortion Ratio (SINAD)  
INL refers to the deviation of each individual code from a line  
drawn from negative full scale to positive full scale. The point  
used as negative full scale occurs ½ LSB before the first code  
transition. Positive full scale is defined as a level 1½ LSB beyond  
the last code transition. The deviation is measured from the  
middle of each code to the true straight line (see Figure 53).  
SINAD is the ratio of the rms value of the actual input signal to  
the rms sum of all other spectral components below the Nyquist  
frequency, including harmonics but excluding dc. The value for  
SINAD is expressed in decibels.  
Rev. A | Page 20 of 40  
 
Data Sheet  
ADAS3022  
Reference Voltage Temperature Coefficient  
Total Harmonic Distortion (THD)  
Reference voltage temperature coefficient is derived from the  
typical shift of output voltage at 25°C on a sample of parts at the  
maximum and minimum reference output voltage (VREF) measured  
at TMIN, T (25°C), and TMAX. The value is expressed in ppm/°C as  
THD is the ratio of the rms sum of the first five harmonic  
components to the rms value of a full-scale input signal and is  
expressed in decibels.  
Spurious-Free Dynamic Range (SFDR)  
SFDR is the difference, expressed in decibels, between the rms  
amplitude of the input signal and the peak spurious signal.  
V
REF (Max)VREF (Min)  
TCVREF (ppm/°C) =  
×106  
V
REF (25°C) × (TMAX TMIN )  
where:  
REF (Max) is the maximum reference output voltage at TMIN  
T (25°C), or TMAX  
Channel-to-Channel Crosstalk  
V
,
Channel-to-channel crosstalk is a measure of the level of crosstalk  
between any channel and all other channels. The crosstalk is  
measured by applying a dc input to the channel under test and  
applying a full-scale, 10 kHz sine wave signal to all other channels.  
The crosstalk is the amount of signal that leaks into the test channel  
and is expressed in decibels.  
.
V
REF (Min) is the minimum reference output voltage at TMIN,  
T (25°C), or TMAX  
.
V
REF (25°C) is the reference output voltage at 25°C.  
T
MAX = +85°C.  
T
MIN = −40°C.  
Rev. A | Page 21 of 40  
ADAS3022  
Data Sheet  
THEORY OF OPERATION  
the ADAS3022 solution include reduced footprint and less  
complex design requirements, which also results in faster time  
to market and lower cost.  
OVERVIEW  
The ADAS3022 is the first system on a single chip that integrates  
the typical components used in a data acquisition system in one  
easy to use, programmable device. This single-chip solution is  
capable of converting up to 1,000,000 samples per second  
(1 MSPS) of aggregate throughput. The ADAS3022 features  
ADAS3022 OPERATION  
As shown in Figure 51, the ADAS3022 internal analog circuitry  
consists of a high impedance, low leakage multiplexer and a  
programmable gain instrumentation amplifier that can accept  
full-scale differential voltages of 0.64 V, 1.28 V, 2.56 V, 5.12 V,  
10.24 V, 20.48 V, and 24.576 V. The ADAS3022 can be con-  
figured to use up to eight single-ended input channels or four  
pairs of channels, that is, 125 kSPS per channel for eight channels  
or effectively 250 kSPS for four channel pairs. The device can also  
provide a relative temperature measurement using the internal  
temperature sensor. In addition, the differential auxiliary channel  
pair (AUX+ and AUX−) is provided with the specified input  
High impedance inputs  
High common-mode rejection  
8-channel, low crosstalk multiplexer (mux)  
Programmable gain instrumentation amplifier (PGIA) with  
seven selectable differential input ranges from 0.64 V to  
24.576 V  
16-bit PulSAR® ADC with no missing codes  
Internal, precision, low drift 4.096 V reference and buffer  
Temperature sensor  
range of  
V
REF . This option bypasses the mux and PGIA stages,  
Channel sequencer  
allowing direct access to the SAR ADC core.  
Reducing the number of channels or pairs increases the throughput  
rate by an amount proportional to the reciprocal of the number  
of sampled channels multiplied by the aggregate throughput:  
The ADAS3022 uses an Analog Devices patented high voltage  
iCMOS® process, allowing up to a 24.576 V differential input  
voltage range when using 15 V supplies, which makes the  
device suitable for industrial applications.  
1/(Number of Channels or Pairs) × 1000 kSPS  
The device is housed in a small, 6 mm × 6 mm, 40-lead LFCSP  
and can operate over the industrial temperature range (−40°C  
to +85°C). A typical discrete multichannel data acquisition  
system containing similar circuitry would require at least three  
times more space on the circuit board. Therefore, advantages of  
For a single channel or channel pair, the maximum throughput  
rate is 1 MSPS. For all eight channels, the AUX channel pair, and  
the temperature sensor, the throughput rate of a given channel  
decreases to 100 kSPS.  
AVDD  
DVDD  
VIO  
RESET  
PD  
VDDH  
DIFF TO  
COM  
DIFF  
PAIR  
ADAS3022  
CNV  
LOGIC/  
INTERFACE  
IN0/IN1  
BUSY  
IN0  
IN1  
CS  
IN2  
IN2/IN3  
IN4/IN5  
IN6/IN7  
IN3  
SCK  
DIN  
SDO  
PulSAR  
ADC  
PGIA  
MUX  
IN4  
IN5  
IN6  
IN7  
TEMP  
SENSOR  
COM  
AUX+  
REFIN  
BUF  
REF  
AUX–  
VSSH  
AGND  
DGND  
REFx  
Figure 51. ADAS3022 Simplified Block Diagram  
Rev. A | Page 22 of 40  
 
 
 
 
Data Sheet  
ADAS3022  
The ADAS3022 offers true high impedance inputs in a differential  
structure and rejects common-mode signals present on the inputs.  
The ADAS3022 architecture does not require any of the additional  
input buffers (op amps) that are usually required to condition  
the input signal and drive the ADC inputs when using switched  
capacitor-based successive approximation register (SAR) analog-  
to-digital converters (ADCs).  
A rising edge on CNV initiates a conversion and changes the  
state of the ADAS3022 from track to hold. In this state, the  
ADAS3022 performs analog signal conditioning. When the  
signal conditioning is complete, the ADAS3022 returns to the  
track state while at the same time quantizing the sample. This  
two-part process satisfies the necessary settling time requirement  
while achieving a fast throughput rate of up to 1 MSPS with 16-bit  
accuracy.  
The inputs are multiplexed to the PGIA using a high voltage  
multiplexer with low charge injection and very low leakage. The  
inputs can be configured for a single-ended to common point  
(COM) measurement or can be paired for up to four fully  
differential inputs with independent gain settings. This requires  
using the advanced sequencer or programming sequential  
configuration words with the desired gain for each pair. The  
digitally controlled, programmable gain is used to select one of  
seven voltage input ranges (see Table 7).  
tCYC  
tACQ  
CNV  
PHASE  
HOLD  
CONVERT/TRACK  
Figure 52. ADAS3022 System Timing  
Regardless of the type of signal (differential or single-ended,  
antiphase or nonantiphase, symmetric or asymmetric), the  
ADAS3022 converts all signals present on the enabled inputs in  
a differential fashion, like an industry-standard difference or  
instrumentation amplifier.  
When the sequencer option is used, an on-chip sequencer scans  
channels in order and offers independent input voltage ranges  
for each channel (see the Channel Sequencer Details section).  
In this mode, a single configuration word initiates the sequencer  
to scan repeatedly without the need to rewrite the register. After  
the last channel is scanned, the ADAS3022 automatically begins  
at IN0 again and repeats the sequence until a word is written to  
stop the sequencer or the asynchronous RESET is asserted.  
Additionally, if changes are made to certain configuration bits,  
the sequencer is reset to IN0.  
The conversion result is available after the conversion is complete  
and can be read back at any time before the end of the next  
conversion. Reading back data should be avoided during the  
quiet period, as indicated by BUSY being active high. Because  
the ADAS3022 has an on-board conversion clock, the serial  
clock (SCK) is not required for the conversion process. It is only  
required to present results to the user.  
The PulSAR-based ADC core is capable of converting 1 MSPS  
from a single rising edge on the convert start input (CNV). The  
conversion results are available in twos complement format and  
are presented on the serial data output (SDO). The digital interface  
TRANSFER FUNCTION  
The ideal transfer characteristics of the ADAS3022 are shown in  
Figure 53. With the inputs configured for differential input  
ranges, the data output is twos complement, as described in  
Table 6.  
CS  
uses a dedicated chip select pin ( ) to transfer data to and from  
the ADAS3022 and also provides a BUSY indicator, asynchronous  
RESET, and power-down (PD) inputs.  
The ADAS3022 on-chip reference uses an internal temperature  
compensated 2.5 V output band gap reference and a precision  
buffer amplifier to provide the 4.096 V high precision system  
reference.  
TWOS  
COMPLEMENT  
011 ... 111  
011 ... 110  
011 ... 101  
All of the bits in Table 11 are configured through a serial (SPI-  
compatible), 16-bit configuration register (CFG). Configuration  
and conversion results can be read after or during a conversion,  
or the readback option can be disabled.  
100 ... 010  
100 ... 001  
100 ... 000  
The ADAS3022 requires a minimum of three power supplies: +5 V,  
+15 V, and −15 V. On-chip low dropout regulators provide the  
necessary 2.5 V system voltages and must be decoupled externally  
via dedicated pins (ACAP, DCAP, and RCAP). The ADAS3022  
can be interfaced to any 1.8 V to 5 V digital logic family using  
the dedicated VIO logic level voltage supply (see Table 9).  
–FSR  
–FSR + 1LSB  
+FSR – 1LSB  
–FSR + 0.5LSB  
+FSR – 1.5LSB  
ANALOG INPUT  
Figure 53. ADC Ideal Transfer Function  
Rev. A | Page 23 of 40  
 
 
ADAS3022  
Data Sheet  
TYPICAL APPLICATION CONNECTION DIAGRAM  
Table 6. Output Codes and Ideal Input Voltages  
As shown in Figure 54, the ADP1613 is used in an inexpensive  
SEPIC-Ćuk topology, which is an ideal candidate for providing  
the ADAS3022 with the necessary high voltage 15 V robust  
supplies (at 20 mA) and low output ripple (3 mV maximum)  
from an external 5 V supply. The ADP1613 satisfies the  
specification requirements of the ADAS3022 with minimal  
external components while achieving greater than 86% of  
efficiency. Refer to the CN-0201 circuit note for complete  
information about this test setup.  
Differential Analog  
Inputs, VREF = 4.096 V  
Digital Output Code  
(Twos Complement, Hex)  
Description  
FSR − 1 LSB  
(32,767 × VREF)/  
(32,768 × PGIA gain)  
0x7FFF  
Midscale + 1 LSB  
VREF/(32,768 × PGIA  
0x0001  
gain)  
Midscale  
Midscale − 1 LSB  
0
0x0000  
0xFFFF  
−(VREF/(32,768 × PGIA  
gain))  
−(32,767 × VREF)/  
−FSR + 1 LSB  
−FSR  
0x8001  
0x8000  
(32,768 × PGIA gain)  
−VREF × PGIA gain  
D2  
C
4.7µF  
3
OUT  
+
L2  
47µH  
C2  
+
1µF  
1.78Ω  
FILT  
L1  
47µH  
R
+5V  
D1  
V
= +5V  
IN  
L3  
1µF  
+15V  
+
C
1µF  
IN  
C1  
1µF  
+
+
R
0
C
1
C
2
B
OUT  
OUT  
1Ω  
1µF  
2.2µF  
VDDH  
AVDD DVDD  
VIO  
RESET PD  
R
EN  
ENABLE  
DIFF DIFF  
PAIR COM  
ADAS3022  
CNV  
50kΩ  
R 1  
S
0Ω  
BUSY  
LOGIC/  
IN0  
IN0/IN1  
IN1  
INTERFACE  
ADP1613  
CS  
IN2  
IN2/IN3  
IN3  
COMP  
SS  
SCK  
DIN  
SDO  
+
1
12nF  
+
C
C
C
10pF  
2
C
PulSAR  
ADC  
PGIA  
IN4  
IN4/IN5  
IN5  
MUX  
FB  
FREQ  
VIN  
R
1
C
IN6  
IN6/IN7  
IN7  
EN  
100kΩ  
REFIN  
BUF  
REF  
TEMP  
SENSOR  
COM  
GND  
SW  
AUX+  
+
+
C 5  
V
R 2  
S
C
SS  
AUX–  
1µF  
DNI  
1µF  
Z1  
+5V  
ADR434  
VSSH  
–15V  
AGND DGND  
REFx  
DNI  
+5V  
+
4.096V  
RF2  
4.22kΩ  
RF1B  
47.5kΩ  
AD8031  
Figure 54. Complete 5 V, Single-Supply, 8-Channel Multiplexed Data Acquisition System with PGIA  
Rev. A | Page 24 of 40  
 
 
 
Data Sheet  
ADAS3022  
Note that because the ADAS3022 can use any input type, such  
as bipolar differential (antiphase or nonantiphase), bipolar single  
ended, or pseudo bipolar, setting the PGIA is important to  
make full use of the allowable input span.  
ANALOG INPUTS  
Input Structure  
The ADAS3022 uses a differential input structure between  
IN[7:0] and COM or between IN[7:0]+ and IN[7:0]− of a  
channel pair. The COM input is sampled identically such that  
the same voltages can be present on inputs IN[7:0]. Therefore,  
the selection of paired channels or all channels referenced to  
one common point is available. Because all inputs are sampled  
differentially, the ADAS3022 offers true high common-mode  
rejection, whereas a discrete system would require the use of  
additional instrumentation or a difference amplifier.  
Table 7 describes each differential input range and the  
corresponding LSB size, PGIA bits settings, and PGIA gain.  
Table 7. Differential Input Ranges, LSB Size, and PGIA  
Settings  
Differential Input Ranges,  
INx+ − INx(V)  
PGIA Gain  
LSB (μV) PGIA Bits (V/V)  
24.5ꢀ7  
20.4ꢁ  
80.24  
5.82  
2.57  
8.2ꢁ  
ꢀꢁ8.25  
725  
000  
888  
008  
080  
088  
800  
808  
0.87  
0.2  
0.4  
0.ꢁ  
8.7  
ꢂ.2  
7.4  
Figure 55 shows an equivalent circuit of the analog inputs. The  
internal diodes provide ESD protection for the analog inputs  
(IN[7:0] and COM) from the high voltage supplies (VDDH and  
VSSH). Care must be taken to ensure that the analog input  
signal does not exceed the supply rails by more than 0.3 V  
because this can cause the diodes to become forward-biased and  
to start conducting current. Note that if the auxiliary input pair  
(AUX±) is used, the diodes provide ESD protection from only the  
lower voltage AVDD (5 V) supply and the system analog ground  
because these inputs are connected directly to the internal SAR  
ADC circuitry.  
ꢂ82.5  
857.ꢂ  
ꢀꢁ.8ꢂ  
ꢂ3.07  
83.5ꢂ  
0.74  
Common-Mode Operating Range  
The differential input common-mode voltage (VCM) range  
changes according to the maximum input range selected and  
the high voltage power supplies (VDDH and VSSH). Note that  
the specified operating input voltage of any input pin (see the  
Specifications section) requires 2.5 V of headroom from the  
VDDH and VSSH supplies; therefore,  
VDDH  
IN[7:0]  
OR COM  
MUX  
PGIA  
C
PIN  
(VSSH + 2.5 V) ≤ INx/COM ≤ (VDDH − 2.5 V)  
VSSH  
This section provides some examples of setting the PGIA for  
various input signals. Note that the ADAS3022 always calculates  
the difference between the IN+ and IN− signals.  
AVDD  
AUX+  
OR AUX–  
C
PIN  
Fully Differential, Antiphase Signals with a  
Zero Common Mode  
AGND  
For a pair of 20.4ꢁ V p-p differential antiphase signals with a  
zero common mode, the maximum differential voltage across  
the inputs is 20.4ꢁ V, and the PGIA gain configuration should  
be set to ±±±.  
Figure 55. Equivalent Analog Input Circuit  
Voltages beyond the absolute maximum ratings may cause  
permanent damage to the ADAS3022 (see Table 4).  
INx+  
INx+  
+10.24V  
Programmable Gain  
20.48V p-p  
The ADAS3022 incorporates a programmable gain instru-  
mentation amplifier with seven selectable ranges (±0.ꢀ4 V,  
±±.2ꢁ V, ±2.5ꢀ V, ±5.±2 V, ±±0.24 V, ±20.4ꢁ V, and ±24.57ꢀ V),  
enabling the use of almost any direct sensor interface. The PGIA  
settings are specified in terms of the maximum absolute differential  
input voltage across a pair of inputs (for example, INx+ to INx−  
or INx+ to COM). The power-on and default conditions are  
preset to the ±20.4ꢁ V (PGIA = ±±±) input range.  
ADAS3022  
–10.24V  
20.48V p-p  
INx–  
INx–  
Figure 56. Differential, Antiphase Inputs with a Zero Common Mode  
Rev. A | Page 25 of 40  
 
 
 
 
 
ADAS3022  
Data Sheet  
for single-ended signals, if possible, is to remove as much dc  
offset as possible between INx+ and INx− to produce a bipolar  
input voltage that is symmetric around the ground sense. In this  
example, the differential voltage across the inputs is never greater  
than 0.64 V, and the PGIA gain configuration is set to 101 for  
the 1.28 V p-p range. This scenario uses all of the codes  
available for the transfer function, making full use of the  
allowable differential input range.  
Fully Differential, Antiphase Signals with a  
Nonzero Common Mode  
For a pair of 5.12 V p-p differential antiphase signals with a  
nonzero common mode (dc common-mode voltage of 7 V in  
this example), the maximum differential voltage across the  
inputs is ±5.12 V (dc common-mode voltage is rejected), and  
the PGIA gain configuration should be set to 010.  
INx+  
INx+  
INx+  
5.12V p-p  
+0.64V  
INx–  
INx+  
ADAS3022  
V
= 7V  
0V  
CM  
1.28V p-p  
ADAS3022  
V
INx–  
CM  
5.12V p-p  
–0.64V  
INx–  
INx–  
Figure 57. Differential, Antiphase Inputs with a Nonzero Common Mode  
Figure 60. Better Single-Ended Configuration—Uses All Codes  
Differential, Nonantiphase Signals with a  
Zero Common Mode  
Notice that the voltages in this example are not integer values  
due to the 4.096 V reference and the PGIA scaling ratios.  
For a pair of 10.24 V p-p differential nonantiphase signals with  
a zero common mode, the maximum differential voltage across  
the inputs is ±10.24 V, and the PGIA gain configuration should  
be set to 001.  
Multiplexer  
The ADAS3022 uses a high voltage, high performance, low  
charge injection multiplexer and a total of nine inputs (IN[7:0]  
and COM). Using the INx and COM bits of the configuration  
register, the ADAS3022 is configurable for differential inputs  
between any of the eight input channels (IN[7:0]) and COM or  
for up to four input pairs. Figure 61 shows various methods for  
configuring the analog inputs for the type of channel (single or  
paired). Refer to the Configuration Register section for more  
information.  
INx+  
INx+  
10.24V p-p  
10.24V p-p  
+5.12V  
0V  
ADAS3022  
–5.12V  
INx–  
INx–  
Figure 58. Differential, Nonantiphase Inputs with a Zero Common Mode  
Single-Ended Signals with a Nonzero DC Offset  
(Asymmetrical)  
The analog inputs can be configured as follows:  
When a 12 V p-p signal with a 6 V dc level-shift is connected to  
one input (INx+) and the dc ground sense of the signal is  
connected to INx− or COM, the PGIA gain configuration is set  
to 000 for the 24.576 V range because the maximum differential  
voltage across the inputs is 12 V p-p and only half the codes  
available for the transfer function are used.  
Figure 61A: IN[7:0] referenced to a system ground.  
Figure 61B: IN[7:0] with a common reference point.  
Figure 61C: IN[7:0] differential pairs. For pairs, COM = 0.  
The positive channel is configured with INx. If INx is even,  
then IN0, IN2, IN4, and IN6 are used. If INx is odd, then  
IN1, IN3, IN5, and IN7 are used, as indicated by the channels  
with parentheses in Figure 61C. For example, for the IN0/IN1  
pair with the positive channel on IN0, INx = 0002. For the  
IN4/IN5 pair with the positive channel on IN5, INx = 1012.  
Note that when the channel sequencer is used, as detailed in  
the Channel Sequencer Details section, the positive channels  
are always IN0, IN2, IN4, and IN6.  
INx+  
INx+  
+12V  
12V p-p  
V
OFF  
0V  
ADAS3022  
V
OFF  
INx–  
INx–  
Figure 59. Typical Single-Ended Unipolar Input—Uses Only Half the Codes  
Figure 61D: inputs configured in a combination of any of  
the preceding configurations (showing that the ADAS3022  
can be configured dynamically).  
Single-Ended Signals with a 0 V DC Offset (Symmetrical)  
Compared with the example in the Single-Ended Signals with a  
Nonzero DC Offset (Asymmetrical) section, a better solution  
Rev. A | Page 26 of 40  
 
 
 
 
Data Sheet  
ADAS3022  
Driver Amplifier Choice  
IN0+  
IN1+  
IN2+  
IN3+  
IN4+  
IN5+  
IN6+  
IN7+  
IN0+  
IN1+  
IN2+  
IN3+  
IN4+  
IN5+  
IN6+  
IN7+  
COM–  
IN0  
IN1  
IN2  
IN3  
IN4  
IN5  
IN6  
IN7  
COM  
IN0  
IN1  
IN2  
IN3  
IN4  
IN5  
IN6  
IN7  
COM  
For systems that cannot drive AUX directly, a suitable op amp  
buffer should be used to preserve the ADAS3022 performance.  
The driver amplifier must meet the following requirements:  
The noise generated by the driver amplifier must be kept as  
low as possible to preserve the SNR and the transition noise  
performance of the ADAS3022. The noise from the  
amplifier is filtered by the ADAS3022 analog input circuit  
or by an external filter, if one is used. Because the typical  
noise of the ADAS3022s SAR ADC core is 35 µV rms (VREF  
4.096 V), the SNR degradation due to the amplifier is  
=
A—8 CHANNELS,  
SINGLE-ENDED  
B—8 CHANNELS,  
COMMON REFERENCE  
IN0+ (–)  
IN0– (+)  
IN1+ (–)  
IN1– (+)  
IN2+ (–)  
IN2– (+)  
IN3+ (–)  
IN3– (+)  
IN0+ (–)  
IN0  
IN1  
IN2  
IN3  
IN4  
IN5  
IN6  
IN7  
COM  
IN0  
IN1  
IN2  
IN3  
IN4  
IN5  
IN6  
IN7  
COM  
IN0– (+)  
IN1+ (–)  
IN1– (+)  
35  
SNRLOSS = 20log  
π
2
352 + f3dB (NeN )2  
IN2+  
IN3+  
where:  
−3dB is the input bandwidth (8 MHz) of the ADAS3022s SAR  
ADC core expressed in megahertz or the cutoff frequency of  
f
IN4+  
IN5+  
an input filter, if one is used.  
COM–  
N is the noise gain of the amplifier (for example, 1 in buffer  
configuration).  
eN is the equivalent input noise voltage of the op amp  
expressed in nV/√Hz.  
C—4 CHANNELS,  
DIFFERENTIAL  
D—COMBINATION  
Figure 61. Multiplexed Analog Input Configurations  
For ac applications, the driver should have a THD performance  
commensurate with the ADAS3022.  
Channel Sequencer  
The ADAS3022 includes a channel sequencer that is useful for  
scanning channels in a repeated fashion. Refer to the Channel  
Sequencer Details section for more information.  
The analog input circuit must settle a full-scale step onto  
the capacitor array at a 16-bit level (0.0015%). In amplifier  
data sheets, settling at 0.1% to 0.01% is more commonly  
specified. This may differ significantly from the settling  
time at a 16-bit level and should be verified prior to driver  
selection.  
Auxiliary Input Channel  
The ADAS3022 includes an auxiliary input channel pair (AUX+  
and AUX−) that bypasses the mux and PGIA stages, allowing direct  
access to the SAR ADC core for applications where the additional  
dedicated channel pair is required. As detailed previously, the  
inputs are protected only from AVDD and AGND because the high  
voltage supplies are used for the mux and PGIA stages but not the  
lower voltage ADC core.  
Table 8. Recommended Driver Amplifiers  
Amplifier Typical Application  
ADA4841-1, ADA4841-2 Very low noise, small, and low power  
ADA4897-1, ADA4897-2 Very low noise, low and high frequencies  
AD8655  
AD8021, AD8022  
OP184  
5 V single supply, low noise  
When the source impedance of the driving circuit is low, the  
AUX inputs can be driven directly. Large source impedances  
significantly affect the ac performance, especially THD. The dc  
performance parameters are less sensitive to the input impedance.  
The maximum source impedance depends on the amount of  
THD that can be tolerated. The THD degrades as a function of  
the source impedance and the maximum input frequency.  
Very low noise and high frequency  
Low power, low noise, and low frequency  
5 V single supply, low power  
AD8605, AD8615  
Rev. A | Page 27 of 40  
 
 
ADAS3022  
Data Sheet  
the main system reference. With REFIN = 2.5 V, REF1 and REF2  
output 4.096 V, which serves as the main system reference.  
VOLTAGE REFERENCE OUTPUT/INPUT  
The ADAS3022 allows the choice of an internal reference or an  
external reference using the on-chip buffer/amplifier, or an  
external reference.  
For this configuration, connect the external source as shown  
in Figure 63. Any type of 2.5 V reference, including those with  
low power, low drift, and a small package, can be used in this  
configuration because the internal buffer handles the dynamics  
of the ADAS3022 reference.  
The internal reference of the ADAS3022 provides excellent  
performance and can be used in almost all applications. To set  
the reference selection mode, use the internal reference enable bit  
(REFEN) and the REFIN pin as described in this section. REF1  
and REF2 must be tied together externally.  
0.1µ  
F
0.1µF  
0.1µF  
REFERENCE  
SOURCE = 2.5V  
10µF  
10µ  
F
10µF  
Internal Reference  
REFN  
REF2 REFN  
REF1 REFN REFIN  
The precision internal reference is factory trimmed and is  
suitable for most applications.  
RCAP  
1µF  
BAND  
GAP  
ADAS3022  
Setting the REFEN bit in the CFG register to 1 (default) enables  
the internal reference and produces 4.096 V on the REF1 and  
REF2 pins; this 4.096 V output serves as the main system  
reference. The unbuffered 2.5 V (typical) band gap voltage is  
output on the REFIN pin, which requires an external parallel  
decoupling using 10 µF and 0.1 µF capacitors to reduce the  
noise on the output. Because the current output of REFIN is  
limited, it can be used as a source if followed by a suitable buffer,  
such as the AD8031. Note that excessive loading of the REFIN  
output will also lower the 4.096 V system reference because the  
internal amplifier uses a fixed gain.  
RGND  
Figure 63. External Reference Using Internal Buffer  
External Reference  
For applications that require a precise, low drift 4.096 V reference,  
an external reference can also be used.  
This option requires disabling the internal buffer by setting  
REFEN to 0 and driving or connecting REFIN to AGND; therefore,  
both hardware and software control are necessary. Attempting  
to drive the REF1 and REF2 pins prior to disabling the internal  
buffer can cause source/sink contention in the driving amplifiers.  
The internal reference output is trimmed to the targeted value  
of 4.096 V with an initial accuracy of 8 mV. The reference is  
also temperature compensated to provide a typical drift of  
5 ppm/°C.  
Connect the precision 4.096 V reference, which serves as the  
main system reference, through a low impedance buffer (such as  
the AD8031 or the AD8605) to REF1 and REF2 as shown in  
Figure 64. Recommended references include the ADR434,  
ADR444, and ADR4540.  
When the internal reference is used, the ADAS3022 should be  
decoupled as shown in Figure 62. Note that both REF1 and  
REF2 connections are required, along with suitable decoupling  
on the REFIN output and the RCAP internally regulated supply.  
REFERENCE  
SOURCE = 4.096V  
0.1µF  
0.1µF  
0.1µ  
F
0.1µ  
F
0.1µF  
10µF  
10µF  
10µF  
10µ  
F
10µF  
REFN  
REF2 REFN REF1  
REFIN  
REFN  
REF2 REFN  
REF1 REFN REFIN  
RCAP  
1µF  
BAND  
GAP  
RCA  
1µF  
P
ADAS3022  
BAND  
GAP  
ADAS3022  
RGND  
RGND  
Figure 64. External Reference  
Figure 62. 4.096 V Internal Reference Connection  
If an op amp is used as the external reference source, take note  
of any concerns regarding driving capacitive loads. Capacitive  
loading for op amps usually refers to the ability of the amplifier  
to remain marginally stable in ac applications but can also play  
a role in dc applications, such as a reference source. Keep in  
mind that the reference source sees the dynamics of the bit  
decision process on the reference pins and further analysis  
beyond the scope of this data sheet may be required.  
External Reference and Internal Buffer  
The external reference and internal buffer are useful when a com-  
mon system reference is used or if improved drift performance  
is required.  
Setting REFEN to 0 disables the internal band gap reference,  
allowing the user to provide an external voltage reference (2.5 V  
typical) to the REFIN pin. The internal buffer remains enabled,  
thus reducing the need for an external buffer amplifier to generate  
Rev. A | Page 28 of 40  
 
 
 
 
Data Sheet  
ADAS3022  
POWER SUPPLY  
Reference Decoupling  
The ADAS3022 uses five supplies: AVDD, DVDD, VIO, VDDH,  
and VSSH (see Table 9). Note that ACAP, DCAP, and RCAP are  
included in Table 9 for informational purposes only because these  
supplies are outputs of the on-chip supply regulators. Refer to  
UG-484 for more information about how these supplies are  
generated on the EVAL-ADAS3022EDZ.  
With any of the reference topologies described in the Voltage  
Reference Input/Output section, the REF1 and REF2 reference  
pins of the ADAS3022 have dynamic impedances and require  
sufficient decoupling, regardless of whether the pins are used as  
inputs or outputs. This decoupling usually consists of a low ESR  
capacitor connected to each REF1 and REF2 and to the accom-  
panying REFN return paths. Using X5R, 1206 size ceramic chip  
capacitors is recommended for decoupling in all the reference  
topologies described in the Voltage Reference Input/Output section.  
Table 9. Power Supplies  
Name  
AVDD  
DVDD  
Function  
Required  
Analog 5 V core  
Digital 5 V core  
Yes  
The placement of the reference decoupling capacitors plays an  
important role in the system performance. Mount the decoupling  
capacitors on the same side as the ADAS3022, close to the REF1  
and REF2 pins, with thick PCB traces. Route the return paths to the  
REFN inputs, which are in turn connected to the analog ground  
plane of the system. The resistance of the return path to ground  
should be minimized by using as many through vias as possible  
when it is necessary to connect to an internal PCB layer.  
Yes, or can connect to  
AVDD  
VIO  
Digital input/output  
Yes, and can connect  
to DVDD (for 5 V  
level)  
VDDH  
VSSH  
ACAP  
DCAP  
RCAP  
Positive high voltage  
Negative high voltage  
Analog 2.5 V core  
Digital 2.5 V core  
Yes, +15 V typ  
Yes, −15 V typ  
No, on chip  
No, on chip  
No, on chip  
Analog 2.5 V core  
The REFN and RGND inputs should be connected with the  
shortest distance to the analog ground plane of the system,  
preferably adjacent to the solder pads, using several vias. One  
common mistake is to route these traces to an individual trace  
that connects to the ground of the system. This can introduce  
noise, which may adversely affect LSB sensitivity. To prevent  
such noise, it is highly recommended to use PCBs with multiple  
layers, including ground planes, rather than using single- or  
double-sided boards. Refer to UG-484 for more information  
about the PCB layout of the EVAL-ADAS3022EDZ.  
Core Supplies  
AVDD and DVDD supply the ADAS3022 analog and digital  
cores, respectively. Sufficient decoupling of these supplies is  
required, consisting of at least a 10 μF capacitor and a 100 nF  
capacitor on each supply. The 100 nF capacitors should be  
placed as close as possible to the ADAS3022. To reduce the  
number of supplies needed, DVDD can be supplied from the  
analog supply by connecting a simple RC filter between AVDD  
and DVDD, as shown in Figure 65.  
For applications that use multiple ADAS3022 devices or other  
PulSAR ADCs, it is more effective to use the internal reference  
buffer to buffer the external reference voltage, thus reducing  
SAR conversion crosstalk.  
VIO is the variable digital input/output supply and can be  
directly interfaced to any logic between 1.8 V and 5 V (DVDD  
supply maximum). To reduce the supplies needed, VIO can  
alternatively be connected to DVDD when DVDD is supplied  
from the analog supply through an RC filter. The recommended  
low dropout regulators are ADP3334, ADP1715, and ADP7102/  
ADP7104 for the AVDD, DVDD, and VIO supplies.  
The voltage reference temperature coefficient (TC) directly  
affects the full-scale accuracy of the system; therefore, in  
applications where full-scale accuracy is crucial, care must be  
taken with the TC. For example, a 15 ppm/°C TC of the  
reference changes the full-scale accuracy by 1 LSB/°C.  
20  
ANALOG  
SUPPLY  
+5V  
+5V DIGITAL  
SUPPLY  
10µF  
100nF  
100nF  
10µF  
1.8V TO 5V  
DIGITAL I/O  
SUPPLY  
AVDD AGND DVDD DGND  
+15V  
10µF  
VDDH  
VIO  
10µF  
100nF  
100nF  
ADAS3022  
10µF  
–15V  
100nF  
DGND  
VSSH  
Figure 65. ADAS3022 Supply Connections  
Rev. A | Page 29 of 40  
 
 
 
ADAS3022  
Data Sheet  
High Voltage Supplies  
be allowed the specified settling time. Returning PD low also  
resets the ADAS3022 digital core, including the CFG register, to  
its default state. Therefore, the desired CFG must be rewritten  
to the device and two dummy conversions must be completed  
before the device operation is restored to the configuration  
programmed prior to PD assertion.  
The high voltage bipolar supplies (VDDH and VSSH) are  
required and must be at least 2.5 V larger than the maximum  
input. For example, the supplies should be 15 V for headroom  
in the 24.576 V differential input range. Sufficient decoupling  
of these supplies is also required, consisting of at least a 10 μF  
capacitor and a 100 nF capacitor on each supply.  
CONVERSION MODES  
Power Dissipation Modes  
The ADAS3022 offers two conversion modes to accommodate  
varying applications. The mode is set with the conversion mode  
select bit (CMS, Bit 1 of the CFG register).  
The ADAS3022 offers two power dissipation modes: fully  
operational mode and power-down mode.  
Warp Mode (CMS = 0)  
Fully Operational Mode  
Setting CMS to 0 is useful when an aggregate throughput rate of  
1 MSPS is required. However, in this mode, the maximum time  
between conversions is restricted. If this maximum period is  
exceeded, the conversion result may be corrupted. Therefore,  
this mode is more suitable for continually sampled applications.  
In fully operational mode, the ADAS3022 can perform  
conversions as soon as all internal bias currents are established.  
Power-Down Mode  
To minimize the operating currents of the device when it is idle,  
place the device in full power-down mode by bringing the PD  
input high. This places the ADAS3022 into a deep sleep mode, in  
which CNV activity is ignored and the digital interface is inactive.  
Refer to the Reset and Power-Down (PD) Inputs section for  
timing details. In deep sleep mode, the internal regulators  
(ACAP, RCAP, and DCAP) and the voltage reference are also  
powered down. To reestablish operation, return PD low. Note  
that before the device can operate at the specified performance, the  
reference voltage must charge up the external reservoir  
capacitor(s) and  
Normal Mode (CMS = 1, Default)  
Setting CMS to 1 is useful for all applications with a maximum  
aggregate throughput of 900 kSPS. In this mode, there is no  
restriction in terms of the maximum time between conversions.  
This mode is the default condition from the assertion of an  
asynchronous RESET. The main difference between normal  
mode and warp mode is the BUSY time; tQUIET is slightly longer  
in normal mode than it is in warp mode.  
Rev. A | Page 30 of 40  
 
 
Data Sheet  
ADAS3022  
DIGITAL INTERFACE  
BUSY Falling Edge—End of a Conversion (EOC)  
The ADAS3022 digital interface consists of asynchronous  
inputs, a busy indicator, and a 4-wire serial interface for  
conversion result readback and configuration register  
programming.  
The EOC event is indicated by BUSY returning low and can be  
used as a host interrupt. In addition, the EOC gates data access  
to and from the ADAS3022. If the current conversion result is  
not read prior to the following EOC event, the data is lost.  
Furthermore, if the CFG update is not completed prior to EOC, it  
is discarded and the current configuration is applied to future con-  
versions. This pipeline ensures that the ADAS3022 has  
sufficient time to acquire the next sample to the specified 16-bit  
accuracy.  
This interface uses the three asynchronous signals (CNV,  
RESET, and PD) and a 4-wire serial interface composed of  
CS  
,
CS  
SDO, SCK, and DIN.  
applications.  
can also be tied to CNV for some  
Conversion results are available on the serial data output pin  
(SDO), and the 16-bit configuration word (CFG) is program-  
med on the serial data input pin (DIN). This register controls  
Conversion Timing  
A detailed timing diagram of the conversion process is shown  
in Figure 66.  
settings such as the channel to be converted, the programmable  
gain setting, and the reference choice (see the Configuration  
Register section for more information).  
tCYC  
SOC  
(n)  
EOC  
(n)  
SOC  
(n + 1)  
CONVERSION CONTROL  
tCONV  
tCBD  
tDDC  
Conversions are initiated by the CNV input. The ADAS3022 is  
fully asynchronous and can perform conversions at any frequency  
from dc up to 1 MHz, depending on the conversion mode.  
tQUIET  
tDDCA  
tDAC  
tAD  
tCH  
CNV  
BUSY  
SAFE  
QUIET  
CNV Rising Edge—Start of a Conversion (SOC)  
CONVER-  
SION  
(n + 1)  
(n)  
A rising edge on CNV changes the state of the ADAS3022 from  
track mode to hold mode and is all that is necessary to initiate a  
conversion. All conversion timing clocks are internally generated.  
After a conversion is initiated, the ADAS3022 ignores other  
activity on the CNV line (governed by the throughput rate) until  
the end of the conversion; the conversion can only be aborted  
by the power-down (PD) or RESET inputs.  
ACQUI-  
SITION  
(n)  
XXX  
tCCS  
(n + 1)  
XXX  
tACQ  
tCCS  
CS  
SDO  
DIN  
DATA  
(n – 1)  
DATA  
(n)  
CFG  
CFG  
x
x
x
(n + 2)  
(n + 3)  
When the ADAS3022 is performing a conversion and the BUSY  
output is driven high, the ADAS3022 uses a unique 2-phase  
conversion process to allow for safe data access and quiet times.  
Figure 66. Basic Conversion Timing  
Register Pipeline  
CS  
The CNV signal is decoupled from the  
pin, allowing  
To ensure that all CFG updates are applied during a known safe  
instant to the various circuit elements, the asynchronous data  
transfer is synchronized to the ADAS3022 timing engine using  
the EOC event. This synchronization introduces an inherent delay  
between updating the CFG register setting and the application  
of the configuration to a conversion. This pipeline from the end  
of the current conversion (n) consists of a two-deep delay (shown  
as (n + 2) in Figure 66) before the CFG setting takes effect. This  
means that two SOC and EOC events must elapse before the  
setting (that is, new channel, gain, and so on) takes effect. Note  
that the nomenclature (n), (n + 1), and so on is used in the  
remainder of the following digital sections for simplicity.  
multiple ADAS3022 devices to be controlled by the same  
processor. For applications where SNR is critical, the CNV  
source should have very low jitter. This can be achieved by  
using a dedicated oscillator or by clocking CNV with a high  
frequency, low jitter clock. For applications where jitter is more  
CS  
tolerable or a single device is in use, CNV can be tied to . For  
more information about sample clock jitter and aperture delay,  
refer to the MT-007 Tutorial, Aperture Time, Aperture Jitter,  
Aperture Delay Time—Removing the Confusion.  
Although CNV is a digital signal, it should be designed to  
ensure fast, clean edges with minimal overshoot, undershoot,  
and ringing. The CNV trace should be shielded by connecting a  
trace to ground, and a low value (such as 50 Ω) serial resistor  
termination should be added close to the output of the component  
that drives this line. In addition, care should be taken to avoid  
digital activity close to the sampling instant because such activity  
may result in degraded SNR performance.  
There is no pipeline after the end of a conversion, however,  
before data can be read back.  
Rev. A | Page 31 of 40  
 
 
 
ADAS3022  
Data Sheet  
RESET AND POWER-DOWN (PD) INPUTS  
Note that in Figure 67 and Figure 68, SCK is shown idling high.  
SCK can idle high or low, requiring that the system developer  
design an interface that suits setup and hold times for both SDO  
and DIN.  
The asynchronous RESET and PD inputs can be used to reset  
and power down the ADAS3022, respectively. Timing details  
are shown in Figure 67.  
tSCK  
A rising edge on RESET or PD aborts the conversion process and  
tSCKH  
tDIS  
tSCKL  
CS  
places SDO into high impedance, regardless of the  
level. Note  
CS  
that RESET has a minimum pulse width (active high) time for  
setting the ADAS3022 into the reset state. See the Configuration  
Register section for the default CFG setting when the ADAS3022  
returns from the reset state. If the default setting is used after  
RESET is deasserted (Logic 0), a period equal to the acquisition  
time (tACQ) must elapse before CNV can be asserted for the  
conversion result to be valid. If a conversion is initiated, the  
result will be corrupted. In addition, the output data from the  
previous conversion is cleared upon a reset. Attempting to  
access the data result prior to initiating a new conversion results  
in an invalid result.  
SCK  
tSDOH  
tEN  
SDO  
tSDOD  
(MISO)  
DIN  
(MOSI)  
tDINS  
tDINH  
Figure 68. Serial Timing  
CPHA  
The clock phase select bit (CPHA, Bit 0) sets the first bit of the  
conversion result on SDO after the end of a conversion (see  
Figure 69).  
When the device returns from power-down mode or from a reset  
and the default CFG is not used, there is no tACQ requirement;  
the first two conversions from power-up are undefined/invalid  
because the two-deep delay pipeline requirement must be satisfied  
to reconfigure the device to the desired setting.  
CS  
Setting CPHA to 0 outputs the MSB when  
is asserted. Sub-  
sequent SCK falling edges clock out bits in an MSB − 1, MSB − 2,  
and so on fashion. This mode is useful for hosts limited to 16 clock  
edges where the first falling (or rising) edge can be used to latch  
the data.  
tACQ  
SEE NOTE  
tRH  
CNV  
n – 1  
n
RESET/  
PD  
CS  
Setting CPHA to 1 outputs the MSB not only when is asserted  
n – 1  
BUSY  
but also after the first SCK falling edge. Subsequent SCK falling  
edges clock out bits in an MSB − 1, MSB − 2, and so on fashion.  
This mode can be useful for sign extension applications.  
tEN  
tDIS  
CS  
n – 2  
n + 1  
n – 1  
x
SDO  
CFG  
CS  
x
x
n + 2  
x
2
15  
16  
1
SEE NOTE  
SCK  
NOTES  
1. WHEN THE PART IS RELEASED FROM RESET, tACQ MUST BE MET FOR  
CONVERSION n IF USING THE DEFAULT CFG SETTING FOR CHANNEL IN0.  
WHEN THE PART IS RELEASED FROM POWER-DOWN, tACQ IS NOT REQUIRED,  
AND THE FIRST TWO CONVERSIONS, n AND n + 1, ARE UNDEFINED.  
MSB MSB – 1 MSB – 2  
LSB + 1  
LSB + 2  
LSB  
MSB  
LSB  
SDO  
CPHA = 0  
SDO  
CPHA = 1  
MSB  
MSB  
MSB – 1  
LSB + 1  
Figure 67. RESET and PD Timing  
Figure 69. CPHA Details  
SERIAL DATA INTERFACE  
Sampling on the SCK Falling Edge  
The ADAS3022 uses a simple 4-wire interface and is compatible  
with FPGAs, DSPs, and common serial interfaces, such as SPI,  
QSPI, and MICROWIRE™. The interface uses the , SCK,  
SDO, and DIN signals. Timing details for the serial interface are  
shown in Figure 68. SDO is activated when  
conversion result is output on SDO and is updated on SCK  
falling edges. Simultaneously, the 16-bit CFG word is updated, if  
desired, on the serial data input (DIN). The state of the clock  
phase select bit (CPHA, Bit 0) determines whether the MSB is  
output again on the first clock or whether the MSB − 1 bit is  
output when SDO is activated after the EOC.  
To achieve the fastest data transfer rate, the host should sample  
data on the SCK falling edge, as long as there is a sufficient hold  
time of ≤tSDOH (see Figure 68). When using this method, data  
transfers should occur during the safe conversion time (tDDC).  
Because this time is fixed, extending data reading or writing into  
the quiet conversion phase (tQUIET) may cause data corruption.  
However, for systems that need slightly more time, tDDCA (data  
during conversion additional) can be used.  
CS  
CS  
is asserted. The  
Rev. A | Page 32 of 40  
 
 
 
 
 
 
Data Sheet  
ADAS3022  
SOC  
EOC  
tDDCA  
Sampling on the SCK Rising Edge (Alternate Edge)  
tAD  
tDDC  
SPI or other alternate edge transfers typically require more time  
to access data because the total data transfer time of these slower  
hosts can be >tDDC. If this is the case, the time from tQUIET to the next  
CNV rising edge, which is known as the data access time after  
conversion (tDAC) and is determined by the user, must be  
adjusted by lowering the throughput rate (CNV frequency),  
thus providing the necessary time. If this does not allow enough  
time, the data access can be broken up so that some data access  
occurs during this time followed by the remainder of data  
access occurring during the next tDDC and tDDCA times.  
tQUIET  
CNV  
BUSY  
CS  
n
n + 1  
n + 2  
n + 1  
n
n – 1  
n + 2  
n
SDO  
DIN  
n + 3  
SCK  
Figure 70. Data Access During Conversion  
CFG Readback  
Data Access After/Spanning Conversion—Host Determined  
Throughput  
The CFG result associated with the current conversion can be read  
back with an additional 16 SCK burst following the conversion  
result (see Figure 69). After the LSB of the conversion result is  
clocked out, the MSB of the CFG associated with that conversion  
follows. Subsequent SCK falling edges repeat the conversion  
result and CFG word. For example, when CPHA is 0, the MSB  
of the conversion result is output on the 32nd falling edge.  
For hosts that do not have the 34 MHz or 25 MHz SCK rates  
available, the maximum throughput rate cannot be achieved  
because the data access time after conversion, tDAC, must be  
increased to allow more time to access data. In this case, there  
are three methods to access data:  
The first method is to adjust tDAC for 17 SCK edges (worst  
CS  
GENERAL CONSIDERATIONS  
case) and the additional  
to CNV setup and hold times.  
Because the time to access data is somewhat restricted, the  
following guidelines are useful in determining the ADAS3022  
throughput, or CNV frequency, and the serial interface details.  
Note that in Figure 70 to Figure 72, tAD is for reference purposes  
only and denotes a time without digital activity because such  
activity should not occur prior to or just after sampling.  
In this case, all data access occurs during tDAC. This is the  
only method that can be used when using a slow host that  
cannot break up data into bytes or other partial data bursts.  
A second method is to break up the data into bursts that  
can transfer part of the data during tDAC of the current  
conversion and the rest of the data during tDDC of the next  
Data Access During Conversion—Maximum Throughput  
CS  
conversion. Note that  
can stay low throughout the CNV  
rising phase; however, serial clock activity should pause  
while the input is being sampled.  
A third method is to use the second method along with the  
additional tDDCA, again noting that digital activity must cease  
after this time to prevent the current conversion from  
becoming corrupted.  
The maximum throughput rate per channel is determined  
mainly by the maximum SCK period of the host. When using  
the maximum throughput rate of 1 MSPS, the ADAS3022 has  
an almost symmetric period for both safe data and quiet times  
(~500 ns each; see Figure 70). Consequently, tDDC is basically  
fixed and only provides the host ~500 ns to access data. Note  
that in Figure 70, tAD is for reference purposes only and denotes  
a time without digital activity because such activity should not  
occur during the sampling edge. For 17 SCK edges (worst case), the  
minimum SCK frequency required to achieve a 1 MSPS (1 µs  
between CNV rising) aggregate throughput rate is  
In any of these methods, if the time between conversions (tCYC  
)
is exceeded for the fastest possible throughput mode (CMS = 0),  
the conversion results will be inaccurate. If this is the case, the  
fully asynchronous mode (CMS = 1) must be selected (see the  
Conversion Modes section for details).  
17  
f
34 MHz  
SCK  
Figure 71 shows a basic timing diagram for all three methods.  
For conversion (n), the data is read back after the end of a  
conversion (n), with the remainder of data read into the next  
(n + 1) conversion.  
tAD + tDDC  
Although additional time to access data can be attained by trans-  
ferring data during tDDCA, this is not recommended because the  
ADAS3022 performs sensitive bit decisions during this time. If  
tDDCA is used, however, the minimum SCK frequency is  
17  
f
25 MHz  
SCK  
tAD + tDDC + tDDCA  
Rev. A | Page 33 of 40  
 
 
ADAS3022  
Data Sheet  
tDDCA  
SOC  
EOC  
SOC  
GENERAL TIMING  
tAD  
tDAC  
tDDC  
Figure 72 is a general timing diagram showing the complete  
register to conversion and readback pipeline delay. The figure  
details the timing upon power-up or upon returning from a full  
power-down by use of the PD input. Figure 73 and Figure 74 show  
the general timing diagrams when only the auxiliary ADC input  
channel pair is enabled for the data read during conversion (RDC)  
mode and the read after conversion (RAC) mode, respectively.  
CNV  
n
n + 1  
tCCS  
BUSY  
n
n + 1  
CS  
SDO  
n – 1  
n + 2  
n
n + 3  
n
DIN  
x
x
x
n + 3  
SCK  
Figure 71. Data Access Spanning Conversion  
tACQ  
EOC  
tCYC  
SOC  
SOC  
EOC  
tQUIET  
NOTE 2  
tDDC  
NOTE 1  
tDAC  
NOTE 1  
POWER  
UP  
CONVERSION (n – 1)  
UNDEFINED  
ACQUISITION (n)  
UNDEFINED  
CONVERSION (n)  
UNDEFINED  
ACQUISITION (n + 1)  
UNDEFINED  
CONVERSION (n + 1)  
UNDEFINED  
PHASE  
CNV  
BUSY  
tDDCA  
NOTE 2  
NOTE 5  
tAD  
NOTE 4  
CS  
X
1
16/32  
NOTE 3  
1
16  
SCK  
CFG  
INVALID  
CFG (n + 2)  
CFG (n + 2)  
CFG (n + 3)  
CFG (n + 3)  
DIN  
DATA  
INVALID  
DATA (n – 1)  
INVALID  
DATA (n – 1)  
INVALID  
DATA (n)  
INVALID  
DATA (n)  
INVALID  
SDO  
EOC  
EOC  
EOC  
ACQUISITION  
(n + 4)  
CONVERSION  
(n + 2)  
ACQUISITION  
(n + 3)  
CONVERSION  
(n + 3)  
CONVERSION  
(n + 4)  
ACQUISITION  
(n + 2)  
PHASE  
CNV  
BUSY  
CS  
1
1
16  
16  
1
SCK  
CFG (n + 4)  
CFG (n + 4)  
CFG (n + 5)  
CFG (n + 5)  
CFG (n + 6)  
CFG (n + 6)  
DIN  
DATA (n + 1)  
INVALID  
DATA (n + 1)  
INVALID  
SDO  
DATA (n + 2)  
DATA (n + 2)  
DATA (n + 3)  
DATA (n + 3)  
NOTES  
1. DATA ACCESS CAN OCCUR DURING A CONVERSION (tDDC), AFTER A CONVERSION (tDAC), OR BOTH DURING AND AFTER A CONVERSION.  
THE CONVERSION RESULT AND THE CFG REGISTER ARE UPDATED AT THE END OF A CONVERSION (EOC).  
2. DATA ACCESS CAN ALSO OCCUR UP TO tDDCA WHILE BUSY IS ACTIVE (SEE THE DIGITAL INTERFACE SECTION FOR DETAILS). ALL OF THE BUSY  
TIME CAN BE USED TO ACQUIRE DATA.  
3. A TOTAL OF 16 SCK FALLING EDGES IS REQUIRED FOR A CONVERSION RESULT. AN ADDITIONAL 16 EDGES ARE REQUIRED TO  
READ BACK THE CFG RESULT ASSOCIATED WITH THE CURRENT CONVERSION.  
4. CS CAN BE HELD LOW OR CONNECTED TO CNV. CS WITH FULL INDEPENDENT CONTROL IS SHOWN IN THIS FIGURE.  
5. FOR OPTIMAL PERFORMANCE, DATA ACCESS SHOULD NOT OCCUR DURING THE SAMPLING EDGE. A MINIMUM TIME  
OF THE APERTURE DELAY (tAD) SHOULD ELAPSE PRIOR TO DATA ACCESS.  
Figure 72. General Timing Diagram  
Rev. A | Page 34 of 40  
 
 
 
Data Sheet  
ADAS3022  
SOC  
EOC  
tAD  
tQUIET  
CNV  
n + 2  
n
n + 1  
BUSY  
CS  
n
n + 1  
n + 2  
n – 1  
n + 2  
SDO  
DIN  
n
n + 1  
n + 4  
n + 3  
16  
16  
1
1
1
16  
SCK  
Figure 73. General Timing Diagram of AUX Input Channel Pair (RDC)  
SOC  
EOC  
tEN  
tAD  
tQUIET  
CNV  
n + 2  
n + 3  
n + 3  
n
n + 1  
BUSY  
CS  
n
n + 1  
n + 2  
n
SDO  
DIN  
n + 1  
n + 4  
n + 2  
n + 5  
n + 3  
16  
1
1
16  
1
16  
SCK  
Figure 74. General Timing Diagram of AUX Input Channel Pair (RAC)  
Rev. A | Page 35 of 40  
 
 
ADAS3022  
Data Sheet  
conversions are required for the user-specified CFG setting to  
take effect. Therefore, the default value is CFG[15:0] = 0x8FCF.  
This sets the ADAS3022 as follows:  
CONFIGURATION REGISTER  
The configuration register, CFG, is a 16-bit, programmable  
register for selecting all of the ADAS3022 user-programmable  
options (see Table 11). The register is loaded when data is read  
back for the first 16 SCK rising edges and is updated at the next  
EOC. Note that there is always a two-deep delay (n + 2) when  
writing CFG and when reading back CFG for the setting  
associated with the current conversion.  
Overwrites contents of CFG register  
Selects the IN0 input channel referenced to COM  
Configures the PGIA gain to 0.20 ( 20.48 V)  
Selects the multiplexer input  
Disables the internal channel sequencer  
Disables the temperature sensor  
Enables the internal reference  
Selects normal conversion mode  
Selects SPI interface mode  
The default CFG setting is applied when the ADAS3022 returns  
from the reset state (RESET = high) to the operational state  
(RESET = low). However, when the ADAS3022 returns from the  
full power-down state (PD = high) to an enabled state (PD = low),  
the default CFG setting is not applied, and at least two dummy  
Table 10. Configuration Register, CFG; Default Value = 0x8FCF (1000 1111 1100 1111)  
15  
14  
13  
12  
11  
10  
9
8
7
6
5
4
3
2
1
0
CFG  
INx  
INx  
INx  
COM  
RSV  
PGIA PGIA PGIA MUX SEQ  
SEQ  
TEMPB REFEN CMS  
CPHA  
Table 11. Configuration Register Bit Description  
Bits  
Bit Name  
Description  
15  
CFG  
Configuration update.  
0 = keep current configuration settings.  
1 = overwrite contents of register (default).  
[14:12] INx  
Input channel selection in binary fashion. See the Multiplexer section.  
Bit 14  
Bit 13  
Bit 12  
Channel  
0
0
0
IN0 (default)  
1
1
1
IN7  
11  
COM  
IN[7:0] common channel input. AUX+ and AUX− are not referenced to COM.  
0 = channels are referenced in differential pairs: IN0/IN1, IN2/IN3, IN4/IN5, and IN6/IN7 (see the Channel Sequencer  
Details section).  
1 = each channel is referenced to a common sense, COM (default).  
Reserved. Setting or clearing this bit has no effect.  
10  
RSV  
[9:7]  
PGIA  
Programmable gain selection (see the Input Structure section). In basic sequencer modes, this register configures  
the range for all channels. In advanced sequencer mode, this register sets the range for IN0 (COM = 1) or the IN0/IN1  
pair (COM = 0). See the Advanced Mode section for the PGIA configurations of individual channels or channel pairs.  
Bit 9  
Bit 8  
Bit 7  
Absolute Input Voltage Range  
0
0
0
0
1
1
1
1
0
0
1
1
0
0
1
1
0
1
0
1
0
1
0
1
24.576 V  
10.24 V  
5.12 V  
2.56 V  
1.28 V  
0.64 V  
Not used  
20.48 V (default)  
6
MUX  
Multiplexer/auxiliary channel input (see the Auxiliary Input Channel section).  
0 = selects auxiliary channel on AUX inputs as active channel.  
1 = uses the selected analog front end (AFE) channel/channel pair (default).  
Rev. A | Page 36 of 40  
 
 
Data Sheet  
ADAS3022  
Bits  
Bit Name  
Description  
[5:4]  
SEQ  
Channel sequencer. Allows for scanning channels sequentially from IN0 to INx. INx is the last channel converted prior  
to resetting the sequence back to IN0 and is specified by the channel selected in the INx[2:0] configuration bits (see  
the Channel Sequencer Details section).  
Bit 5  
Bit 4  
Function  
0
0
1
1
0
1
0
1
Disable sequencer (default)  
Update configuration during basic sequence  
Initialize advanced sequencer  
Initialize basic sequencer  
Temperature sensor enable control (see the Channel Sequencer Details section).  
0 = internal temperature sensor enabled.  
1 = internal temperature sensor disabled (default).  
3
2
TEMPB  
REFEN  
Internal reference selection (see the Pin Configuration and Function Descriptions and Voltage Reference  
Input/Output sections for more information).  
0 = disables the internal reference. The internal reference buffer is disabled by pulling REFIN to ground.  
1 = enables the internal reference (default).  
1
0
CMS  
Conversion mode select (see the Conversion Modes section).  
0 = uses the warp mode for conversions with a time between conversion restriction.  
1 = uses the normal mode for conversions (default).  
CPHA  
MSB select (see the CPHA section).  
0 = asserting CS after the end of a conversion places the MSB on SDO, and the first SCK falling edge places (MSB − 1) on SDO.  
1 = asserting CS after the end of a conversion places the MSB on SDO, and the first SCK falling edge repeats MSB on SDO  
(default).  
CHANNEL SEQUENCER DETAILS  
Table 12. Typical Channel Sequencer Example  
The ADAS3022 includes a channel sequencer, which is useful for  
scanning channels in a sequential order. Channels are scanned  
individually with reference to COM or as pairs and can also  
include the auxiliary channel pair and/or the internal temperature  
sensor measurement. After the last programmed measurement  
is sampled, the ADAS3022 sequencer is reset to the first channel  
(IN0) or channel pair (IN0/IN1) and repeats the sequence until  
the sequencer is disabled or an asynchronous RESET or PD occurs.  
INx[14:12]  
COM  
MUX  
TEMPB  
End of Sequence  
IN3 (to COM)  
IN7 (to COM)  
IN6 to IN7  
TEMPB  
011  
111  
11x  
111  
111  
111  
1
1
0
1
1
1
1
1
1
1
0
0
1
1
1
0
1
0
AUX  
AUX  
INx and COM Inputs (MUX = 1, TEMPB = 1)  
When the channel sequencer is enabled, for all differential  
pairs, the positive terminals are the even channels (IN0, IN2,  
IN4, and IN6), and the negative terminals are, conversely, the  
odd channels (IN1, IN3, IN5, and IN7). When the channel  
sequencer is disabled, the user can assign either positive or  
negative terminals to even or odd channels for all differential  
pairs, depending on the INx[14:12] settings. For example, if  
INx[14:12] = 001 when using the IN0/IN1 pair, IN1 is the  
positive input and IN0 is the negative input.  
To use individual INx channels with reference to COM or pairs  
of INx channels in a sequence without converting the AUX or  
temperature sensor channels, the MUX and TEMPB bits must  
be set to 1. The last channel to be converted in the sequence is  
specified by the channel set in the INx bits. After the last channel is  
scanned, the next conversion starts over at IN0 or IN0/IN1. For  
paired channels, the channels are paired depending on the last  
channel set in INx. Note that the channels are always paired  
with the positive input on the even channels (IN0, IN2, IN4,  
IN6) and the negative input on the odd channels (IN1, IN3, IN5,  
IN7). Therefore, setting INx to 110 or 111 scans all pairs with  
the positive inputs dedicated to IN0, IN2, IN4, and IN6. For  
example, to scan four single channels, set INx to 011, COM to 1,  
and MUX to 1, which results in a sequence order of IN0, IN1,  
IN2, IN3, IN0, IN1, IN2, and IN3.  
Each sequence loop always starts with IN0 or IN0/IN1 and  
terminates with either the last channel/channel pair set in the  
INx bits, the temperature sensor, or the auxiliary input channel,  
depending on the configuration word. Table 12 provides a quick  
reference for how the device responds to the programmed configu-  
ration. For the first case, the channel sequencer scans Channel IN0  
through Channel IN3 in a repeated fashion. Note that the last  
conversion is corrupted when exiting the sequencer.  
Rev. A | Page 37 of 40  
 
 
ADAS3022  
Data Sheet  
Update During Sequence (SEQ = 01)  
INx and COM Inputs with AUX Inputs (MUX = 0, TEMPB = 1)  
Some of the CFG settings, such as PGIA and CMS, can be updated  
during a sequence. Writing a new CFG word with the appropriate  
bits to be changed for the (n + 2) conversion updates the sequencer  
from that point; all channels then use, for example, the new PGIA  
value. Note that changing bits in INx for the last channel or chang-  
ing COM reinitializes the sequencer at the (n + 2) conversion. A  
more practical method is to use the advanced sequencer mode as  
described in the Advanced Sequencer Mode (SEQ = 10) section.  
To use individual INx channels with reference to COM or pairs  
of INx channels with the AUX inputs in a sequence, the MUX  
bit must be set to 0 to append the AUX channel to the end of the  
sequence (after the channel set in INx is scanned). Note that the  
AUX input is a pair, whereas the INx channel can be referenced to  
COM or pairs of INx channels. For example, to scan four single  
channels and the AUX inputs, set INx to 011, COM to 1, and  
MUX to 0, which results in a sequence order of IN0, IN1, IN2,  
IN3, AUX, IN0, IN1, IN2, IN3, AUX, and so on.  
Advanced Sequencer Mode (SEQ = 10)  
INx and COM Inputs with Temperature Sensor  
(MUX = 1, TEMPB = 0)  
The advanced mode is useful for systems that require different  
gains for different individual INx inputs or different pairs of  
INx inputs. In this mode, two additional registers are used to  
program the various gain settings. After the initial CFG word  
enabling the advanced sequencer mode is written, the ADAS3022  
expects to receive at least one additional data transfer for the  
first advanced sequencer register, ASR0, or both advanced  
sequencer registers, depending on how many channels are in the  
sequence. Each ASR requires a conversion and a corresponding  
EOC to load the data into the device. The user cannot simply  
write 48 bits all at once because, as with all CFG word transfers,  
only the first 16 bits are latched and updated at EOC.  
To append the temperature sensor conversion to the end of the  
input channel sequence, the TEMPB bit must be set low in the  
configuration word. Note that the temperature sensor requires  
at least 5 µs between conversions. The data is output in straight  
binary format.  
INx and COM Inputs with AUX Inputs and Temperature  
Sensor (MUX = 0, TEMPB = 0)  
Both temperature sensor conversions and auxiliary channel  
conversions can be appended to the end of the input sequence  
by setting the MUX and TEMPB bits in the CFG register. For  
example, to scan all input channels with respect to COM, the  
temperature sensor, and the auxiliary channel at once, the user  
must set INx to 111, COM to 1, MUX to 0, and TEMPB to 0.  
The resulting sequence would be IN0, IN1, IN2, IN3, IN4, IN5,  
IN6, IN7, temperature sensor, and AUX.  
Note that the PGIA setting for IN0 or IN0/IN1 is written in the  
initial CFG register, and if using pairs of INx channels, only  
ASR0 is required. After the CFG and the associated advanced  
sequencer registers are updated, DIN must be held low for at  
least the MSB of subsequent data transfers; otherwise, the  
advanced sequencer mode will be aborted.  
Sequencer Modes  
The ADAS3022 has two sequencer modes, which are  
Table 13. Advanced Sequencer Register 0  
configured with the SEQ bits: basic mode and advanced mode.  
Basic mode can be used when all channels are configured with  
the same PGIA range. Advanced mode allows individual  
channel ranges to be programmed using two additional  
advanced sequence registers, ASR0 and ASR1. The SEQ bits are  
used to enable the sequencer. Setting SEQ to 01, 10, or 11 specifies  
which sequencer mode is used. Depending on the mode, basic  
or advanced sequencing determines the next data into DIN.  
Bits  
Function  
15  
ASR0 write enable  
0 = update ASR0 following CFG for advanced sequencer  
1 = enters normal CFG update  
Reserved  
[14:11]  
[10:8]  
7
PGIA for IN1 or IN2/IN3  
Reserved  
[6:4]  
3
PGIA for IN2 or IN4/IN5  
Reserved  
Note that for any sequencer update there exists a two-deep  
delay when writing the register for the setting to take effect.  
[2:0]  
PGIA for IN3 or IN6/IN7  
Table 14. Advanced Sequencer Register 1  
Basic Sequencer Mode (SEQ = 11)  
Bits  
Function  
The basic mode is useful for systems that use the same PGIA  
range on all channels. In basic sequencer mode, all that is  
required is a single CFG word to place the ADAS3022 in an  
automatically scanned mode. On the second conversion  
following the EOC for sequencer CFG, the sequencer starts.  
15  
ASR1 write enable  
0 = update ASR1 following ASR0  
1 = enters normal CFG update  
PGIA for IN4  
[14:12]  
11  
Reserved  
[10:8]  
7
PGIA for IN5  
After the CFG for basic sequence updates, DIN must be held  
low for at least the MSB during the data readback or a new CFG  
word will update, disabling the sequencer.  
Reserved  
[6:4]  
3
PGIA for IN6  
Reserved  
[2:0]  
PGIA for IN7  
Rev. A | Page 38 of 40  
 
Data Sheet  
ADAS3022  
OUTLINE DIMENSIONS  
6.10  
6.00 SQ  
5.90  
0.30  
0.25  
0.18  
PIN 1  
INDICATOR  
PIN 1  
INDICATOR  
31  
30  
40  
1
0.50  
BSC  
*
4.70  
EXPOSED  
PAD  
4.60 SQ  
4.50  
21  
10  
11  
20  
0.45  
0.40  
0.35  
0.25 MIN  
TOP VIEW  
BOTTOM VIEW  
FOR PROPER CONNECTION OF  
THE EXPOSED PAD, REFER TO  
THE PIN CONFIGURATION AND  
FUNCTION DESCRIPTIONS  
1.00  
0.95  
0.85  
0.05 MAX  
0.02 NOM  
SECTION OF THIS DATA SHEET.  
COPLANARITY  
0.08  
0.20 REF  
SEATING  
PLANE  
*
COMPLIANT TO JEDEC STANDARDS MO-220-VJJD-5  
WITH EXCEPTION TO EXPOSED PAD DIMENSION.  
Figure 75. 40-Lead Lead Frame Chip Scale Package (LFCSP_VQ)  
6 mm × 6 mm Body, Very Thin Quad  
(CP-40-15)  
Dimensions shown in millimeters  
ORDERING GUIDE  
Model1  
Temperature Range  
Package Description  
Package Option  
ADAS3022BCPZ  
ADAS3022BCPZ-RL7  
EVAL-ADAS3022EDZ  
−40°C to +85°C  
−40°C to +85°C  
40-Lead Lead Frame Chip Scale Package (LFCSP_VQ) CP-40-15  
40-Lead Lead Frame Chip Scale Package (LFCSP_VQ) CP-40-15  
Evaluation Board  
1 Z = RoHS Compliant Part.  
Rev. A | Page 39 of 40  
 
 
 
ADAS3022  
NOTES  
Data Sheet  
©2012–2013 Analog Devices, Inc. All rights reserved. Trademarks and  
registered trademarks are the property of their respective owners.  
D10516-0-1/13(A)  
Rev. A | Page 40 of 40  

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