Radiation Hardening by Design is one of the hardware based solution to one of the most troublesome problem faced by digital circuits in the space.
RHBD provides varieties of techniques to make the circuit resilient towards such effects and ensures proper malfunctioning of the circuit.
2.
Introduction to Radiation Hardening
Radiation Effect on Semiconductors
Types of Radiation Hardening by Design
RHBD – Gate Sizing
A Novel Gate Approach
References
Conclusion
3.
In physics radiation is a process in
which energetic particles or energy or waves
travel through a medium or space.
Radiation hardening is a method of
designing and testing electronic components
and systems to make them resistant to damage
or malfunctions caused by ionizing
radiation(particle
radiation
and
highenergy electromagnetic radiation).
4.
Major causes of radiation are
1.) Trapped Electrons
2.) Trapped Protons
3.) Solar Protons
4.) Cosmic Rays
5.
Trapped electrons are negatively charged
particles that are relatively low in mass, but
they are also extremely energetic. Due to their
small masses, they are typically found is very
high orbits such as the Geosynchronous orbits
(or GEO orbits) that are approximately 36,000
km above the earth.
6.
Trapped protons are positively charged
particles held captive by a planet’s gravitation
field. They are less energetic that
electrons, but they are approximately 2000
times more massive than electrons. They exist
in high concentrations at low altitudes. For
example, Low Earth Orbits (LEOs), such as
those located 1400km – 2000km from the
earth’s surface, are proton-dominated orbits.
7.
Solar protons are similar to trapped protons
except they are ejected from the Sun during a
solar fare event and are therefore not trapped
in the planet’s gravitation field.
8.
Cosmic rays are the final source of natural
space-borne radiation. They are comprised of
alpha particles, heavy ions and protons. Heavy
ions are the primary concern when considering
the effects of cosmic rays on semiconductors
because these massive, highly charged
particles can cause severe damage to devices.
9.
TID:
SEL:
SEU:
Total Ionizing Dose is the amount of radiation or
energy that a semiconductor can absorb before it stops
functioning. It is measured in rad(Si), or radiation absorbed
relative to silicon.
Measured in MeV, it is defined as the event in which
the highly energized particle collides with the device and the
current dramatically increases beyond the specification value.
Digitally, SEU is mainly responsible for changing of
a0 to a1. In analog circuits, it produces a spike in the output.
Measured in MeV.
11. It utilizes extra parity bits to check for and possibly
correct the corrupted data.
Radiation Effects may destroy the memory content
even if the system is not accessing the RAM, the so
called scrubber circuit should be used to continuously
sweep the RAM. Following three steps are involved.
1.) Reading out the DATA
2.) Checking the PARITY of the data-errors
3.) Writing back any correction to the RAM
APPLICATIONS:
The error correcting memory is especially suitable for
high tolerant applications such as servers as well as deep
space applications due to cosmic radiations.
12. Redundancy is the duplication of critical
components of the system so as to enhance
system reliability typically in the case of a
backup or a fail-safe.
An error in one component can be outvoted by
the other two.
In a triply redundant system three subcomponents
must fail before the system does. Since each one
seldom fails and is expected to fail independently.
The probability that all three fail is calculated to
be extremely small.
13.
There are four major types of redundancies as follows:
1.) Hardware Redundancy. Eg. DMR (Dual Module
Redundancy) and TMR (Triple Module Redundancy)
2.) Information Redundancy. Eg. Error Detection and
correction methods.
3.) Time Redundancy. Eg. Transient fall detection
methods such as alternate logic.
4.) Software Redundancy. Eg. N version programming.
14. A watchdog timer will perform a hard reset of a
system unless some sequence is performed that
generally indicates the system is alive, such as a
write operation from an on board processor.
During normal operations software schedules a
write the watchdog timer at regular intervals to
prevent the timer from running out.
So if the system is detected to be affected by
radiation the timer will time out and the system
will perform hard reset.
15.
In this method we modify the W/L ratio of the
transistor so that we can have desired current
handling capacity.
The proposed algorithm uses an efficient fault
simulation-based technique to identify and
rank the critical nodes that contribute
significantly to the soft error failure rate of a
combinational logic block.
16.
Part 1: Gate Level SEU protection
Approach A: PN Junction Diode based SEU Clamping
Circuits
Approach B: Diode-connected Device based SEU
Clamping Circuits
Part 2: Logic Block Level Protection
Radiation hardening for all gates
Fixed depth protection
Variable depth protection
17. PN Junction Diode based SEU Clamping Circuits
V (out)
Radiation
Strike
1V
in
out
G
0V
D2
1.4V
GP
Shadow Gate
0.8
0.6
0.4
0.2
0
D1
V (outP)
outP
-0.4V
time
Higher VT
device
0.8
0.6
0.4
0.2
0
-0.4
time
17
18. Diode-connected Device based SEU Clamping Circuits
V (out)
Radiation
Strike
1V
in
out
G
0V
D2
Ids
1.4V
GP
0.8
0.6
0.4
0.2
0
D1
V (outP)
outP
-0.4V
time
Higher VT
device
0.8
0.6
0.4
0.2
0
-0.4
time
18
19. Performed layout and spice level simulation
Approach A has higher area penalty than B
But performance of approach A is slightly better than B
Therefore, selected approach B
20.
ABSTRACT:
This employs cost effective methodology for soft error reduction.
Experiments were performed for various technologies ranging from 180
nm - 70nm. On average 38.1% , 27.1%, 38% radiation hardening was
observed in area, power reduction and delay were observed for worst case
SEUs.
21.
Proposed technique is used for radiation
hardening that increases critical charge on
node. Qcrit is the minimum charge required to
develop SEU.
A node is hardened by adding capacitance (to
increase Qcrit ) or drive (to dissipate the deposited
charge) or combination of both.
This can be achieved by altering the W/L ratio.
22.
Proposed technique is compatible with other
optimization techniques that specifically target
area, delay or power reduction.
It can also be used to complement other fault
avoidance and fault detection techniques, such as SOI
(silicon-on-insulator) substrates, error detection and
correction codes, etc.
By addressing SEU robustness earlier in design
cycle, it aids the synthesis of inherently reliable
circuits, thereby reducing the number of iterations.
23.
The three interrelated factors that
determine whether a particle
strike at a node produces a SEU
at that node are:
1) The total charge deposited at
the node
2) The drive strength of the gate
that drives the node
3) The capacitance of the node.
24.
Consider a two-input NAND gate driving a lumped capacitance Cp at its
output N in Fig. 1. The total capacitance at N is
The charge deposition due to a particle strike at N is modeled by a double
exponential current pulse Iin at the site of the particle strike.
Where Q is the charge (positive or negative) deposited as a result of the
particle strike, τα is the collection time constant of the junction, and τβ is the
ion-track establishment time constant. τα and τβ are constants that depend on
several process-related factors.
25.
The limit to the peak value is set to 0.5Vdd. However it
is to be kept in mind that the following method is
equally applicable for all the values of peak.
The output voltage is obtained as a solution to the
following equation:
Where Ctotal is the total capacitance at N (Eq. 1), Iin is
the current from the particle strike (Eq. 2), and (W/L)
is the aspect ratio of a single nMOS transistor in the
gate.
Id is the effective drain current through the nMOS
transistor network in the gate and is a function of Vout.
26. In each subfigure, it is clear that as the size of the nMOS transistors (which dissipate the
deposited charge) increases, the magnitude and duration of the SEU transient diminish rapidly.
28.
The first condition is that the slope dVout/dt
must equal 0 at tmax, i.e.,
The second condition is given by the charge
conservation.
29.
Since ID is a nonlinear equation that depends
on Vout, the following approximation is used to
simplify the integral.
It is assumed that the voltage Vout rises from 0
to the peak value of 0.5VDD linearly, i.e.,
30.
31.
Gate Sizing technique implemented has the
characteristic
of
compatibility,
also
complements the fault avoidance and
detection/tolerance.
It also emphasizes on reliability by reducing
the number of iterations.
We have presented a novel circuit design
approach for radiation hardened circuit
design.
We use shadow gates and protecting diodeconnected devices to protect the primary
gate from a radiation strike.
32.
1.) M. Dowd, “How Rad Hard do you need? The Changing
Approach”, Maxwell Technologies Microelectronics.
2.)http://en.wikipedia.org/wiki/Radiation_hardening
3.)http://www.militaryaerospace.com/articles/2011/05/radiationhardened-electronics.html
4.) Ron Locoe, Aerospace Corp., “Designing Radiation Hardened CMOS
Microelectronic Components At Commercial Foundries: Space and
Terrestrial Radiation Environments and Device and Circuit Techniques to
mitigate Radiation Effects”
5.) G.U. Youk, N. H. Lee, B.S. Kim, Y.B. Lee, Seungho Kim, “Technology
Development for the Radiation Hardening of Robots”, Proceedings of the
1999 IEEERSJ International Conference on Intelligent Robots and
Systems
6.) H. Hatano, “Radiation hardened high performance CMOS VLSI circuit
designs”, Ph.D
7.) Z. Hu, Z. Liu, H. Shao, Z. Zhang, B. Ning, M. Chen, D. Bi and S.
Zou,“Radiation Hardening by Applying Substrate Bias”, IEEE
TRANSACTIONS ON NUCLEAR SCIENCE, VOL. 58, NO. 3, JUNE
2011, pp. 1355-1360.