Techniques and Applications for High Throughput and

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CONTENTS
INTRODUCTION
1.
2.
2
. . . . . . . . .. . .. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
. . . . . . . . . . . . . . .._._..................................................
2
4
. . .. . . .. .. . . . . .. .. . . .. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .. .. . . . . . . .. .. . . . . . . . . . . . . . . . . . . . . .
8
. . . . . . . . . . . . . . . . . . . . . . . . . . . . .. .. . . . . . . . . . . .. . .. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Bias Source in S Parameter Measurements
HP 4142B and External Power Supplies . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .. . . . . . . . . . . .. .
Evaluation
of Solar Cell Characteristics
. . . . . . . . . . . . . . .._._................_..................................................
Evaluation
of CMRR, PSRR, and Open Loop Gain of an Opamp . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
. . .. . . .. . . . . . . . . .. .. . . . . . . . . .. .. .. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Transient Thermal Resistance Measurements
Dielectric Absorption
Measurements
. . . . . .. . . . . . . . . . . .. . . . . . . . . . . . . .. . . . . . . . . . . .. .. . . . . . . . . . . . . . . . . . . . . . . . .. . . . . . . . . . . . . . . . . . . .
Simplified Capacitance Measurements
using the AFU . .. .. . . . . . . . . . . . . . . .. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Noise Evaluation
by FFT Analysis . . . . . . . . . . . .. .. . . . . . . . . .. . . . . . .. . .. .. . . . . . . . . . . . . . . .. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
8
9
10
10
12
14
15
16
References
FOR HIGH
THROUGHOUT
AND
STABLE
of Very Low Currents
High Speed Measurements
Preventing
Oscillation in High-Frequency
Devices
APPLICATION
2.1
2.2
2.3
2.4
2.5
2.6
2.7
2.8
Page
1
..... ............ .
TECHNIQUES
1.1
1.2
. . . . . . . . . . .. .. . . . . . . . . . . . . . . . . . . . . .. . . . . . . . . . . . . .. . . . . . . . . . . . . .. . . . . . . . . . . . . .. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ................
EXAMPLES
CHARACTERIZATION
.. . . . . . . . . . . . . . . . . . . . . . . . . . .. .. .. . . .. . . . . . . . . . . . . . . . . . . . . . . . . . . . . .. . . . . . . . . . . . . .. .. . . . . . . .. .. .. . . . . . . . . . . . . .. . . . . . . . . . . . .............................
.-
16
APPENDIX
PROGRAM
Listings
CMRR Measurements
. . .. . . . . . . . .. . . . . . . . . . . . . . . . .._.............................................................................
. .. .. . . . . . . . . . . .._...................................._____._.........._...
Transient Thermal Resistance Measurements
. . . . . . . . . . .. . . . . . . . . .. . . . . . . . . . . . . . . . . . . . . . . . . . . . .. . . . . . . . . . . .. . . . . . . . . . . .. .. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
C Measurements
Noise Evaluation by FFT Analysis . . . . . . . . . . . . . . . . . . . . .. . . . . . . . . . . . . . . .. . . . . . . . . .. .. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .. . . . . . . . . . . . .
1.7
18
1.9
20
u
INTRODUCTION
r-
Module Configuration
The HP 4142B Modular DC Source/Monitor
is a high speed,
highly accurate computer-controlled
DC parametric
measurement
instrument
for characterizing
semiconductor
devices, such as MOSFETs, GaAs devices, operational
amplifiers, etc., plus other components,
such as capacitors,
insulators, etc.
This Application
Note provides helpful information
on using
the HP 4142B,
and includes many application examples.
measurement
in high-
Chapter 2 describes practical application
examples utilizing
the Analog Feedback Unit (AFU) and various testing
capabilities of the HP 4142B such as synchronous
staircase
sweep, high-speed
spot measurements,
etc.
For the basic principles of HP 4142B operation,
refer to the
application note “High Speed DC characterization
of
Semiconductor
Devices from Sub pA to IA” (Application
Note
356).
Quantity
Description
HP 41420A
HP
41421B
Source
Monitor
40pV--2ooVi2ofA-IA
Unit
1
Source Monitor
Unit
4
4OpV-lOOV/20fA-lOOmA
HP-41424A
Voltage
Voltage
ImV-4OV,
Chapter 1 describes techniques for high-speed
of low currents, and how to prevent oscillation
frequency semiconductor
devices.
as shown below
HP 41425A
Analog
Source/
Monitor
Unit
1
2OpA-lOOmA/4pV-40V
Feedback Unit
1
1. TECHNIQUES FOR HIGH THROUGHPUT
STABLE CHARACTERIZATION
1.1 High -Speed Measurements
of Very
Low Currents
Generally,
the higher the accuracy of measuring
picoamperelevel currents, the longer the measurement
time. This is due
to the following
reasons:
2.
3.
4.
5.
The ranging time required for switching to a low current
range increases.
A lower current range requires longer time for charging
the parasitic capacitance of devices and the test system.
Since the frequency bandwidth
of the measuring
instrument
is narrower
with a lower current
range, the
settling time becomes longer.
Lower current ranges require a longer time for averaging
in order to reduce the influence of noise.
In low current ranges, devices and dielectric absorption
elements in a test system have a great influence on the
time required for settling after a change of set voltage.
Important
points for compensating
for these conditions
when measuring low currents at high speed using the
HP 4142B are described below.
Minimize
Ranging Time
If a current range is not specified, HP 4142B operates in the
auto-ranging
mode. In other words, the current ranges are
switched one by one, starting from the range determined
by
current compliance, until the current range of maximum
resolution
without overflow
is reached. The HP4142B has ten
current ranges. This means that it may be necessary to
traverse across as many as nine ranges in some cases.
Table 1.1.1 lists typical times required for switching from
one range to another. The values in the table include waiting
time accompanying
range-switching
operation.
The table
shows that the lower the final current range in auto-ranging
mode, the longer the time required for switching
(ranging
time).
l
Jnhle
7.7.7
Jypirnl
Time
Required
for
Su~ifrlring
from
Ranging
time
One
Rnnge
to Another
I range
IOOfiA-
IA
20
IOnA-lOOpA
I nA-
IO ms
IOnA
ms
50 ms
To specify a current range, two ranging methods are
available: Limited Auto-Ranging
and Fixed-Range.
Limited
Auto-Ranging
allows automatic range changes between the
specified range and higher ranges. This method does not
involve unnecessary
switching to a lower current range, and
thereby reduces the ranging time accordingly.
Another method is Fixed-Range operation, in which the
range is switched from the present range to a specified range
along the shortest route. For example, switching
from lOOpA
(initial range) to 1 nA (minimum
range) in the fixed range
mode takes about 50 ms including waiting time (>I30 ms in
auto-ranging
mode). Therefore,
to minimize the ranging time,
it is recommended
to specify a range and switch to it in the
Limited Auto-Ranging
mode or Fixed-Range
mode.
2
of Balance between
Waiting Time
Maximum
Resolution
and
Table 1.1.2 lists the ratio of measurement
waiting time of
three low current ranges (taking the waiting time for the 100
nA range as 1) and the maximum measurement
resolution.
The table shows that in low current ranges the waiting time
doubles successively for each lower range. It is therefore
desirable to select the range that provides acceptable
resolution
with as large a full scale as possible.
Electronic devices made by advance process technology,
such
as micro lithography,
require highly accurate high speed
measurements
of very low currents. This section describes
several programming
techniques that will enable you to make
high-speed,
low currents measurements.
1.
Consideration
Measurement
l
AND
7.7.2
Jnhle
/
/
Wait
I range
time”
IOOnA
IOnA
InA
* Ratio
l
from
Minimizing
Resolution
,
(measurement)
2
I
2.4
/
I
5.5
PA
2:: 1971
the time at 100 nA
Settling
Time
The settling time is the time required to settle to a newly set
value when the setting of the Source/Monitor
Unit (SMU)
output is changed. The settling time consists of a slewing
period and a period of convergence to a final value.
Figure 1.1.1 shows an example of a measurement
circuit
applying a voltage to a load resistance. figure 1.1.1 (a) shows
the case of a purely resistive load. The SMU output rises at
the maximum slew rate, which is determined
by the SMU
current range and current compliance. Figure 1.1.3 shows the
maximum
slew rate with respect to current compliance.
In actuality, there are stray capacitances in the
measurement
environment,
such as in the instrument,
cabling,
fixturing
and DUT, so the slew rate is limited
by current
compliance Ic and load capacitance CL to ~/CL.
Figure 1.1.2 shows this situation with the SMU operation
curve. Route @ corresponds
to figure 1.1.1 (a), and routes @
and @’ to figure 1.1.1 (b). In other words, if the DUT has
parasitic capacitances, the SMU operates with constant
current while the voltage is rising.
Route @ represents the case of small-current
compliance,
and @’ large current compliance. It is assumed, in the case of
route @, the current is decided by the maximum slew rate of
the SMU, while, in other case 0, the current is limited by the
current compliance.
After the slewing period, the SMU operates with constant
voltage (from points B and B’) until converging
to the final
value at point A. This period of convergence
is longer for
lower current ranges.
Thus, to minimize the settling time, set as large a current
compliance as possible when changing SMU output.
Example
This section gives an example of measuring low currents
using an actual device. Figure 1.1.4 shows a measurement
circuit, items being measured, and test conditions. Figure 1.1.5
shows the SMU output voltage waveforms during the
measurement:
(a) corresponds to leakage current
measurement
in the auto-ranging
mode, and (b), to the
measurement
in the limited auto-ranging
mode. This shows
that the total measurement
time is reduced by about half.
l
-mei
._
Figure 7.1.1
SMU
Output
Figure I.1 .d Diode Test Example
Change
A
DIJT
SMU
----+
(a) Resistive
K
time
Load
~
GNDU
-time
(b) Resistive
Load with Parasitic
Figure 1.1.5 (a) SMU
Capacitahce
,htir,neI
Figure 1,1.2
MpI
Graph
Operatitig Curve of SMU
Waveform in Auto-Ranging
Output
----------_-__---
20.8
m
V/dlv
Status:
-36.8
v
Rcqulsltlon
280
Cursor x
-___-_-_-L’
,968
-490
mV
ms
0
968
660
mV
ms
iursor
cursor
o-x
a.0i3 v
1.15 s
.v
Channel
818
w
I
Maximum
Slew Rate in 1 Source
MRX
SLEW
RRTE
(@ILoop)
-756.0
ms/d t v
ms
.: ....’...‘.
:.. :....... ...(
..j.‘. in..~
r:....:I
/
I
L------
”
------------------Status:
Hcqulsitlon
Auto Scale
Store
Ilode
Coupling
I. 1.3
Stopped--..--
1:
I
*
Figure
Mode
Mode
Graph
20.0
m
l:,
Cursor x
Cursor
-38.8
v
288
ms/drv
-750.0
ms
1
i
X Selected
-323
-370
V/drv
m
Stopped-----
mV
ms
0
968 mV
140 ms
:,
z
IE-3.
//
.
I
/
/
I
3
1.2 Preventing
Oscillation in
High-Frequency
Devices
Figure
7.2.7
General
Setup of a Mensurement
Cirmit
When measuring
parameters
(HFE, gm, etc.) of
high-frequency
devices like power MOSFETs,
GaAs MESFETs
and high-frequency
bipolar transistors using an HP 4142B SMU,
oscillation
may cause measurement
problems.
This section
describes oscillation
problems and techniques for solving them.
There
SMUs.
are two type of oscillation
1. Oscillation
(Oscillation
Related to the SMU
frequency < 300 kHz)
(1) Oscillation
of SMU output
by inductive load
(2) Oscillation
when inductive
source mode.
* Note:
2. Oscillation
(Oscillation
Oscillation
that may occur when using
The guard
amplifier
part (guard
amplifier*)
load is connected
forces a guard
Not Related to the SMU
frequency > 3 MHz)
associated with the following
voltage.
caused
to SMU in I
(See A/N356
Figure I .2.2
p.2.)
AC
Equivalent
Circuit
devices:
(1) FETs (power MOSFETs, GaAs MESFETs)
(2) High frequency bipolar transistors
Oscillation
in 1. may not arise as a problem because the
minimum
capacitance required to prevent oscillation is added
to the SMU output part. This section, therefore,
will focus on
the oscillation
not related to the SMU.
This section uses GaAs MESFET as an example and
describes conditions for oscillation and techniques to prevent
oscillation.
Conditions
for Oscillation
Figure 1.2.1 shows the general setup of a measurement
circuit. Suppose that both drain and gate are connected to the
SMU in the voltage mode via a cable of 1.5 m to 3 m length.
Figure 1.2.2 shows an AC equivalent circuit. The output
impedance of the SMU at 3 MHz or higher is capacitive
regardless of the SMU operation
mode (voltage/current
mode)
and so can be considered as equivalent
to a common voltage.
It can be seen that this circuit forms a negative feedback
amplifier,
with feedback by Cgd. If this negative feedback
amplifier meets the conditions
for oscillation, it becomes a
Hartley oscillator. The frequency of oscillation of the circuit is
expressed as
l
Figure
7.2.3
of
Figure 7.2.4
‘W
4
Circuit
with
nn Open
A 1 Amplifier
B : Load Impedance
C : Feedback
Cirucit
fci= 27rqqJ *
When Lg = 1 PH and Cgd = 100 pF, the frequency
oscillation
is calculated as
1
fo = 2TJ10-~ . 1o-‘o = 16 MHz
Equivalent
Feedback Circuit
‘W
Feedhnck
Loop
Next, let us examine the conditions
for oscillation
aspect of loop gain. Figure 1.2.3 shows an equivalent
with an open feedback loop. In the figure, rs and Ls
stabilizing elements and considered as 0 in the worst
The voltage-controlled
current source is inverted to
polarity of loop gain positive. The equivalent
circuit
divided into three blocks: amplifier,
load impedance,
feedback circuit.
from the
circuit
are
case.
make the
can be
and
Figure
7.2.5
Trnnsfm
Chomfcristir
of Feedbnrk
Cirrrrif
Im
Now, let us look at the feedback circuit. In a frequency
range of 3 to 30 MHz, we can assume the following:
1
->>
wcgs
0Lg
Cgs, therefore,
can be omitted. As a result, the feedback
circuit can be represented
as shown in figure 1.2.4. Figure
1.2.~ shows the transfer characteristic
of the circuit.
Figure 1.2.5 (a) shows the gain and phase characteristics,
and figure 1.2.5 (b) the characteristics
represented
on a
vector plane.
The transfer characteristic
of the feedback circuit has a
resonance point, the peak of which is equal to Q of a series
resonance circuit.
Next, let us look at the load impedance. In a frequency
range of 3 to 30 MHz, the following
can be assumed:
1>>
wcgs
More
More
*More
l
unstable
unstable
unstable
Bode
Figure 7.2.6
(b)
plot
Loop Gnin
Locus
Chorncterisfirs
on vector
fNyquisf
Plnntl
Im
t
oLd
The load impedance, therefore,
can be considered to be
inductive.
Thus, the frequency characteristic
of loop gain is
represented
on a vector plane (Nyquist Plane) as shown in
figure 1.2.6 0. In the figure, point U (-1, 0) is where the
conditions for oscillation are met, and point P is where loop
gain is at its peak. Spacing between points U and I’ is
proportional
to the gain margin. As the spacing is reduced,
oscillation is more likely to occur. The maximum loop gain at
point P is proportional
to gm, Q of the feedback circuit, and load
inductance
Ld. Therefore,
conditions
for instability
are as
follows:
l
I
bf
(a)
Figure 7.2.7
as gm increases.
as Lg increases or rg decreases.
as Ld increases.
Figure 1.2.7 shows
the qualitative
interrelationship
of gm,
Lg, and rg with respect to their influence on stability.
gm
Inh-rrelnhnship
of Gm,
Lg. rind rg
plane
Preventing
Oscillation
Taking into consideration
the above, the following
can be used to prevent
oscillation (figure 1.2.8).
l
@ Add external series resistance Rg or
at the input to the gate.
@ Add a series RC circuit between the
@ Add a series RC circuit between the
@ Add a bypass capacitor between the
resistive
ferrite
beads
gate and drain.
gate and source.
drain and source.
Reasons for these methods are explained below.
First, method
@ is intended to increase the gain margin by
decreasing the Q of the feedback circuit and thereby reducing the
loop gain. Since the resistive impedance of ferrite beads isat most
100 ohms or so, devices of large gm require multiple sets of ferrite
beads.
To make the measure effective, Rg must meet
Rg>L
where
Tflble
woLg
WO:frequency
of oscillation
(~0 =2?rfo)
If an external resistance cannot be inserted, for example
when the gate resistance rg of the device itself is to be
measured, methods @ and @ are effective. The additional RC
element operates near a resonance point of the feedback
circuit to reduce the peak of the loop gain that would occur
due to resonance. These methods bring the loop gain to
characteristic
@ in figure 1.2.6 and thus add an increase of
gain margin, thereby stabilizing
the operation of the SMU.
To make the solutions effective, the additive elements must
meet the following
criteria:
(i) RI, RZ </$
(ii) --CfR, ,
CB,
< wo
Method @ reduces the inductance due to a long cable
connected to drain and source by means of the bypass
capacitor, and thereby decrease the loop gain.
Connect this bypass capacitor as near the device as possible.
The capacitance should be in the range 100-1000
pF. Do not
use a large capacitance, otherwise
the SMIJ will oscillate or
respond slowly.
The above description
used a GaAs MESFET as an example
of a device. The same solutions can be applied to power
MOSFETs and high-frequency
bipolar transistors
to prevent
them from oscillating.
6
Example
This section gives an example of oscillation during an actual
measurement
and describes methods for preventing
oscillations. This example concerns the measurement
of the
Id-Vds characteristics
of a GaAs FET having the characteristics
shown in table 1.2.1. The device and HP 4142B are connected
via a 1.5 m cable. Figure 1.2.9 shows the measurement
results. With Vds = 0.5 V or higher, proper measurement
is
not possible due to oscillation. The oscillation waveform
is
shown in figure 1.2.10.
The oscillation frequency and
amplitude
are 26 MHz and 8 Vpp respectively.
To prevent oscillation, an RC circuit is inserted between the
gate and drain as shown in figure 1.2.11. Figure 1.2.12 shows
measurements
after inserting the RC circuit. The
measurement
can be made properly after this has been done
l
methods
1.2.7
I
; Parameter
1
ldss
Cgd
Value
I
IO
25
/ Unit
j
Conditions
jAlVcs=O
PF
j
I
VCD =
-4V,
Id = 0
..--s
Figure
7.2.8
Methods
to Prevent
Oscillation
Figure
7.2.11
Prurtire
Example
SMUI
(200V/IA)
of Oscillation
Prevention
I OOP
D
I K
G
SMU2
(lOtii/lOOmA)
S
GNDU
Figure
1.2.9
Measurement
Id-Vds
1111
1.2. I.?
Measurement
I d-Vds
Result
after
Inserting
the RC
Curcuit
CURVE
I
I
/
.8 t--------
ljraph
Figure
CURVE
t
Figure
Result
5
------’
I .I. IO
.
L
2.88
Oscillation
Vfdlv
Waveform
a.00
v
(Drain
58.8
ns,‘div
Voltage)
99.75
--
us
7
2. APPLICATION
EXAMPLES
2.1 Bias Source in S Parameter
Measurements
Figure
2.1.2
Biasing Using
TWO Independent Sources
S parameter
measurement
using network analyzers is a very
commonly used method for evaluating
high-frequency
semiconductor
devices, such as GaAs MESFETs and
microwave range bipolar transistors (BJT). Use of the
HP 4142B as the external bias source improves device
characterization
by using the advanced output control
capability of the Analog Feedback Unit (AFU).
This section shows the advantage of the HP 4142B by
reviewing
BJT measurements
as an example.
Present
biasing
difficulties
Figure
are as follows:
2. I .3
Drift
offer
Binsing
(1) Biasing
Point Drift
The usual S parameter
test set uses two independent
DC
bias sources to supply bias to the base and collector. By this
method (figure 2.1.2), the biasing points tend to drift due to
internal heating caused by current flows as shown in figure
2.1.3(a) . This is because Ie-Vbe characteristics
and HFE are
temperature
dependent (figure 2.1.3(b)).
Two independent
(2) Unexpected
Damage to Test Devices
Such high-frequency
devices can easily be damaged by spikes
during biasing.
Using the HP 4142B AFU with two SMUs solves these
problems. Figure 2.1.1 shows the HP 4142B test setup. SMUl
supplies Vce, and SMU2 supplies Vbe and Ib. SMUl monitors
the current, and the AFU operates SMUZ in response to the
monitored
current. Figure 2.1.4 shows a simplified feed back
loop to stabilize Ice. This method has the following
advantages:
(1) A stable biasing point that eliminates drift because the
AFU regulates IC to a steady specified value.
(2) A slew rate that is programmable
from 0.5 V/s to sokV/s
without spikes, thus preventing
device damage.
Using the HP 4142B
as shown in figure 2.1.1 enables reliable
measurements
up to f500mA
(limited by HP 85046.4).
Figure 2.1.5 shows an example of measuring the S
parameter by the method of biasing using the AFU and the
circuit in figure 2.1.1, then calculating fT from the measured
parameter.
Figure
2.1.7
S Pnmmeter
Mensurement
T,>To
Figure
8
AFU
Circuit
s parameter
HP4142B
Bins using
S
Figure 2.7.5
Test Set
(HP 85046A)
2.7.4
DUT
Measurement
Exnmple
(JT)
2.2 HP 4142B and External
Supplies
Power
The combination
of the HP 4142B
and an external power
supply can easily evaluate the characteristics
to 1 A or higher.
This section describes the method of evaluating
characteristics
of power devices by effectively combining
an external power
supply and the Analog Feedback Unit (AFU).
Figure 2.2.1 shows an example
of a measurement
circuit to
measure the gm and ON resistance of a power MOSFET by
the combination
of an external power supply with a maximum
current of 10 A (HP 6621A) and an HP 4142B. For this
measurement,
use an external power supply of the series
regulator type featuring
quick response. Measure a current by
measuring the voltage drop across external resistance Rs.
To set bias points Vds, Id for measuring gm, first use the
AFU to establish the gate bias Vgs that $es
bias point Id,
then apply voltage pulses of this Vgs to the gate (pulse width
1 ms). (Pulse mode measurement,
see figure 2.2.2.)
As for ON resistance, use the external power supply in the
current mode, measure Vds by the voltage monitor (VM) of
the HP 4142B, then calculate ON resistance as
External
HP4142B
Power
Supply
(2 IfJA)
HP662 I A
+
Sense(+)
SMU
t
,
AFU
Controller
HP 9000
Series
300
I ure
Fk
2.2.2
Sequence
of Gm
Mensurement
AI
gm=AV
Id
Ido+AI
Ido
---------
---_--------
0
r
Usina
AFU
2.3 Evaluation
of Solar Cell
Characteristics
2.4 Evaluation
of CMRR, PSRR, and
Open Loop Gain of an Opamp
Recently inexpensive
solar cells with high conversion
efficiency made of amorphous
silicon and other materials have
been developed and used in many fields.
The power SMU of the HP 4142B (200 VI1 A) enables easy
and quick evaluation
of V-I characteristics
of solar cells with a
maximum current up to 1 A.
Figure 2.3.1 shows a measurement
circuit for solar cells. The
circuit can be made up of just the 200 Vl1A range SMU and
GNDU. Expose a solar cell to light, increase the output
voltage of the SMU from 0 V, and measure the current IO
flowing from the solar cell to SMU (figure 2.3.2). The
measurements
yield the maximum power (Pmax) and
optimum voltage/current
(Voc) when the terminals are open,
and short-circuit
current (10~).
Figure
2.3.~
S&r
Cd
Mensurmrnt
Circuif
--
This section describes how to measure important
parameters
of an operational
amplifier (opamp), CMRR, PSRR and open
loop gain, using various sweep functions and highly accurate
measurement.
Figure 2.4.1 shows the opamp measurement
circuit. The
measurement
circuit uses the NULL AMP method. The
measurement
circuit uses two SMUs to supply power to the
opamp to be measured, one SMU to set its output voltage,
and VS/VMU
to measure the output voltage of the null amp.
CMRR Measurement
Operate the SMU used to supply power to the DUT to vary
the common-mode
voltage from -12 V to 12 V to DUT in the
synchronous
sweep mode as figure 2.4.2. Measure the nullamp output voltage Vo to obtain the change in input offset
voltage caused by the common-mode
voltage (figure 2.4.3).
The CMRR is obtained as
l
CMRR
= ($1&)
’
HP4142B
where
AVo: change in null-amp output
AVCO: change in common-mode
voltage
Figure 2.4.4 shows an example of measurements
TL071.
Note: See fhe sample program list on page 17.
JY
Light
of a
PSRR Measurement
PSRR is defined as the ratio of the change in input offset
voltage to the change in power supply voltage producing
it.
Vary the power supply voltage (+Vcc) from +5 V to S.5 V
in the synchronous
staircase sweep mode (figure 2.4.5).
Using the changes in input offset voltage thus obtained,
PSRR is calculated as
l
GNDU
I
I
F.
S
4
_
PSRR
Figure
2.3.2
Mtmuremm~ Result
E.rumpk
I,(A)
= (2
A)
’
where AVcc: change in power supply voltage
Figure 2.4.6 shows an example of measurements
TL071.
of a
Open Loop Gain Measurement
Vary the SMU3 output voltage to the DUT and obtain the
open loop gain from the resultant change in input voltage. In
other words, perform a staircase sweep of the SMU3 output
from -10 V to 10 V, and measure the input voltage. Then,
the open loop gain is calculated as
l
P=Vo.Io
Ad = (+$&)-’
where
change.
Figure
V,(V)
Figuw
AVr:
change
in DUT output
2.4.7 shows an example
2.4.7
OP
Amp
M~su~P~~IP~I~
5IK
10
voltage,
equal to SMU3
of measurements
Cirrrrif
(NULL
AMP
of a TL071.
Mdhorfl
v
2.5 Transient
Thermal
Measurements
Resistance
The thermal characterization
of power semiconductor
devices is important
for predicting
the reliability
and
performance
of these devices, and ensuring their safe
operation. This section gives information
about the transient
thermal resistance of bipolar power transistors and the
method for measuring
thermal resistance.
Usually, thermal resistance is defined as the ratio of the
applied power dissipation
to the temperature
rise at the
reference point. The temperature
rise is caused by thermal
conduction
from a heat source (PN junction). Therefore,
a
certain amount of time which is proportional
to the thermal
time constant, is required for the device to reach steady state.
The ratio of the temperature
rise to the applied power in the
transient state is defined as transient thermal resistance
(figure 2.5.1). Figure 2.5.2 shows the structure of a package
device. Component
parts are made of different
materials with
various masses and thus have different thermal resistances
and thermal time constants. Figure 2.5.3 shows an electric
circuit model of the device.
The concept of thermal resistance is based upon an analogy
between the electrical and thermal properties of materials,
with temperature,
power dissipation, and thermal resistance
being analogous to voltage, current, and electrical resistance
respectively. One of the aims of transient thermal resistance
measurement
is to ensure satisfactory contact
between the
silicon substrate and case. If the attachment
is nonuniform
and there are voids, the thermal resistance between the
substrate and case will be higher. This can be detected by
measuring
the transient thermal resistance between the
junction and the case.
Figure 2.5.4 shows the measurement
circuit. This example
uses two power SMUs (200 V/l A) and one GNDU. Power to
be applied to a device is set by the product of Vcs and Ir. Set
VCB with SMUl, and apply IE in the form of pulses with
SMU2. For example, with VCB = 20 V and IE = 0.7 A, peak
power is approx. 14 W.
To obtain the junction temperature
(Tj), use the
temperature
coefficient of VBE (approx. -2 mV/“C). To estimate
Tj, accurately, measure the temperature
coefficient at a certain
bias current (1~1) in advance.
In this example, VBEI is sampled N times by high speed spot
measurement
(figure
2.5.5) (“TV” commands are written to
program memory of the HP 4142B N times, and then
triggered.).
Bias (IEI) must be set such that power applied to a
device small. For example, set the bias to 1 mA.
Plot the VBE values thus obtained using fialong
the
horizontal
axis (figure 2.5.6). In the range of small t, the plot
forms a straight line. Obtain VBE at t 0 by drawing an
asymptotic line. Subtract VBE before applying pulses from the
value of VBE thus obtained, then divide by the temperature
coefficient of VBE to obtain the junction temperature
rise.
where
12
K: temperature
coefficient
of VBE
From the temperature
rise of this junction and applied
power dissipation
(14 W), transient thermal resistance Rth (t)
for the pulse width used in this measurement
is obtained as
Rth (t) =+
Figures 2.5.6 and 2.5.7 show actual measurements
of a
power transistor with I,,,, = 10 A and I’,,,, = 150 W.
Note:
See the sample
program
2.5.7
Figure
78.
list on page
Temperature
Rise after
Forcing
Power
I
AT
t
I
Figure
R,,(t)
= +
c-----
2.5.2
Steady-state
Rise
Packngd
Device
Structure
and Thermal
I-
Cirruif
: Junction
T&t
: Attachment
Ta
Constant
Time/
Model
Tj
T-se:
Time
i Thermal
I
Fipm 2.5.3
Temperature
Case
: Ambient
Temperature
Temperature
Temperature
Temperature
2.6
Dielectric
Absorption
Measurements
When using a capacitor in circuits requiring
high accuracy,
such as S/H circuits and integrator
circuits, dielectric
absorption
must be taken into consideration.
This section
describes how to measure dielectric absorption.
Figure 2.6.1 (a) shows the principle measurement
diagram.
Capacitor Cx to be tested is charged for time t at constant
voltage, is discharged (short circuit) for the same time t, then
is disconnected
from the circuit (figure 2.6.1 (b)). After such
an operation,
the capacitor terminal voltage usually increases.
This is because an actual capacitor does not have an ideal
capacitance and there exist dielectric absorption
elements (Cl,
RI, C2, R2) as represented
in figure 2.6.2.
Figure 2.6.3 shows an actual measurement
circuit using an
HP 4142B.
The measurement
circuit setup is very simple
because the SMU serves as a voltage source for charging and
discharging
and as a voltmeter when the capacitor is
disconnected
(open
circuit).
Set the SMU using the following
procedure. First, set the
SMU to operate as a 10 V voltage source for time t to charge
the capacitor.
Next, set the SMU as a 0 V voltage source for the same
time t to discharge the capacitor. Then, set the SMU to act as
a voltmeter
(current compliance OA) and sample the voltage N
times by high speed spot measurement
(figure 2.6.4). For
quicker measurement,
write N “TV” commands to the
HP 4142B program
memory.
Figure 2.6.5 shows an example of measurements,
a test of a
0.01 UF ceramic capacitor and a 0.01 uF polyester film
capacitor. It can be seen from this example that the dielectric
absorption
characteristic
of a ceramic capacitor is very poor.
Figure
Dielectric
2.6.7
Absorption
Measurement
Figure
Principle
Vs
VC
AVa
t
0
0
---*t
SW
Dielectric
(b)
14
Lf ------
a
Absorption
(DA)
Definition
b
c
= T
x 100 (%)
of Dielectric
Absorption
Equimlent
Cirruif
absoption
Figure
fvfensuremen~
2.6.3
elements
Cirruit
SMU
t;
CX
<
GNDU
Figure 2.6.4
Programming
Example
200
OUTPUT
210
WAIT
220
OUTPUT
230
WAIT
240
OUTPUT
@ DSM ; “D I2.0.0.3”
240
OUTPUT
@DSM
Finure
(a) Measurement
Cnpnrifor
2.6.2
@ DSM ; “DV2.0,
IO”
0. I
@DSM
; “DV2.0.0”
0. I
2.6.5
:“DO
Mensurement
I”
Results
2.7 Simplified
Capacitance
Measurements using the AFU
The HP 4142B does not have the capability of measuring
capacitance using AC signals, but it enables measuring
a
capacitance ranging from 10 pF to 10 nF or so by the DC
method using a precision low current source. This section
describes a simplified capacitance measuring method using the
AFU as a timer for time measurement.
Figure 2.7.1 (a) shows the principle of measurement.
When
constant current IO is applied to capacitance Cx, terminal
voltage Vc increases linearly at a gradient of IolCx (figure
2.7.1(b)).
The terminal voltage at time ti, therefore,
can be
calculated as
Figure 2.7.1 C Mensuremt-nt Prinriple
(a) Measurement
Principle
vc
Vc(t ) =$
’ Cx’
One of the two following
methods can be used to obtain Cx:
1. With charging current 10 and charging time ti given, the
terminal voltage at ti is measured to obtain Cx.
2. With charging current IO and terminal voltage given, ti is
measured to obtain Cx.
In method 1, there are two ways of setting the charging
time: one is to use current pulses and set the pulse width, and
the other is to use the system controller’s
timer. The
disadvantage
of using current pulses is that the range of
current pulses (100 PA min, B 20 V range) has a lower limit.
The disadvantage
of using the system controller’s
timer is
that there is a difference in time resolution
with various
models. This section describes an example of capacitance
measurement
by method 2. This method uses the AFU as a
timer for measuring
ti.
Figure 2.7.2 shows
an example of an actual measurement
circuit. Use SMUl as a sense SMU, and SMU2 as a search
SMU. Keep the output of the SMU2 disconnected. The AFU
is used in the ramp mode only. First, set charging current IO,
target voltage Vet and ramp speed RS, then trigger the
measurement.
(Set the hold time, delay time, and feedback
integration
time to 0, 0, and minimum
respectively.)
Figure 2.7.3 shows the change in outputs from SMUl and
SMU2. Charging
time ti is obtained by measuring Vs as
-
VS
t1 =Jg
Then,
Cx is obtained
Fi,qure 2.7.2
Voltage
Mensuremenf
Circuil
SMU I
AFU
as
cx=AsL
-Iovs
Vet t’ - Vet RS
Although
the hold time is set to 0, preprocessing
by the AFU
causes a time lag (4 ms to 3 ms) between rise of charging
current and start of ramp voltage. To minimize the error
caused by this time lag,make the charging time at least 40-50
ms by adjusting Vs and RS.
The measurement
range of this method is expressed as
- lOnF
*lo%
(t B 50ms, Vet = lOV, 10 = 1nA--IpA)
Note: See the sample program list on page 19.
-
of Terminal
SMUZ
capacitance
C= lopF
(b) Change
GNDU
Figure 2.7.3
AFU-R&ted
Wmeforms
2.8 Noise Evaluation
by FFT Analysis
The precision measurement
performance
of the HP 4142B
(17-bit accuracy) and improved
time resolution
(1 ms) enable
fast Fourier transform
(FFT) analysis with a maximum
frequency of 400 Hz and dynamic range of 80 dB or more.
This section describes how to evaluate the noise
characteristics
of an opamp by FFT analysis using high-speed
spot measurements.
Figure 2.8.1 shows the measurement
circuit. Set the gain of
the opamp to 1000x,
connect a low-pass filter to the output to
prevent Aliasing effect, and connect the VSIVMU.
Write N “TV” commands to the HP 4142B program memory
to enable trigger measurements
and sampling to be done at
maximum speed. The sampling interval ts should be about 1.2
ms (figure 2.8.2). Make the number of sampling points a
power of 2 for convenience
in FFT operation.
(N=512
maximum because of HP 4142B data memory capacity in
ASCII Data format)
Weight the obtained data by a proper window function
Hanning, etc. and then perform the FFT.
The results obtained are in the form of a complex number,
and the power is the sum of squares. Divide it by the
maximum frequency resolution
(corresponding
to the filter
width) to obtain the power spectrum density. (This value is
independent
of the number of sampling points N and interval
ts.)
Figure 2.8.3 shows an example of measurements.
This graph
shows the noise characteristics
of a TL071
FET opamp. The
average noise level at 100 Hz and above is about 20-30
nV/Hz.
Note:
See the sample
program
lisf on pages LO-2
1,
References
1. Siliconix Inc: [MOSPOWER
Application]
2. S. Takagi et al: [Programmable
Stimulus/
Measurement
Units Simplify Device
HP Journal, October 1982, P15-20
3. S. Rubin et al: [Thermal Resistance
Measurement
on Power Transistors]
NBS 400-14
16
Test Setups]
Figure
I
2.8.1
No&
Mmsurmen~
Circuit
51K
Figure-
2.8.2
Sntnpling
Timing
,Sampling
Point
ts = I .2ms
Figure
2.8.3
Measuremenf
Results