FEATURES
Low Noise: 0.3 V p-p 0.1 Hz to 10 Hz
Low Nonlinearity: 0.003% (G = 1)
High CMRR: 120 dB (G = 1000)
Low Offset Voltage: 50 V
Low Offset Voltage Drift: 0.5 V/ⴗC
Gain Bandwidth Product: 25 MHz
Pin Programmable Gains of 1, 10, 100, 1000
Input Protection, Power On–Power Off
No External Components Required
Internally Compensated
MIL-STD-883B and Chips Available
16-Lead Ceramic DIP and SOIC Packages and
20-Terminal Leadless Chip Carriers Available
Available in Tape and Reel in Accordance
with EIA-481A Standard
Standard Military Drawing Also Available
PRODUCT DESCRIPTION
The AD524 is a precision monolithic instrumentation amplifier
designed for data acquisition applications requiring high accuracy under worst-case operating conditions. An outstanding
combination of high linearity, high common mode rejection, low
offset voltage drift and low noise makes the AD524 suitable for
use in many data acquisition systems.
The AD524 has an output offset voltage drift of less than 25 µV/°C,
input offset voltage drift of less than 0.5 µV/°C, CMR above
90 dB at unity gain (120 dB at G = 1000) and maximum nonlinearity of 0.003% at G = 1. In addition to the outstanding dc
specifications, the AD524 also has a 25 kHz gain bandwidth
product (G = 1000). To make it suitable for high speed data
acquisition systems the AD524 has an output slew rate of 5 V/µs
and settles in 15 µs to 0.01% for gains of 1 to 100.
As a complete amplifier the AD524 does not require any external components for fixed gains of 1, 10, 100 and 1000. For
other gain settings between 1 and 1000 only a single resistor is
required. The AD524 input is fully protected for both power-on
and power-off fault conditions.
The AD524 IC instrumentation amplifier is available in four
different versions of accuracy and operating temperature range.
The economical “A” grade, the low drift “B” grade and lower
drift, higher linearity “C” grade are specified from –25°C to
+85°C. The “S” grade guarantees performance to specification
over the extended temperature range –55°C to +125°C. Devices
are available in 16-lead ceramic DIP and SOIC packages and a
20-terminal leadless chip carrier.
Instrumentation Amplifier
AD524
FUNCTIONAL BLOCK DIAGRAM
PRODUCT HIGHLIGHTS
1. The AD524 has guaranteed low offset voltage, offset voltage
drift and low noise for precision high gain applications.
2. The AD524 is functionally complete with pin programmable
gains of 1, 10, 100 and 1000, and single resistor programmable for any gain.
3. Input and output offset nulling terminals are provided for
very high precision applications and to minimize offset voltage changes in gain ranging applications.
4. The AD524 is input protected for both power-on and poweroff fault conditions.
5. The AD524 offers superior dynamic performance with a gain
bandwidth product of 25 MHz, full power response of 75 kHz
and a settling time of 15 µs to 0.01% of a 20 V step (G = 100).
REV. E
Information furnished by Analog Devices is believed to be accurate and
reliable. However, no responsibility is assumed by Analog Devices for its
use, nor for any infringements of patents or other rights of third parties
which may result from its use. No license is granted by implication or
otherwise under any patent or patent rights of Analog Devices.
Power Supply Rangeⴞ6±15ⴞ18ⴞ6±15ⴞ18ⴞ6±15ⴞ18ⴞ6±15ⴞ18V
Quiescent Current3.55.03.55.03.55.03.55.0mA
NOTES
1
Does not include effects of external resistor RG.
2
VOL is the maximum differential input voltage at G = 1 for specified nonlinearity.
at the maximum = 10 V/G.
V
DL
= Actual differential input voltage.
V
D
Example: G = 10, V
= 12 V – (10/2 × 0.50 V) = 9.5 V.
V
CM
Specification subject to change without notice.
All min and max specifications are guaranteed. Specifications shown in boldface are tested on all production units at final electrical test. Results from those tests are used to
calculate outgoing quality levels.
Lead Temperature (Soldering 60 secs) . . . . . . . . . . . . +300°C
NOTES
1
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.
2
Max input voltage specification refers to maximum voltage to which either input
terminal may be raised with or without device power applied. For example, with ±18
volt supplies max V
is ±18 volts, with zero supply voltage max VIN is ±36 volts.
AD524AD–40°C to +85°C16-Lead Ceramic DIPD-16
AD524AE–40°C to +85°C20-Terminal Leadless Chip CarrierE-20A
AD524AR-16–40°C to +85°C16-Lead Gull-Wing SOICR-16
AD524AR-16-REEL–40°C to +85°CTape & Reel Packaging 13"
AD524AR-16-REEL7–40°C to +85°CTape & Reel Packaging 7"
AD524BD–40°C to +85°C16-Lead Ceramic DIPD-16
AD524BE–40°C to +85°C20-Terminal Leadless Chip CarrierE-20A
AD524CD–40°C to +85°C16-Lead Ceramic DIPD-16
AD524SD–55°C to +125°C16-Lead Ceramic DIPD-16
AD524SD/883B–55°C to +125°C16-Lead Ceramic DIPD-16
5962-8853901EA*–55°C to +125°C16-Lead Ceramic DIPD-16
AD524SE/883B–55°C to +125°C20-Terminal Leadless Chip CarrierE-20A
AD524SCHIPS–55°C to +125°CDie
*
Refer to official DESC drawing for tested specifications.
CAUTION
ESD (electrostatic discharge) sensitive device. Electrostatic charges as high as 4000 V readily
accumulate on the human body and test equipment and can discharge without detection.
Although the AD524 features proprietary ESD protection circuitry, permanent damage may
occur on devices subjected to high energy electrostatic discharges. Therefore, proper ESD
precautions are recommended to avoid performance degradation or loss of functionality.
REV. E–4–
LOAD RESISTANCE – V
OUTPUT VOLTAGE SWING – V
p-p
30
20
0
1010010k
1k
10
AD524–Typical Characteristics
20
15
10
+258C
INPUT VOLTAGE – 6V
5
0
0520
SUPPLY VOLTAGE – 6V
1015
Figure 1. Input Voltage Range vs.
Supply Voltage, G = 1
8.0
6.0
4.0
2.0
QUIESCENT CURRENT – mA
0
05201015
SUPPLY VOLTAGE – 6V
Figure 4. Quiescent Current vs.
Supply Voltage
20
15
10
5
OUTPUT VOLTAGE SWING – 6V
0
05201015
SUPPLY VOLTAGE – 6V
Figure 2. Output Voltage Swing vs.
Supply Voltage
16
14
12
10
8
6
4
2
INPUT BIAS CURRENT – 6nA
0
0520
SUPPLY VOLTAGE – 6V
1015
Figure 5. Input Bias Current vs.
Supply Voltage
Figure 3. Output Voltage Swing vs.
Load Resistance
40
30
20
10
0
–10
–20
INPUT BIAS CURRENT – nA
–30
–40
–75125
–252575
TEMPERATURE – 8C
Figure 6. Input Bias Current vs.
Temperature
16
14
12
10
8
6
4
INPUT BIAS CURRENT – 6nA
2
0
05201015
INPUT VOLTAGE – 6V
Figure 7. Input Bias Current vs. Input
Voltage
0
1
2
3
4
5
FROM FINAL VALUE – mV
OS
6
DV
0 1.08.02.0 3.0 4.0 5.0 6.0 7.0
WARM-UP TIME – Minutes
Figure 8. Offset Voltage, RTI, Turn
On Drift
1000
100
10
GAIN – V/V
1
01010M100 1k 10k 100k 1M
FREQUENCY – Hz
Figure 9. Gain vs. Frequency
REV. E
–5–
AD524
FREQUENCY – Hz
VOLT NSD – nV/ Hz
1000
100
0.1
110100k
1001k10k
10
1
G = 1
G = 10
G = 100, 1000
G = 1000
–140
G = 1000
G = 100
–120
G = 10
–100
G = 1
–80
–60
CMRR – dB
–40
–20
0
01010M100 1k 10k 100k 1M
FREQUENCY – Hz
Figure 10. CMRR vs. Frequency RTI,
Zero to 1k Source Imbalance
160
140
120
100
80
60
40
20
POWER SUPPLY REJECTION – dB
0
10100k
1001k10k
FREQUENCY – Hz
+VS = 15V dc +
1V p-p SINEWAVE
G = 1000
G = 100
G
= 10
G = 1
Figure 13. Positive PSRR vs.
Frequency
30
p-p
20
10
FULL POWER RESPONSE – V
0
1k10k1M100k
G1000G100 G10
FREQUENCY – Hz
G = 1, 10, 100
BANDWIDTH LIMITED
Figure 11. Large Signal Frequency
Response
160
140
120
100
80
60
40
20
POWER SUPPLY REJECTION – dB
0
10100k
1001k10k
FREQUENCY – Hz
–VS = –15V dc +
1V p-p SINEWAVE
G = 1000
G = 100
G
= 10
G = 1
Figure 14. Negative PSRR vs.
Frequency
10.0
8.0
6.0
4.0
SLEW RATE –V/ms
2.0
0
11000
GAIN – V/V
G = 1000
10100
Figure 12. Slew Rate vs. Gain
Figure 15. RTI Noise Spectral
Density vs. Gain
100k
10k
1000
100
0110k
CURRENT NOISE SPECTRAL DENSITY – fA/ Hz
101001k
FREQUENCY – Hz
Figure 16. Input Current Noise vs.
Frequency
VERTICAL SCALE; 1 DIVISION = 5mV
Figure 17. Low Frequency Noise␣ –
G = 1 (System Gain = 1000)
0.1 – 10Hz
VERTICAL SCALE; 1 DIVISION = 0.1mV
Figure 18. Low Frequency Noise –
G = 1000 (System Gain = 100,000)
0.1 – 10Hz
REV. E–6–
AD524
–12 TO +12
–8 TO +8
–4 TO +4
OUTPUT
STEP – V
+4 TO –4
+8 TO –8
+12 TO –12
020
1%0.1%0.01%
1%0.1%0.01%
51015
SETTLING TIME – ms
Figure 19. Settling Time Gain = 1
Figure 20. Large Signal Pulse
Response and Settling Time – G =1
–12 TO +12
–8 TO +8
–4 TO +4
OUTPUT
STEP – V
+4 TO –4
+8 TO –8
+12 TO –12
1%
1%
0.1%
0.1%
0.01%
0.01%
–12 TO +12
–8 TO +8
–4 TO +4
OUTPUT
STEP – V
+4 TO –4
+8 TO –8
+12 TO –12
020
0.1%0.01%
1%
1%
51015
SETTLING TIME – ms
0.1%
0.01%
Figure 21. Settling Time Gain = 10
Figure 22. Large Signal Pulse
Response and Settling Time
G = 10
–12 TO +12
–8 TO +8
–4 TO +4
OUTPUT
STEP – V
+4 TO –4
+8 TO –8
+12 TO –12
080
Figure 25. Settling Time Gain = 1000
1%0.1% 0.01%
1%0.1% 0.01%
204060
SETTLING TIME – ms
70103050
02051015
SETTLING TIME – ms
Figure 23. Settling Time Gain = 100
Figure 26. Large Signal Pulse Response and Settling Time G = 1000
Figure 24. Large Signal Pulse
Response and Settling Time
G = 100
REV. E–7–
AD524
INPUT
20V p-p
11kV
0.1%
100kV
0.1%
0.1%
1kV
100V
0.1%
RG
G = 10
G = 100
G = 1000
RG
10kV
0.01%
+V
1
AD524
2
–V
10kV
1kV
0.1%
10T
V
S
S
OUT
Figure 27. Settling Time Test Circuit
+V
S
V
B
R56
20kV
S
50mA
G100
G1000
C4C3
Q2, Q4
RG
I
2
R52
20kV
A3
R55
20kV
CH
1
SENSE
V
O
REFERENCE
+IN
R53
20kV
R54
20kV
I
4
50mA
CH2, CH3,
CH
4
2
–IN
CH2,
CH3, CH
CH
1
4
50mA
I
3
20kV
Q1, Q3
I
1
50mA
A1A2
R57
4.44kV
RG
1
404V
40V
–V
Figure 28 Simplified Circuit of Amplifier; Gain Is Defined as
((R56 + R57)/(R
)) + 1. For a Gain of 1, RG Is an Open Circuit
G
Theory of Operation
The AD524 is a monolithic instrumentation amplifier based on
the classic 3 op amp circuit. The advantage of monolithic construction is the closely matched components that enhance the
performance of the input preamp. The preamp section develops
the programmed gain by the use of feedback concepts. The
programmed gain is developed by varying the value of R
values increase the gain) while the feedback forces the collector
currents Q1, Q2, Q3 and Q4 to be constant, which impresses
the input voltage across R
.
G
(smaller
G
As RG is reduced to increase the programmed gain, the transconductance of the input preamp increases to the transconductance of the input transistors. This has three important advantages.
First, this approach allows the circuit to achieve a very high
open loop gain of 3 × 10
8
at a programmed gain of 1000, thus
reducing gain-related errors to a negligible 30 ppm. Second, the
gain bandwidth product, which is determined by C3 or C4 and
the input transconductance, reaches 25 MHz. Third, the input
voltage noise reduces to a value determined by the collector
current of the input transistors for an RTI noise of 7 nV/√Hz at
G = 1000.
INPUT PROTECTION
As interface amplifiers for data acquisition systems, instrumentation amplifiers are often subjected to input overloads, i.e.,
voltage levels in excess of the full scale for the selected gain
range. At low gains, 10 or less, the gain resistor acts as a current
limiting element in series with the inputs. At high gains the
lower value of R
will not adequately protect the inputs from
G
excessive currents. Standard practice would be to place series
limiting resistors in each input, but to limit input current to
below 5 mA with a full differential overload (36 V) would require over 7k of resistance which would add 10 nV√Hz of noise.
To provide both input protection and low noise a special series
protect FET was used.
A unique FET design was used to provide a bidirectional current limit, thereby, protecting against both positive and negative
overloads. Under nonoverload conditions, three channels CH
, CH
CH
, act as a resistance (≈1 kΩ) in series with the input as
3
4
,
2
before. During an overload in the positive direction, a fourth
channel, CH
, acts as a small resistance (≈3 kΩ) in series with
1
the gate, which draws only the leakage current, and the FET
limits I
the gate current must go through the small FET formed by CH
. When the FET enhances under a negative overload,
DSS
1
and when this FET goes into saturation, the gate current is
limited and the main FET will go into controlled enhancement.
The bidirectional limiting holds the maximum input current to
3 mA over the 36 V range.
INPUT OFFSET AND OUTPUT OFFSET
Voltage offset specifications are often considered a figure of
merit for instrumentation amplifiers. While initial offset may be
adjusted to zero, shifts in offset voltage due to temperature
variations will cause errors. Intelligent systems can often correct
for this factor with an autozero cycle, but there are many smallsignal high-gain applications that don’t have this capability.
10
100
1000
RG
+V
S
AD712
+V
1/2
G1, 10, 100
100V
s
1mF
1.62MV
1/2
1mF
–V
S
16.2kV
1.82kV
9.09kV
1kV
AD524
DUT
2
–V
S
16.2kV
1mF
G1000
Figure 29. Noise Test Circuit
REV. E–8–
AD524
40,000
2.105
G =
+1 = 20 620%
–V
S
+V
S
AD524
V
OUT
REFERENCE
1kV
RG
1
+INPUT
–INPUT
RG
2
2.105kV
1.5kV
40,000
4000
||4444.44
G =
+1 = 20 617%
G = 10
*R|
G = 10
= 4444.44V
*R|
G = 100
= 404.04V
*R|
G = 1000
= 40.04V
*NOMINAL (620%)
–V
S
+V
S
AD524
V
OUT
REFERENCE
RG
1
+INPUT
–INPUT
RG
2
4kV
RG
2
G = 100
G = 1000
RG
1
R2
5kV
R3
2.26kV
R
L
R1
2.26kV
G =
(R2||40kV) + R1 + R3
(R2||40kV)
(R1 + R2 + R3)||R
L
$ 2kV
G = 10
–V
S
+V
S
AD524
V
OUT
+INPUT
–INPUT
Voltage offset and drift comprise two components each; input
and output offset and offset drift. Input offset is that component
of offset that is directly proportional to gain i.e., input offset as
measured at the output at G = 100 is 100 times greater than at
G = 1. Output offset is independent of gain. At low gains, output offset drift is dominant, while at high gains input offset drift
dominates. Therefore, the output offset voltage drift is normally
specified as drift at G = 1 (where input effects are insignificant),
while input offset voltage drift is given by drift specification at a
high gain (where output offset effects are negligible). All inputrelated numbers are referred to the input (RTI) which is to say
that the effect on the output is “G” times larger. Voltage offset
vs. power supply is also specified at one or more gain settings
and is also RTI.
By separating these errors, one can evaluate the total error independent of the gain setting used. In a given gain configuration
both errors can be combined to give a total error referred to the
input (R.T.I.) or output (R.T.O.) by the following formula:
Total Error R.T.I. = input error + (output error/gain)
Total Error R.T.O. = (Gain × input error) + output error
As an illustration, a typical AD524 might have a +250 µV out-
put offset and a –50 µV input offset. In a unity gain configura-
tion, the total output offset would be 200 µV or the sum of the
two. At a gain of 100, the output offset would be –4.75 mV or:
+250 µV + 100(–50 µV) = –4.75 mV.
The AD524 provides for both input and output offset adjustment. This simplifies very high precision applications and minimize offset voltage changes in switched gain applications. In
such applications the input offset is adjusted first at the highest
programmed gain, then the output offset is adjusted at G = 1.
For best results R
temperature coefficient. An external R
should be a precision resistor with a low
G
affects both gain accuracy
G
and gain drift due to the mismatch between it and the internal
thin-film resistors. Gain accuracy is determined by the tolerance
of the external R
and the absolute accuracy of the internal resis-
G
tors (±20%). Gain drift is determined by the mismatch of the
temperature coefficient of R
and the temperature coefficient of
G
the internal resistors (– 50 ppm/°C typ).
Figure 31. Operating Connections for G = 20
The second technique uses the internal resistors in parallel with
an external resistor (Figure 32). This technique minimizes the
gain adjustment range and reduces the effects of temperature
coefficient sensitivity.
GAIN
The AD524 has internal high accuracy pretrimmed resistors for
pin programmable gain of 1, 10, 100 and 1000. One of the
preset gains can be selected by pin strapping the appropriate
gain terminal and RG
–INPUT
G = 100
G = 1000
+INPUT
together (for G = 1 RG2 is not connected).
2
10kV
INPUT
OFFSET
NULL
RG
G = 10
+V
S
1
AD524
RG
2
–V
S
V
OUT
OUTPUT
SIGNAL
COMMON
Figure 30. Operating Connections for G = 100
The AD524 can be configured for gains other than those that
are internally preset; there are two methods to do this. The first
method uses just an external resistor connected between pins 3
and 16, which programs the gain according to the formula
(see Figure 31).
REV. E–9–
40k
R
=
G
G =–1
Figure 32. Operating Connections for G = 20, Low Gain
T.C. Technique
The AD524 may also be configured to provide gain in the output stage. Figure 33 shows an H pad attenuator connected to
the reference and sense lines of the AD524. R1, R2 and R3
should be made as low as possible to minimize the gain variation
and reduction of CMRR. Varying R2 will precisely set the gain
without affecting CMRR. CMRR is determined by the match of
R1 and R3.
Input bias currents are those currents necessary to bias the input
transistors of a dc amplifier. Bias currents are an additional
source of input error and must be considered in a total error
budget. The bias currents, when multiplied by the source resistance, appear as an offset voltage. What is of concern in calculating bias current errors is the change in bias current with respect to
signal voltage and temperature. Input offset current is the difference between the two input bias currents. The effect of offset
current is an input offset voltage whose magnitude is the offset
current times the source impedance imbalance.
+V
S
AD524
LOAD
–V
S
TO POWER
SUPPLY
GROUND
a. Transformer Coupled
Although instrumentation amplifiers have differential inputs,
there must be a return path for the bias currents. If this is not
provided, those currents will charge stray capacitances, causing
the output to drift uncontrollably or to saturate. Therefore,
when amplifying “floating” input sources such as transformers
and thermocouples, as well as ac-coupled sources, there must
still be a dc path from each input to ground.
COMMON-MODE REJECTION
Common-mode rejection is a measure of the change in output
voltage when both inputs are changed equal amounts. These
specifications are usually given for a full-range input voltage
change and a specified source imbalance. “Common-Mode
Rejection Ratio” (CMRR) is a ratio expression while “CommonMode Rejection” (CMR) is the logarithm of that ratio. For
example, a CMRR of 10,000 corresponds to a CMR of 80 dB.
In an instrumentation amplifier, ac common-mode rejection is
only as good as the differential phase shift. Degradation of ac
common-mode rejection is caused by unequal drops across
differing track resistances and a differential phase shift due to
varied stray capacitances or cable capacitances. In many applications shielded cables are used to minimize noise. This technique can create common mode rejection errors unless the
shield is properly driven. Figures 35 and 36 shows active data
guards that are configured to improve ac common mode rejection by “bootstrapping” the capacitances of the input cabling,
thus minimizing differential phase shift.
+V
S
AD524
LOAD
–V
S
b. Thermocouple
+V
S
AD524
LOAD
–V
S
c. AC Coupled
Figure 34. Indirect Ground Returns for Bias Currents
TO POWER
SUPPLY
GROUND
TO POWER
SUPPLY
GROUND
Figure 35. Shield Driver, G ≥ 100
Figure 36. Differential Shield Driver
GROUNDING
Many data acquisition components have two or more ground
pins that are not connected together within the device. These
grounds must be tied together at one point, usually at the system power-supply ground. Ideally, a single solid ground would
be desirable. However, since current flows through the ground
wires and etch stripes of the circuit cards, and since these paths
have resistance and inductance, hundreds of millivolts can be
generated between the system ground point and the data
REV. E–10–
AD524
AD524
REF
SENSE
LOAD
AD711
+INPUT
–INPUT
R1
V
X
I
L
V
X
R1
I
L
= =
= (1 +
V
IN
R1
)
40,000
R
G
A2
acquisition components. Separate ground returns should be
provided to minimize the current flow in the path from the sensitive points to the system ground point. In this way supply currents
and logic-gate return currents are not summed into the same
return path as analog signals where they would cause measurement errors.
Since the output voltage is developed with respect to the potential on the reference terminal, an instrumentation amplifier can
solve many grounding problems.
DIG
COM
DIGITAL P.S.
+5V
C–15V
1mF
1mF1mF
AD574A
SIGNAL
GROUND
DIGITAL
DATA
OUTPUT
AD524
OUTPUT
REFERENCE
ANALOG P.S.
C+15V
0.1mF0.1
mF
6
*IF INDEPENDENT; OTHERWISE RETURN AMPLIFIER REFERENCE
TO MECCA AT ANALOG P.S. COMMON
0.1mF0.1
AND HOLD
*ANALOG
GROUND
mF
AD583
SAMPLE
Figure 37. Basic Grounding Practice
SENSE TERMINAL
The sense terminal is the feedback point for the instrument
amplifier’s output amplifier. Normally it is connected to the
instrument amplifier output. If heavy load currents are to be
drawn through long leads, voltage drops due to current flowing
through lead resistance can cause errors. The sense terminal can
be wired to the instrument amplifier at the load, thus putting
the IxR drops “inside the loop” and virtually eliminating this
error source.
V+
(SENSE)
OUTPUT
(REF)
CURRENT
BOOSTER
X1
R
L
VIN+
V
IN
AD524
–
V–
Figure 38. AD524 Instrumentation Amplifier with Output
Current Booster
Typically, IC instrumentation amplifiers are rated for a full ±10
volt output swing into 2 kΩ. In some applications, however, the
need exists to drive more current into heavier loads. Figure 38
shows how a high-current booster may be connected “inside the
loop” of an instrumentation amplifier to provide the required
current boost without significantly degrading overall performance. Nonlinearities, offset and gain inaccuracies of the buffer
are minimized by the loop gain of the IA output amplifier. Offset drift of the buffer is similarly reduced.
REV. E–11–
REFERENCE TERMINAL
The reference terminal may be used to offset the output by up
to ±10 V. This is useful when the load is “floating” or does not
share a ground with the rest of the system. It also provides a
direct means of injecting a precise offset. It must be remem-
bered that the total output swing is ±10 volts to be shared be-
tween signal and reference offset.
When the IA is of the three-amplifier configuration it is necessary that nearly zero impedance be presented to the reference
terminal.
Any significant resistance from the reference terminal to ground
increases the gain of the noninverting signal path, thereby upsetting the common-mode rejection of the IA.
In the AD524 a reference source resistance will unbalance the
CMR trim by the ratio of 20 kΩ/R
. For example, if the refer-
REF
ence source impedance is 1 Ω, CMR will be reduced to 86 dB
(20 kΩ/1 Ω = 86 dB). An operational amplifier may be used to
provide that low impedance reference point as shown in Figure
39. The input offset voltage characteristics of that amplifier will
add directly to the output offset voltage performance of the
instrumentation amplifier.
+V
S
VIN+
SENSE
AD524
–
V
IN
REF
–V
S
AD711
LOAD
V
OFFSET
Figure 39. Use of Reference Terminal to Provide Output
Offset
An instrumentation amplifier can be turned into a voltage-tocurrent converter by taking advantage of the sense and reference
terminals as shown in Figure 40.
Figure 40. Voltage-to-Current Converter
By establishing a reference at the “low” side of a current setting
resistor, an output current may be defined as a function of input
voltage, gain and the value of that resistor. Since only a small
current is demanded at the input of the buffer amplifier A
forced current I
drift specifications of A
will largely flow through the load. Offset and
L
must be added to the output offset and
2
, the
2
drift specifications of the IA.
AD524
R2
10kV
1mF
35V
–V
S
OUTPUT
OFFSET
NULL
+V
S
TO –V
AD524
1
2
3
4
5
6
7
8
16
15
14
13
12
11
10
9
20kV
20kV
20kV
404V
4.44kV
20kV
+V
S
20kV
20kV
40V
PROTECTION
PROTECTION
–IN
+IN
(+INPUT)
(–INPUT)
10kV
INPUT
OFFSET
NULL
10pF
20kV
AD711
–V
S
+V
S
AD7590
V
SS
V
DD
GND
39.2kV
28.7kV
316kV
1kV
1kV
1kV
V
DD
A2 A3
A4
WR
V
OUT
–IN
+IN
–V
+V
ANALOG
COMMON
1
PROTECTION
2
PROTECTION
INPUT
OFFSET
TRIM
S
S
1mF
35V
C1
GAIN TABLE
A
B
0
0
0
1
1
0
1
1
C2
3
4
R1
10kV
5
6
7
8
K1 – K3 =
THERMOSEN DM2C
4.5V COIL
D1 – D3 = IN4148
GAIN
10
1000
100
1
20kV
20kV
AD524
A1
20kV
+V
S
20kV
20kV
20kV
INPUTS
GAIN
RANGE
16
15
14
4.44kV
13
404V
12
40V
11
10
9
A
B
+5V
NC = NO CONNECT
R2
10kV
OUT
74LS138
DECODER
OUTPUT
OFFSET
TRIM
SHIELDS
NC
RELAY
Y0
Y1
Y2
G = 10
K1
G = 100
K1
K2
G = 1000
K3
+5V
K3D1
D2
K2
7407N
BUFFER
DRIVER
D3
10mF
LOGIC
COMMON
Figure 41. Three Decade Gain Programmable Amplifier
PROGRAMMABLE GAIN
Figure 41 shows the AD524 being used as a software programmable gain amplifier. Gain switching can be accomplished with
mechanical switches such as DIP switches or reed relays. It
should be noted that the “on” resistance of the switch in series
with the internal gain resistor becomes part of the gain equation
and will have an effect on gain accuracy.
The AD524 can also be connected for gain in the output stage.
Figure 42 shows an AD711 used as an active attenuator in the
output amplifier’s feedback loop. The active attenuation presents a very low impedance to the feedback resistors, therefore
minimizing the common-mode rejection ratio degradation.
Figure 42. Programmable Output Gain
REV. E–12–
AD524
WR
CS
+INPUT
G = 10
–INPUT
G = 100
G = 1000
RG
2
RG
1
+V
S
AD7524
+V
S
–V
S
–V
S
+V
S
OUT2
39kV
AD589
MSB
LSB
DATA
INPUTS
–V
S
1/2
AD712
1/2
AD712
R3
20kV
R4
10kV
R6
5kV
C1
GND
R5
20kV
OUT1
V
REF
AD524
RG
2
RG
1
+V
S
–V
S
8
AD524
15 16
14
13
V
DD
GND
0.1mF LOW
LEAKAGE
10
CH
1kV
V
OUT
910
A1A2A3A4
200ms
V
SS
ZERO PULSE
AD7510KD
AD711
11
12
+INPUT
(–INPUT)
G = 10
G = 100
G = 1000
–INPUT
(+INPUT)
DAC A/DAC B
RG
RG
1
13
12
11
16
1
3
2
2
DATA
INPUTS
PROTECTION
4.44kV
404V
40V
PROTECTION
CS
WR
AD524
V
b
20kV
20kV
+V
S
17
3
4
14
7
15
16
6
18
DAC A
DB0
DB7
AD7528
DAC B
5
20kV
20kV
20kV
10
9
6
20kV
1/2
AD712
2
1/2
AD712
256:1
1
19
20
V
OUT
Figure 43. Programmable Output Gain Using a DAC
Another method for developing the switching scheme is to use a
DAC. The AD7528 dual DAC, which acts essentially as a pair
of switched resistive attenuators having high analog linearity and
symmetrical bipolar transmission, is ideal in this application.
The multiplying DAC’s advantage is that it can handle inputs of
either polarity or zero without affecting the programmed gain.
The circuit shown uses an AD7528 to set the gain (DAC A) and
to perform a fine adjustment (DAC B).
Figure 44. Software Controllable Offset
In many applications complex software algorithms for autozero
applications are not available. For those applications Figure 45
provides a hardware solution.
AUTOZERO CIRCUITS
In many applications it is necessary to provide very accurate
data in high gain configurations. At room temperature the offset
effects can be nulled by the use of offset trimpots. Over the
operating temperature range, however, offset nulling becomes a
problem. The circuit of Figure 44 show a CMOS DAC operating in the bipolar mode and connected to the reference terminal
to provide software controllable offset adjustments.
REV. E–13–
Figure 45. Autozero Circuit
AD524
ERROR BUDGET ANALYSIS
To illustrate how instrumentation amplifier specifications are
applied, we will now examine a typical case where an AD524 is
required to amplify the output of an unbalanced transducer.
Figure 46 shows a differential transducer, unbalanced by 100 Ω,
supplying a 0 to 20 mV signal to an AD524C. The output of the
IA feeds a 14-bit A-to-D converter with a 0 to 2 volt input volt-
age range. The operating temperature range is –25°C to +85°C.
Therefore, the largest change in temperature ∆T within the
operating range is from ambient to +85°C (85°C – 25°C = 60°C).
+10V
350V
350V350V
350V
RG
G = 100
RG
1
2
Figure 46. Typical Bridge Application
Table II. Error Budget Analysis of AD524CD in Bridge Application
In many applications, differential linearity and resolution are of
prime importance. This would be so in cases where the absolute
value of a variable is less important than changes in value. In
these applications, only the irreducible errors (45 ppm = 0.004%)
are significant. Furthermore, if a system has an intelligent processor monitoring the A-to-D output, the addition of a autogain/autozero cycle will remove all reducible errors and may
eliminate the requirement for initial calibration. This will also
reduce errors to 0.004%.
+V
S
10kV
14-BIT
AD524C
–V
S
ADC
0V TO 2V
F.S.
Effect onEffect on
AbsoluteAbsoluteEffect
AD524CAccuracyAccuracyon
Error SourceSpecifications Calculationat TA = +25ⴗC at TA = +85ⴗCResolution
*Output offset voltage and output offset voltage drift are given as RTI figures.
REV. E–14–
AD524
Figure 47 shows a simple application, in which the variation of
the cold-junction voltage of a Type J thermocouple-iron(+)–
constantan–is compensated for by a voltage developed in series
by the temperature-sensitive output current of an AD590 semiconductor temperature sensor.
R
A
NOMINAL
TYPE
J
K
E
T
S, R
MEASURING
JUNCTION
VALUE
52.3V
41.2V
61.4V
40.2V
5.76V
REFERENCE
JUNCTION
+158C < TA < +358C
IRON
V
CONSTANTAN
T
EO = VT – VA +
≅ V
T
+V
S
I
+ 2.5V
A
52.3V
R
A
AD590
CU
– 2.5V
T
A
V
A
52.3VI
1 +
7.5V
2.5V
AD580
R
A
E
O
52.3V
8.66kV
R
T
1kV
NOMINAL VALUE
9135V
G = 100
+V
S
–V
S
OUTPUT
AMPLIFIER
OR METER
AD524
Figure 47. Cold-Junction Compensation
The circuit is calibrated by adjusting RT for proper output voltage
with the measuring junction at a known reference temperature
and the circuit near 25°C. If resistors with low tempcos are
used, compensation accuracy will be to within ±0.5°C, for
temperatures between +15°C and +35°C. Other thermocouple
types may be accommodated with the standard resistance values
shown in the table. For other ranges of ambient temperature,
the equation in the figure may be solved for the optimum values
and RA.
of R
T
The microprocessor controlled data acquisition system shown in
Figure 48 includes both autozero and autogain capability. By
dedicating two of the differential inputs, one to ground and one
to the A/D reference, the proper program calibration cycles can
eliminate both initial accuracy errors and accuracy errors over
temperature. The autozero cycle, in this application, converts a
number that appears to be ground and then writes that same
number (8-bit) to the AD7524, which eliminates the zero error
since its output has an inverted scale. The autogain cycle converts the A/D reference and compares it with full scale. A multiplicative correction factor is then computed and applied to
subsequent readings.
For a comprehensive study of instrumentation amplifier design
and applications, refer to the Instrumentation Amplifier Applica-tion Guide, available free from Analog Devices.
V
AD7507
A0 A2
EN A1
LATCH
RG
2
RG
1
20kV
1/2
AD712
AD524
10kV
AD712
5kV
ADDRESS BUS
20kV
1/2
ADDRESS BUS
AD583
–V
REF
AD7524
DECODE
V
N
I
AGND
AD574A
CONTROL
REF
PROCESSOR
MICRO-
Figure 48. Microprocessor Controlled Data Acquisition System
REV. E–15–
AD524
OUTLINE DIMENSIONS
Dimensions shown in inches and (mm).
16-Lead Ceramic DIP
(D-16)
0.005 (0.13) MIN
0.200 (5.08)
MAX
0.200 (5.08)
0.125 (3.18)
0.358 (9.09)
0.342 (8.69)
SQ
TOP
VIEW
0.080 (2.03) MAX
16
1
0.840 (21.34) MAX
0.023 (0.58)
0.014 (0.36)
PIN 1
0.100
(2.54)
BSC
9
8
0.070 (1.78)
0.030 (0.76)
0.310 (7.87)
0.220 (5.59)
0.060 (1.52)
0.015 (0.38)
0.150
(3.81)
MAX
SEATING
PLANE
0.320 (8.13)
0.290 (7.37)
20-Terminal Leadless Chip Carrier
(E-20A)
0.200 (5.08)
BSC
REF
0.055 (1.40)
0.045 (1.14)
0.075
(1.91)
REF
19
18
14
13
20
1
BOTTOM
VIEW
0.150 (3.81)
4
8
BSC
0.100 (2.54)
0.064 (1.63)
0.358
(9.09)
MAX
SQ
0.088 (2.24)
0.054 (1.37)
0.095 (2.41)
0.075 (1.90)
0.011 (0.28)
0.007 (0.18)
R TYP
0.075 (1.91)
0.015 (0.38)
0.008 (0.20)
0.100 (2.54) BSC
0.015 (0.38)
3
MIN
0.028 (0.71)
0.022 (0.56)
0.050 (1.27)
BSC
9
45° TYP
C722e–0–4/99
0.0118 (0.30)
0.0040 (0.10)
16-Lead SOIC
0.4133 (10.50)
0.3977 (10.00)
169
PIN 1
0.0500
0.0192 (0.49)
(1.27)
0.0138 (0.35)
BSC
(R-16)
0.2992 (7.60)
81
0.1043 (2.65)
0.0926 (2.35)
SEATING
PLANE
0.2914 (7.40)
0.4193 (10.65)
0.3937 (10.00)
0.0125 (0.32)
0.0091 (0.23)
0.0291 (0.74)
0.0098 (0.25)
0.0500 (1.27)
8°
0°
0.0157 (0.40)
x 45°
PRINTED IN U.S.A.
REV. E–16–
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