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Gaurav Saxena, Rekha Agrawal, Sandhya Sharma / International Journal of Engineering
Research and Applications (IJERA) ISSN: 2248-9622 www.ijera.com
Vol. 3, Issue 4, Jul-Aug 2013, pp.2171-2175
2171 | P a g e
Single Event Upset (SEU) in SRAM
Gaurav Saxena1
, Rekha Agrawal2
, Sandhya Sharma3
1, 2, 3
Department of Electronics and Communication, Suresh Gyan Vihar University, Jaipur
ABSTRACT
Radiation in space is potentially
hazardous to microelectronic circuits and systems
such as spacecraft electronics. Transient effects on
circuits and systems from high energetic particles
can interrupt electronics operation or crash the
systems. This phenomenon is particularly serious
in complementary metal-oxide-semiconductor
(CMOS) integrated circuits (ICs) since most of
modern ICs are implemented with CMOS
technologies. The problem is getting worse with
the technology scaling down. Radiation-
hardening-by-design (RHBD) is a popular method
to build CMOS devices and systems meeting
performance criteria in radiation environment.
Single-event transient (SET) effects in digital
circuits have been studied extensively in the
radiation effect community.
The goal of this research is the implementation of
a radiation hardened MOS devices using ORCAD
that is able to accurately compute in the presence
of radiation induced SEUs. This research
specifically concentrates on the ability of the
system to detect and mark or correct SEUs in
semiconductor memory systems. This work does
not address error detection and correction
(EDAC) of memory systems. It only address the
areas where fault can be likely found in MOS
based devices and then make a circuit which
perfectly work in radiation environment too.
Keywords- linear energy transfer (LET), single
event upset (SEU), single event error (SEE), single
event transient (SET)
I. INTRODUCTION
In microelectronics, Single-event effects can
cause changes in memory state in space borne,
airborne, and even terrestrial electronics. They are
result of charge collection from a radiation particle
strike. Since the sensitivity of microelectronics to
single-event upset is expected to increase as
technology scaling continues, therefore single event
effects are a severe problem nowadays. In
complementary metal-oxide-semiconductor (CMOS)
transistor technology, single event effects are a key of
research interest. As devices are downscaled, a
reduction in the amount of charge held on memory
storage nodes increases CMOS vulnerability to
single-event upset.
Single Event Effects (SEE) are caused by the
interaction of ionizing particles with semiconductor
devices. The passing of an ionizing particle through a
semiconductor device generates electron-hole pairs
(ehps) along the track path and may be collected at
the terminals of a device. Linear Energy Transfer
(LET) is defined as the energy loss per unit path
length, normalized by the density of the material.
LET has units of MeV/mg/cm2
. A calculation of the
charge deposited per unit length can be determined if
the LET of the ion, average energy needed to create
an ehp for a material, and density of the material are
known [1]. For silicon, an ion with a LET of 97
MeV/mg/cm2 will deposit 1pC of charge per micron
length of the ion track [2].
The charge collection process in
semiconductor devices normally occur in reversed
biased p/n junctions due to the presence of the high
electric field in the reverse-biased junction depletion
region (drift collection). Diffusion collection process
is due to the presence of carriers outside of the
depletion region that can diffuse back toward the
junction. Bipolar amplification process is another
collection mechanism. This collection mechanism is
due to a lowering of the body potential and turns-on
of a parasitic bipolar transistor for CMOS submicron
technologies [3] Single Event Upsets (SEU) occur
when the SEE leads to a logic gate switch, voltage
transients, or alteration of stored information. The
first reported instance of SEU was in 1975 by Binder,
et al [4].
SEUs don’t just happen in deep space or
when high levels of radiation are present. The same
cosmic rays that warm the earth's atmosphere carry
energetic particles that cause upsets in earth-based
equipment. In 1979, James Ziegler of IBM and W.A.
Lanford first described how terrestrial cosmic rays
could cause single event upsets in electronics. Over
the next 15 years, IBM, led by Ziegler, continued to
study SEUs, finding that while the rate of upset
decreases as altitudes approach sea level, on average,
every device – such as an image (memory cell) in a
digital camera – experiences an SEU approximately
once a year. Because this is the average, it’s
reasonable to expect that some cameras may
experience no upsets in a one year period while
others may experience multiple instances. In addition
to IBM, other companies including Motorola have
studied SEUs extensively. Their findings have
determined additional causes of upsets here on Earth,
such as power glitches, Alpha particles, impurities in
chips, software bugs, product quality. The number of
upsets has been found to increase as the amount of
Gaurav Saxena, Rekha Agrawal, Sandhya Sharma / International Journal of Engineering
Research and Applications (IJERA) ISSN: 2248-9622 www.ijera.com
Vol. 3, Issue 4, Jul-Aug 2013, pp.2171-2175
2172 | P a g e
storage capacity of the affected devices increases.
Therefore, as memory capacities have multiplied
significantly over the years, the number of SEUs in
those devices has also increased .
II. SENSITIVE NODES
In CMOS circuits, the “off” transistors
struck by a heavy ion in the junction area are most
sensitive to single event upset (SEU) by particles
with high enough LET (linear energy transfer) of
around 20 MeV-cm2
/mg. which is shown in (fig 1).
Figure 1: Diagram of critical nodes within an
FPGA circuit [6].
When these particles hit the silicon bulk, the
minority carriers are created and if collected by the
source drain diffusion regions, the change of the
voltage value of those nodes occurs. The induced
transient voltage pulse may propagate through
several of logic gates. Because a particle can induce
an SEU when it strikes either the channel region of
an off NMOS transistor or the drain region of an off
PMOS transistor, we will consider the strike at an off
PMOS drain area.
A particles can induce SEU when it strikes
at the channel region of an off NMOS transistor or
the drain region of an off PMOS transistor. The
ionization can induce a current pulse in a p-n
junction. A schematic view of how the SEE induced
current pulse translate into an SEE induced voltage
pulse is given in figure1.
The amount of charge deposited per unit time is
therefore quantified as the linear energy transfer
(LET). As the amount of charge deposited by a
radiation strike is directly proportional to the Let (L)
and charge collection depth (t) which is seen in the
following equation.
Q=0.01036.L.t (1)
Here L is expressed in MeV-cm2
/mg, t in
microns, and Q in pC. For example, an alpha particle
with 5 MeV-cm2
/mg LET deposits around 50fC/µm
[3]. The minimum amount of deposited charge that is
required to cause an SEU is defined as critical charge
(Qcrit). Additionally, the probability distribution of
energetic particles drops off rapidly with increasing
LETs [6]. The largest population of particles have an
LET of 20MeV-cm2
/mg or less, and particles with an
LET greater than 30MeV-cm2
/mg are exceedingly
rare [4]. The current pulse that results from a
particles strike is traditionally describe as a double
exponential function. The radiation particles strike is
modeled by
current pulse as
(2)
Here Q is the amount of charge collected as a result
of the ion strike, while τα is the collection time
constant for the junction and is the ion track
establishment constant. Time constant and
depends upon several process related parameters, and
typically is on the order of 100ps and is on the
order of tens of picoseconds. In our experiments, we
have used Q=150pC, =150ps and =38ps. The
radiation induced current always flows from n-
diffusion to p-diffusion.
Single event upsets are events in which an
incident particle can strike key node within a device
(Fig2)
Figure 2: SEU in memory cell due to a heavy ion
strike.
resulting in a local ionization that can cause a state
change in a bit with sufficient voltage [3].
Experiments with similar device types have shown
that the minimum free charge required to change the
state of a logic cell is approximately 100 fC. Given
that the average energy to create an electron-hole pair
in the Silicon is 3.6 eV and the average thickness of
an active volume of a device is on the order of 2 μm,
an ionization of 1 MeV μm is required - well beyond
the average ionizing energy loss of protons (where
dE dX ≈ 40keV μm at an energy of 1 MeV) [20].
Thus, upsets are associated primarily with ion strikes
in the Silicon which result in the creation of heavier
secondary fragments such as (Figure 3.1) and
through elastic collisions with the Silicon nuclei
(Figure 3.2) which result in nuclear “recoils”, leaving
a local trail of heavy ionization [3, 4]. Experimental
testing by Xilinx at Texas A&M University with their
radiation-tolerant devices has yielded SEU (and other
Gaurav Saxena, Rekha Agrawal, Sandhya Sharma / International Journal of Engineering
Research and Applications (IJERA) ISSN: 2248-9622 www.ijera.com
Vol. 3, Issue 4, Jul-Aug 2013, pp.2171-2175
2173 | P a g e
fault condition) cross-sections for configuration logic
bits for protons and heavy ions [4].
Electron-hole pair is generated when
radiation is incident on silicon substrate as shown in
figure and SEU effect is induces in the device.
Figure (3.1)
Figure(3.2)
Figure 3: Electron –hole pair tracks from an
alpha particles strike through (3.1) an n+
in P-
substrate junction, and through (3.2) a p+
in n-well
junction where truncation of the collected charge
occurs.
In CMOS circuits, the “off” transistors
struck by a heavy ion in the junction area are most
sensitive to SEU by particles with high enough LET
(linear energy transfer) of around 20 MeV-cm2
/mg.
When these particles hit the silicon bulk, the minority
carriers are created and if collected by the
source/drain diffusion regions, the change of the
voltage value of those nodes occurs. The induced
transient voltage pulse may propagate through
several levels of logic gates [6]. Because a particle
can induce an SEU when it strikes either the channel
region of an off NMOS transistor or the drain region
of an off PMOS transistor, we will consider the strike
at an off PMOS drain area [10].
A particle can induce SEU when it strikes at
the channel region of an off NMOS transistor or the
drain region of an off PMOS transistor. The
ionization can induce a current pulse in a p-n
junction.
A schematic view of how the SEE induced current
pulse translates into an SEE induced voltage pulse is
given in Figure 3.
Figure 4: Generation of SEE induced voltage
pulse
Due to reduction of feature size the SEUs play an
increasing role in failures observed during operation
of digital circuits, particularly in environments with
remarkable rediation level (avionics, nuclear, high
energy, physics instrumentation etc.). in a few years
SEUs will significantly affect the digital electronics
not only in this special radiation environment but at
the normal operating conditions as well. Therefore
the counter measure against SEUs gains importance
as technology feature size drops down [5]. The
electronic sysyem can be build using radiation-
hardened semiconductor devices but they skyrocket
the system cost.
Most other circuit level approaches model the effect
of a particle strike[12] with the help of a transient
current source as shown in figure
Figure 5: Particles strike modeled by a
transient current source
A common approximation to determine the
current slope I(t) is the double exponential function
in equation [15]. Here τα is the collection time-
constant of the p-n junction and τβ denotes the time
constant for establishing the electron-hole track. An
alternative model is given by formula with
parameters Q, t and K, where q is the collectiod
charge, t is a pulse shaping parameter and K is a
constant [14].
(3)
(4)
Gaurav Saxena, Rekha Agrawal, Sandhya Sharma / International Journal of Engineering
Research and Applications (IJERA) ISSN: 2248-9622 www.ijera.com
Vol. 3, Issue 4, Jul-Aug 2013, pp.2171-2175
2174 | P a g e
simplification is appropriate for modeling diffusion,
but charge collection by drift depends on the electric
field strength, and thus on the voltage.
III. Modeling and simulation of SRAM
Using VPULSE input signal source, having
value, V1=0V, V2=5V, TD=0, TR=1m, TF=1m,
PW=5m, PER=10m, the WORD line is connected to
high voltage level, due to this MOS transistor Q5
and Q6 are ON
Figure 6: Modeling of 6t SRAM cell in ORCAD
PSPICE 16.5
In this figure 6, BIT and BITBAR are
complement to each other which is the basic working
of the SRAM cell [6,7,8,9,10,11]. The following
figure is a simulation waveform (ORCAD PSPICE
16.5) of schematic of 6 transistor SRAM cell
Figure 7: Simulation result of 6t SRAM cell
The figure shows voltage status at the two
output level BIT and BITBAR, which is complement
to each other (according to the working of SRAM)
[9]. The green line show the voltage level of
BITBAR and red line show the voltage level of BIT
which is complement to each other.
Figure 8: SEU effect on 6t SRAM by injecting
current source
In this figure SEU effect is injecting by
parallel connection of current source to the NMOS
which is OFF due to this the desired output is not
available [3].
Figure 9: Simulation of figure, injecting SEU
effect in SRAM cell
The figure shows that the value of BIT and
BITBAR are equal. The green line which show the
voltage level of BITBAR are overlap to red line
which show the voltage level of BIT.
To remove this SEU effect the radiation hardened
circuit of full SRAM is used which is shown below.
Figure 10: Modeling of Radiation Hardened 6t
SRAM cell in ORCAD PSPICE 16.5 [5]
Gaurav Saxena, Rekha Agrawal, Sandhya Sharma / International Journal of Engineering
Research and Applications (IJERA) ISSN: 2248-9622 www.ijera.com
Vol. 3, Issue 4, Jul-Aug 2013, pp.2171-2175
2175 | P a g e
In this circuit current source is still
connected in the circuit but some other changes is
used to removed the radiation effect which is cause
by the injecting current source parallel to the NMOS
[3].
The figure shows that, due to the use of
radiation hardened circuit , SEU effect is almost
removed in SRAM and the circuit resumes its actual
behaviour which is reflect in the resultant waveform,
in which BITBAR and BIT are complement to each
other.
Figure 11: Simulation waveform of SRAM
hardened circuit.
IV. Conclusion
In this paper we see how we can induced single event
upset in SRAM and how we can remove it using
radiation hardened circuit. Radiation hardened circuit
is used to protect your digital device from radiation
effect. But the radiation hardened circuit is complex
so this is the limitation of this project.
REFERENCES
Journal Papers:
[1] L. W. Massengill, “SEU modeling and
prediction techniques,” in IEEE NSREC
Short Course, 1993, pp. III-1–III-93
[2] P. E. Dodd and L. W. Massengill, “Basic
mechanisms and modeling of single-event
upset in digital microelectronics,” IEEE
Trans. Nucl. Sci., vol. 50, pp. 583–602, June
2003.
[3] J. S. Fu, C. L. Axness, and H. T. Weaver,
“Memory SEU simulations using 2-D
transport calculations,” IEEE Electron.
Device Lett., vol. 6, pp. 422–424, Aug. 1985.
[4] D. Binder, E.C. Smith, and A. B. Holman,
“Satellite anomalies from galactic cosmic
rays,” IEEE Trans. Nucl. Sci., vol. 22, pp.
2675-2680, Dec. 1975.
[5] K. Hirose et al. SEU resistance in advanced
SOI-SRAMs fabricated by commercial
technology using a rad-hard circuit design.
IEEE Transactions on Nuclear Science,
49(6), 2002.
[6] Joseph J. Fabula and Austin Lesea. The
NSEU response of static latch based FPGAs.
In MAPLD 2003, Washington, D.C.,
September 2003. Military and Aerospace
Programmable Logic Devices International
Conference. Paper C5.
[7] F. Vargas and M. Nicolaidis, “Seu - tolerant
sram design based on current monitoring,”
Fault-Tolerant Computing, 1994. FTCS-24.
Digest of Papers., pp. 106–115, 1994.
[8] P. C. Murley and G. R. Srinivasan, “Soft-
error monte carlo modeling program,
semm,” IBM J. RES. DEVELOP.,vol. 40,
no. 1, pp. 109–118, 1996.
[9] P. Hazucha, K. Johansson, and C. Svensson,
“Neutron induced soft errors in cmos
memories under reduced bias,” IEEE
Transactions on Nuclear Science, vol. 45,
no. 6, pp. 2921–2928, 1998.
[10] L. Anghel and M. Nicolaidis, “Cost
reduction and evaluation of a temporary
faults detecting technique,” Design,
Automation and Test in Europe Conference
and Exhibition 2000, pp. 591–598, 2000.
[11] G. C. Messenger, “Collection of charge on
junction nodes from ion tracks,” IEEE
Transactions on Nuclear Science, vol. 29,
no. 6, pp. 2024–2031, 1982.
[12] C. Hsieh and P. Murley, “A field-funneling
effect on the collection of alpha-particle-
generated carriers in silicon devices,” IEEE
Electron Device Letters, Vol. 2, No. 4, pp.
103-105, 1981.
[13] L. Freeman, “Critical charge calculations for
a bipolar SRAM array,” IBM Journal of
Research and Development, Vol. 40, No. 1,
pp. 119-129, 1996.
[14] K. Clark, et al., “Modeling single-event
effects in a complex digital device,” IEEE
Trans. on Nuclear Science, Vol. 50, No. 6,
pp. 2069-2080, 2003.
[15] G. Messenger, “Collection of charge on
junction nodes from ion tracks,” IEEE
Trans. on Nuclear Science, Vol. 29, No. 6,
pp. 2024-2031, 1982.

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Mc3421712175

  • 1. Gaurav Saxena, Rekha Agrawal, Sandhya Sharma / International Journal of Engineering Research and Applications (IJERA) ISSN: 2248-9622 www.ijera.com Vol. 3, Issue 4, Jul-Aug 2013, pp.2171-2175 2171 | P a g e Single Event Upset (SEU) in SRAM Gaurav Saxena1 , Rekha Agrawal2 , Sandhya Sharma3 1, 2, 3 Department of Electronics and Communication, Suresh Gyan Vihar University, Jaipur ABSTRACT Radiation in space is potentially hazardous to microelectronic circuits and systems such as spacecraft electronics. Transient effects on circuits and systems from high energetic particles can interrupt electronics operation or crash the systems. This phenomenon is particularly serious in complementary metal-oxide-semiconductor (CMOS) integrated circuits (ICs) since most of modern ICs are implemented with CMOS technologies. The problem is getting worse with the technology scaling down. Radiation- hardening-by-design (RHBD) is a popular method to build CMOS devices and systems meeting performance criteria in radiation environment. Single-event transient (SET) effects in digital circuits have been studied extensively in the radiation effect community. The goal of this research is the implementation of a radiation hardened MOS devices using ORCAD that is able to accurately compute in the presence of radiation induced SEUs. This research specifically concentrates on the ability of the system to detect and mark or correct SEUs in semiconductor memory systems. This work does not address error detection and correction (EDAC) of memory systems. It only address the areas where fault can be likely found in MOS based devices and then make a circuit which perfectly work in radiation environment too. Keywords- linear energy transfer (LET), single event upset (SEU), single event error (SEE), single event transient (SET) I. INTRODUCTION In microelectronics, Single-event effects can cause changes in memory state in space borne, airborne, and even terrestrial electronics. They are result of charge collection from a radiation particle strike. Since the sensitivity of microelectronics to single-event upset is expected to increase as technology scaling continues, therefore single event effects are a severe problem nowadays. In complementary metal-oxide-semiconductor (CMOS) transistor technology, single event effects are a key of research interest. As devices are downscaled, a reduction in the amount of charge held on memory storage nodes increases CMOS vulnerability to single-event upset. Single Event Effects (SEE) are caused by the interaction of ionizing particles with semiconductor devices. The passing of an ionizing particle through a semiconductor device generates electron-hole pairs (ehps) along the track path and may be collected at the terminals of a device. Linear Energy Transfer (LET) is defined as the energy loss per unit path length, normalized by the density of the material. LET has units of MeV/mg/cm2 . A calculation of the charge deposited per unit length can be determined if the LET of the ion, average energy needed to create an ehp for a material, and density of the material are known [1]. For silicon, an ion with a LET of 97 MeV/mg/cm2 will deposit 1pC of charge per micron length of the ion track [2]. The charge collection process in semiconductor devices normally occur in reversed biased p/n junctions due to the presence of the high electric field in the reverse-biased junction depletion region (drift collection). Diffusion collection process is due to the presence of carriers outside of the depletion region that can diffuse back toward the junction. Bipolar amplification process is another collection mechanism. This collection mechanism is due to a lowering of the body potential and turns-on of a parasitic bipolar transistor for CMOS submicron technologies [3] Single Event Upsets (SEU) occur when the SEE leads to a logic gate switch, voltage transients, or alteration of stored information. The first reported instance of SEU was in 1975 by Binder, et al [4]. SEUs don’t just happen in deep space or when high levels of radiation are present. The same cosmic rays that warm the earth's atmosphere carry energetic particles that cause upsets in earth-based equipment. In 1979, James Ziegler of IBM and W.A. Lanford first described how terrestrial cosmic rays could cause single event upsets in electronics. Over the next 15 years, IBM, led by Ziegler, continued to study SEUs, finding that while the rate of upset decreases as altitudes approach sea level, on average, every device – such as an image (memory cell) in a digital camera – experiences an SEU approximately once a year. Because this is the average, it’s reasonable to expect that some cameras may experience no upsets in a one year period while others may experience multiple instances. In addition to IBM, other companies including Motorola have studied SEUs extensively. Their findings have determined additional causes of upsets here on Earth, such as power glitches, Alpha particles, impurities in chips, software bugs, product quality. The number of upsets has been found to increase as the amount of
  • 2. Gaurav Saxena, Rekha Agrawal, Sandhya Sharma / International Journal of Engineering Research and Applications (IJERA) ISSN: 2248-9622 www.ijera.com Vol. 3, Issue 4, Jul-Aug 2013, pp.2171-2175 2172 | P a g e storage capacity of the affected devices increases. Therefore, as memory capacities have multiplied significantly over the years, the number of SEUs in those devices has also increased . II. SENSITIVE NODES In CMOS circuits, the “off” transistors struck by a heavy ion in the junction area are most sensitive to single event upset (SEU) by particles with high enough LET (linear energy transfer) of around 20 MeV-cm2 /mg. which is shown in (fig 1). Figure 1: Diagram of critical nodes within an FPGA circuit [6]. When these particles hit the silicon bulk, the minority carriers are created and if collected by the source drain diffusion regions, the change of the voltage value of those nodes occurs. The induced transient voltage pulse may propagate through several of logic gates. Because a particle can induce an SEU when it strikes either the channel region of an off NMOS transistor or the drain region of an off PMOS transistor, we will consider the strike at an off PMOS drain area. A particles can induce SEU when it strikes at the channel region of an off NMOS transistor or the drain region of an off PMOS transistor. The ionization can induce a current pulse in a p-n junction. A schematic view of how the SEE induced current pulse translate into an SEE induced voltage pulse is given in figure1. The amount of charge deposited per unit time is therefore quantified as the linear energy transfer (LET). As the amount of charge deposited by a radiation strike is directly proportional to the Let (L) and charge collection depth (t) which is seen in the following equation. Q=0.01036.L.t (1) Here L is expressed in MeV-cm2 /mg, t in microns, and Q in pC. For example, an alpha particle with 5 MeV-cm2 /mg LET deposits around 50fC/µm [3]. The minimum amount of deposited charge that is required to cause an SEU is defined as critical charge (Qcrit). Additionally, the probability distribution of energetic particles drops off rapidly with increasing LETs [6]. The largest population of particles have an LET of 20MeV-cm2 /mg or less, and particles with an LET greater than 30MeV-cm2 /mg are exceedingly rare [4]. The current pulse that results from a particles strike is traditionally describe as a double exponential function. The radiation particles strike is modeled by current pulse as (2) Here Q is the amount of charge collected as a result of the ion strike, while τα is the collection time constant for the junction and is the ion track establishment constant. Time constant and depends upon several process related parameters, and typically is on the order of 100ps and is on the order of tens of picoseconds. In our experiments, we have used Q=150pC, =150ps and =38ps. The radiation induced current always flows from n- diffusion to p-diffusion. Single event upsets are events in which an incident particle can strike key node within a device (Fig2) Figure 2: SEU in memory cell due to a heavy ion strike. resulting in a local ionization that can cause a state change in a bit with sufficient voltage [3]. Experiments with similar device types have shown that the minimum free charge required to change the state of a logic cell is approximately 100 fC. Given that the average energy to create an electron-hole pair in the Silicon is 3.6 eV and the average thickness of an active volume of a device is on the order of 2 μm, an ionization of 1 MeV μm is required - well beyond the average ionizing energy loss of protons (where dE dX ≈ 40keV μm at an energy of 1 MeV) [20]. Thus, upsets are associated primarily with ion strikes in the Silicon which result in the creation of heavier secondary fragments such as (Figure 3.1) and through elastic collisions with the Silicon nuclei (Figure 3.2) which result in nuclear “recoils”, leaving a local trail of heavy ionization [3, 4]. Experimental testing by Xilinx at Texas A&M University with their radiation-tolerant devices has yielded SEU (and other
  • 3. Gaurav Saxena, Rekha Agrawal, Sandhya Sharma / International Journal of Engineering Research and Applications (IJERA) ISSN: 2248-9622 www.ijera.com Vol. 3, Issue 4, Jul-Aug 2013, pp.2171-2175 2173 | P a g e fault condition) cross-sections for configuration logic bits for protons and heavy ions [4]. Electron-hole pair is generated when radiation is incident on silicon substrate as shown in figure and SEU effect is induces in the device. Figure (3.1) Figure(3.2) Figure 3: Electron –hole pair tracks from an alpha particles strike through (3.1) an n+ in P- substrate junction, and through (3.2) a p+ in n-well junction where truncation of the collected charge occurs. In CMOS circuits, the “off” transistors struck by a heavy ion in the junction area are most sensitive to SEU by particles with high enough LET (linear energy transfer) of around 20 MeV-cm2 /mg. When these particles hit the silicon bulk, the minority carriers are created and if collected by the source/drain diffusion regions, the change of the voltage value of those nodes occurs. The induced transient voltage pulse may propagate through several levels of logic gates [6]. Because a particle can induce an SEU when it strikes either the channel region of an off NMOS transistor or the drain region of an off PMOS transistor, we will consider the strike at an off PMOS drain area [10]. A particle can induce SEU when it strikes at the channel region of an off NMOS transistor or the drain region of an off PMOS transistor. The ionization can induce a current pulse in a p-n junction. A schematic view of how the SEE induced current pulse translates into an SEE induced voltage pulse is given in Figure 3. Figure 4: Generation of SEE induced voltage pulse Due to reduction of feature size the SEUs play an increasing role in failures observed during operation of digital circuits, particularly in environments with remarkable rediation level (avionics, nuclear, high energy, physics instrumentation etc.). in a few years SEUs will significantly affect the digital electronics not only in this special radiation environment but at the normal operating conditions as well. Therefore the counter measure against SEUs gains importance as technology feature size drops down [5]. The electronic sysyem can be build using radiation- hardened semiconductor devices but they skyrocket the system cost. Most other circuit level approaches model the effect of a particle strike[12] with the help of a transient current source as shown in figure Figure 5: Particles strike modeled by a transient current source A common approximation to determine the current slope I(t) is the double exponential function in equation [15]. Here τα is the collection time- constant of the p-n junction and τβ denotes the time constant for establishing the electron-hole track. An alternative model is given by formula with parameters Q, t and K, where q is the collectiod charge, t is a pulse shaping parameter and K is a constant [14]. (3) (4)
  • 4. Gaurav Saxena, Rekha Agrawal, Sandhya Sharma / International Journal of Engineering Research and Applications (IJERA) ISSN: 2248-9622 www.ijera.com Vol. 3, Issue 4, Jul-Aug 2013, pp.2171-2175 2174 | P a g e simplification is appropriate for modeling diffusion, but charge collection by drift depends on the electric field strength, and thus on the voltage. III. Modeling and simulation of SRAM Using VPULSE input signal source, having value, V1=0V, V2=5V, TD=0, TR=1m, TF=1m, PW=5m, PER=10m, the WORD line is connected to high voltage level, due to this MOS transistor Q5 and Q6 are ON Figure 6: Modeling of 6t SRAM cell in ORCAD PSPICE 16.5 In this figure 6, BIT and BITBAR are complement to each other which is the basic working of the SRAM cell [6,7,8,9,10,11]. The following figure is a simulation waveform (ORCAD PSPICE 16.5) of schematic of 6 transistor SRAM cell Figure 7: Simulation result of 6t SRAM cell The figure shows voltage status at the two output level BIT and BITBAR, which is complement to each other (according to the working of SRAM) [9]. The green line show the voltage level of BITBAR and red line show the voltage level of BIT which is complement to each other. Figure 8: SEU effect on 6t SRAM by injecting current source In this figure SEU effect is injecting by parallel connection of current source to the NMOS which is OFF due to this the desired output is not available [3]. Figure 9: Simulation of figure, injecting SEU effect in SRAM cell The figure shows that the value of BIT and BITBAR are equal. The green line which show the voltage level of BITBAR are overlap to red line which show the voltage level of BIT. To remove this SEU effect the radiation hardened circuit of full SRAM is used which is shown below. Figure 10: Modeling of Radiation Hardened 6t SRAM cell in ORCAD PSPICE 16.5 [5]
  • 5. Gaurav Saxena, Rekha Agrawal, Sandhya Sharma / International Journal of Engineering Research and Applications (IJERA) ISSN: 2248-9622 www.ijera.com Vol. 3, Issue 4, Jul-Aug 2013, pp.2171-2175 2175 | P a g e In this circuit current source is still connected in the circuit but some other changes is used to removed the radiation effect which is cause by the injecting current source parallel to the NMOS [3]. The figure shows that, due to the use of radiation hardened circuit , SEU effect is almost removed in SRAM and the circuit resumes its actual behaviour which is reflect in the resultant waveform, in which BITBAR and BIT are complement to each other. Figure 11: Simulation waveform of SRAM hardened circuit. IV. Conclusion In this paper we see how we can induced single event upset in SRAM and how we can remove it using radiation hardened circuit. Radiation hardened circuit is used to protect your digital device from radiation effect. But the radiation hardened circuit is complex so this is the limitation of this project. REFERENCES Journal Papers: [1] L. W. Massengill, “SEU modeling and prediction techniques,” in IEEE NSREC Short Course, 1993, pp. III-1–III-93 [2] P. E. Dodd and L. W. Massengill, “Basic mechanisms and modeling of single-event upset in digital microelectronics,” IEEE Trans. Nucl. Sci., vol. 50, pp. 583–602, June 2003. [3] J. S. Fu, C. L. Axness, and H. T. Weaver, “Memory SEU simulations using 2-D transport calculations,” IEEE Electron. Device Lett., vol. 6, pp. 422–424, Aug. 1985. [4] D. Binder, E.C. Smith, and A. B. Holman, “Satellite anomalies from galactic cosmic rays,” IEEE Trans. Nucl. Sci., vol. 22, pp. 2675-2680, Dec. 1975. [5] K. Hirose et al. SEU resistance in advanced SOI-SRAMs fabricated by commercial technology using a rad-hard circuit design. IEEE Transactions on Nuclear Science, 49(6), 2002. [6] Joseph J. Fabula and Austin Lesea. The NSEU response of static latch based FPGAs. In MAPLD 2003, Washington, D.C., September 2003. Military and Aerospace Programmable Logic Devices International Conference. Paper C5. [7] F. Vargas and M. Nicolaidis, “Seu - tolerant sram design based on current monitoring,” Fault-Tolerant Computing, 1994. FTCS-24. Digest of Papers., pp. 106–115, 1994. [8] P. C. Murley and G. R. Srinivasan, “Soft- error monte carlo modeling program, semm,” IBM J. RES. DEVELOP.,vol. 40, no. 1, pp. 109–118, 1996. [9] P. Hazucha, K. Johansson, and C. Svensson, “Neutron induced soft errors in cmos memories under reduced bias,” IEEE Transactions on Nuclear Science, vol. 45, no. 6, pp. 2921–2928, 1998. [10] L. Anghel and M. Nicolaidis, “Cost reduction and evaluation of a temporary faults detecting technique,” Design, Automation and Test in Europe Conference and Exhibition 2000, pp. 591–598, 2000. [11] G. C. Messenger, “Collection of charge on junction nodes from ion tracks,” IEEE Transactions on Nuclear Science, vol. 29, no. 6, pp. 2024–2031, 1982. [12] C. Hsieh and P. Murley, “A field-funneling effect on the collection of alpha-particle- generated carriers in silicon devices,” IEEE Electron Device Letters, Vol. 2, No. 4, pp. 103-105, 1981. [13] L. Freeman, “Critical charge calculations for a bipolar SRAM array,” IBM Journal of Research and Development, Vol. 40, No. 1, pp. 119-129, 1996. [14] K. Clark, et al., “Modeling single-event effects in a complex digital device,” IEEE Trans. on Nuclear Science, Vol. 50, No. 6, pp. 2069-2080, 2003. [15] G. Messenger, “Collection of charge on junction nodes from ion tracks,” IEEE Trans. on Nuclear Science, Vol. 29, No. 6, pp. 2024-2031, 1982.