| Pugh Matrix: Decisions, Decisions, Decisions... |
By Mike
Walmsley
Most
decisions we make in life are not complicated. We assess the pertinent
information available to us, blend in a little common sense and intuition, and
arrive at a direction to pursue. We are either successful in the outcome or
not. If not, we learn. On the other hand, decisions in the business sector are
fairly complicated. Penalties for making an incorrect decision can cost us
customer dissatisfaction, millions of dollars in lost capital, market share,
and in the extreme case, our very business.
The
academic field of Operations Research has recognized this concern and has
developed a separate branch of research known as the “Decision Sciences”. The
original emphasis was placed on co-jointly developing techniques with the DoD
(Department of Defense), DoE (Department of Energy) to address and identify
risk management policy for potential safety hazardous situations in our
environment and community (such as impacts due to nuclear, biological and
chemical events). Later, the concepts were recognized to be applicable in the
business sector. While many of the techniques are fairly complicated in their
mathematical reasoning, one such technique is not. It has been in existence and
use since the late 1980s with a formal introduction cited in the text “Creating
Innovative Products Using Total Design” * by Stuart Pugh (1996
Addison Wesley). Known as the “Pugh Matrix” technique, it is a favorite method
for management teams dealing with problem solving in Multi-Concept, Multiple-
Attribute situations.
The output
results of the process are product / process design concepts that are chosen
and optimized based on open and documented criteria. Such a process forms
well-understood product / process design values and forces cross-functional
negotiation and buy-in. These criteria and their importance have been put in
place by organizational consensus building and relate back to the driving
customer wants and needs (CTQs). This is key to the Six Sigma DMAIC, DFSS process/product
design improvement processes respectively. Because of this, the Pugh decision
analysis matrix has become a key tool in the Six Sigma toolbox.
The
optimum use of the tool is for those situations where we have many alternative concepts
to choose from, with each concept entailing multiple attributes (product /
process considerations).
The process
flow for tool use is:
- From Six Sigma,
Define the problem.
- Define the
cross-functional team that will work on the problem.
- Define what we
consider to be the “baseline”. e.g. a product or process that we have in place
that is considered non-optimal.
- Define the
requirements (CTQs ~“attributes”) and criteria that will be used in the
analysis.
- Define the
alternative concepts that will be included in the analysis.
- Define rating
scale that will be used in the prioritization and trade-off attribute analysis.
- Define the scaling
criteria that will be used in the concept analysis.
- Set up the Pugh
Matrix.
- Analyze and rank
each concepts benefit.
- Conduct “what-if” simulation studies and re-assess
concepts benefit (optional).
- Select the concept(s) that detail the most benefit.
- Initiate development/optimization analysis activities
on the concept chosen.
As an
example of how the tool can be used consider the following from the automotive
industry. Antilock brake system Wheel Speed Sensors (3 / 4 per vehicle).

Figure
1 The
application and basic mode of operation
 |
Mode
of operation:
Sensors are located at wheel ends (Hub or Hub and integral bearing). Sensor
head is at most 2mm from ferromagnetic ring, integral to brake rotor. As
wheel is turned, a field change is generated and a pulse is issued thru
sensor head to vehicle ECU. Pulse width and frequency of pulses is compared
to a tabled algorithm. This algorithm defines to a comparator in the ECU the
speed at which a particular wheel is moving. All (4) wheels are monitored
simultaneously. If a significant deceleration departure on one wheel is noted
(indicating slip, lock), the vehicle anti-lock system is activated by the ECU. |
The
problem definition:
When ABS systems first came out, the existing technology was deemed non-optimal
to environmental temperatures, vehicle packaging, signal accuracy, resolution,
high and low speed design limits, output signal level and waveform,
Reliability, serviceability, packaging size (mass), EMI/EMC robustness,
manufacturability, cost, and others. The “Attributes”
Scope of
analysis: Research at
the time had indicated that there exist at most (14) separate design concept
configurations that could be potentially pursued. The “Concept
Alternatives”. Note that only one was in actual physical existence at
the time (VR). Since the physical theory exists for the others, assessing the
other concepts will require a great deal of design simulation, materials
analysis and potential pricing with respect to the proposed environment and
duty cycle.
Goal
Statement: Find and
select at most (3) sensor technologies that would entail the most benefit in
terms of future development.
Solution: A team was formed, the technology
concepts were researched and the initial Pugh Matrix was set up.
Figure
2 The
initial Matrix and scoring criteria
Attribute
rating criteria Concept
Alternative scaling criteria
Note:
0
= Low
10 = High |
- = Disadvantage
0 = No improvement (Same as
existing system)
+ = Advantage |
The concept Alternatives
|
Customer wants & needs (CTQs: Attributes) |
Importance
of need |
Design Baseline |
Opt #1
|
Opt #2
|
Opt #3
|
Opt #4
|
Opt #5
|
Opt #6
|
Opt #7
|
Opt #8
|
Opt #9
|
Opt #10
|
Opt #11
|
Opt #12
|
Opt #13
|
Opt #14
|
|
Pc. Cost comparison to existing system |
5 |
0 |
|
|
|
|
|
|
|
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|
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|
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|
Systems
cost impact |
8 |
0 |
|
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|
Manufacturability |
10 |
0 |
|
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|
System
compatability |
10 |
0 |
|
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|
Net build
at asm. |
10 |
0 |
|
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|
Thermal
range |
10 |
0 |
|
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|
Air gap |
8 |
0 |
|
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|
Low speed
limit |
4 |
0 |
|
|
|
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|
High
speed limit |
4 |
0 |
|
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|
Resolution capability |
9 |
0 |
|
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| Pulse
width encoding |
5 |
0 |
|
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|
| Accuracy/precision |
10 |
0 |
|
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| Output
signal level |
10 |
0 |
|
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|
| Output
waveform |
4 |
0 |
|
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|
| Reliability/Durability |
10 |
0 |
|
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| Serviceability
|
4 |
0 |
|
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|
Materials availability |
10 |
0 |
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| Package
size (mass) |
10 |
0 |
|
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| EMI/EMC robustness |
10 |
0 |
|
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|
SUM
|
151 |
0 |
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|
Ranked
Attribute Scaled (zeroed)
importance
baseline
How it works:
To assess each of the concept alternatives, the concept
alternative scaling criteria “sign”
will be placed in front of the attribute importance for each attribute of a
given concept alternative. E.g. If it were determined from research measurement that
for Option #1 the attribute“ Piece cost comparison to existing system” were to be a benefit
over the existing baseline system, then a “+5” would be placed in that cell. The “5” coming
from the importance of need for the attribute. If the particular research measurement were to show
that a disadvantage would exist with respect to the existing baseline system, then a
“- 5” would be placed in the cell. Each and every cell in the matrix would be assessed
similarly.
Once all the cells are filled in, we would “sum” each column and look for those
concept alternatives that were largest from a positive standpoint over all the others.
A “larger the better” scenario.
Each member of the team was assigned research tasks that required obtaining
meaningful
variables measurements for each of the key Attributes.
Obtaining the measurements required a period of two months to accomplish. Once
the
measurements were obtained, they met in a team meeting and completed the
matrix.
Figure
3 The completed matrix (and solutions identified).
| Customer wants & needs (CTQs: Attributes) |
Importance
of need |
Design
Baseline |
Opt #1
|
Opt #2
|
Opt #3
|
Opt #4
|
Opt #5
|
Opt #6
|
Opt #7 |
Opt #8 |
Opt #9 |
Opt #10
|
Opt #11
|
Opt #12
|
Opt #13
|
Opt #14
|
| Pc. Cost comparison to existing system |
5 |
0 |
- |
- |
- |
- |
- |
- |
- |
- |
- |
- |
- |
- |
+ |
- |
| Systems cost impact |
8 |
0 |
- |
- |
- |
- |
- |
- |
- |
- |
- |
+ |
- |
- |
+ |
- |
| Manufacturability
|
10 |
0 |
- |
- |
- |
- |
- |
- |
0 |
+ |
0 |
0 |
- |
- |
- |
0 |
| System compatability |
10 |
0 |
- |
- |
- |
- |
0 |
0 |
0 |
0 |
0 |
0 |
0 |
0 |
0 |
- |
| Net build
at asm. |
10 |
0 |
- |
- |
- |
- |
- |
0 |
0 |
+ |
0 |
0 |
0 |
0 |
- |
0 |
| Thermal range |
10 |
0 |
0 |
+ |
+ |
+ |
+ |
- |
+ |
+ |
0 |
0 |
0 |
0 |
0 |
- |
| Air gap
|
8 |
0 |
+ |
+ |
+ |
+ |
0 |
0 |
0 |
0 |
0 |
0 |
0 |
0 |
- |
- |
| Low speed limit |
4 |
0 |
+ |
+ |
+ |
+ |
+ |
+ |
+ |
+ |
+ |
0 |
0 |
0 |
+ |
- |
| High speed limit |
4 |
0 |
0 |
+ |
+ |
+ |
0 |
0 |
0 |
0 |
0 |
0 |
0 |
0 |
- |
- |
| Resolution capability |
9 |
| |