Here are the key results from the response table:
- For WL, the highest level of 2.0/ww had the steepest slope and highest S/N ratio, indicating it is the most robust setting
- For WW, the middle level of 0.75 had the steepest slope and highest S/N ratio, indicating it is the most robust setting
This step identifies the most robust settings for each control factor based on the experiment results.
How to Design a Paper Gyrocopter Using Robust Design
1. What is Robust Design or
Taguchi’s method?
• An experimental method to achieve product
and process quality through designing in an
insensitivity to noise based on statistical
principles.
2. History of the method
• Dr. Taguchi in Japan: 1949-NTT
– develops “Quality Engineering”
– 4 time winner of Demming Award
• Ford Supplier Institute, early 1980s
• American Supplier Institute, ASI
– Engineering Hall of Fame
• Statistics Community
– DOE
– S/N Ratio
3. Who uses Taguchi’s Methods
• Lucent • Toyota
• Ford • TRW
• Kodak • Chrysler
• Xerox • GTE
• Whirlpool • John Deere
• JPL • Honeywell
• ITT • Black & Decker
4. Documented Results from Use
• 96% improvement of NiCAD • $900,000 annual savings in the
battery on satellites (JPL/ NASA) production of sheet-molded
• 10% size reduction, 80% compound parts (Chrysler)
development time reduction and • $1.2M annual savings due to
20% cost reduction in design of a reduction in vacuum line
choke for a microwave oven (L.G. connector failures (Flex
Electronics) Technologies)
• $50,000 annual cost savings in • 66% reduction in variability in
design of heat staking process arrival time and paper
(Ann Arbor Assembly Corp) orientation (Xerox)
• 60% reduction in mean response • 90% reduction in encapsulation
time for computer system (Lucent) variation (LSI Corp)
5. Insensitivity to Noise
• Noise = Factors which the engineer can not or
chooses not to control
– Unit-to-unit
• Manufacturing variations
– Aging
• Corrosion
• UV degradation
• wear
– Environmental
• human interface
• temperature
• humidity
6. How Noise Affects a System
Noise
Useful Energy
Energy Ideal Function of Quality Characteristic, y
Signal Factor, M Product or Process
Harmful Energy
Caused by Noise
Control
Factors
7. Step 1: Define the Project Scope 1/2
• A gyrocopter design is to be published in a Sunday Comics
section as a do-it-yourself project for 6-12 year old kids
• The customers (kids) want a product they can easily build
and have a long flight time.
| WW |
---
WL
--- ---
---
1/4”
BL
----
8. Step 1: Define the Project Scope 2/2
• This is a difficult problem from an engineering standpoint
because:
– hard to get intuitive feel for effect of control variables
– cant control materials, manufacturing or assembly
– noise factors are numerous and have strong effect on
flight.
9. Step 2: Identify Ideal Function
• Ideally want the most flight time (the quality characteristic
or useful energy) for any input height (signal or input
energy)
• Minimize Noise Effect
• Maximize Slope
Time of Flight
Drop Height
10. Step 3: Develop Noise Strategy 1/2
• Goal is to excite worst possible noise conditions
• Noise factors
– unit-to-unit
– aging
– environment
11. Step 3: Develop Noise Strategy 2/2
• Noise factors
– unit-to-unit
Construction accuracy
Paper weight and type
angle of wings + many, many others
– aging
damage from handling
– environment
angle of release
humidity content of air
wind
12. Step 4: Establish Control Factors and Levels
1/4
• Want them independent to minimize interactions
– Dimensionless variable methods help
– Design of experiments help
– Confirm effect of interactions in Step 7
• Want to cover design space
– may have to guess initially and perform more
than one set of experiments. Method will help
determine where to go next.
13. Step 4: Establish Control Factors and Levels
2/4
• Methods to explore the design space
– shot-gun
– one-factor-at-a-time
– full factorial
– orthogonal array (a type of fractional factorial)
14. Step 4: Establish Control Factors and Levels
3/4
Control factor array for the paper gyrocopter parameter optimization
experiment
1 2 3 4 5 6 7 8
Run WL WW BL Size B_Fold Gussets
1 1 1.0/ww 0.50 1.33 x WL 100% 1 0 None
2 1 1.0/ww 0.75 1.67 x WL 75% 2 15% 45deg
3 1 1.0/ww 1.00 2.00 x WL 50% 3 30% 45deg
4 1 1 .5/ww 0.50 1.33 x WL 75% 2 30% 45deg
5 1 1.5/ww 0.75 1.67 x WL 50% 3 0 None
6 1 1.5/ww 1.00 2.00 x WL 100% 1 15% 45deg
7 1 2.0/ww 0.50 1.67 x WL 100% 3 1 5% 45deg
8 1 2.0/ww 0.75 2.00 x WL 75% 1 30% None
9 1 2.0/ww 1.00 1.33 x WL 50% 2 0 45deg
10 2 1.0/ww 0.50 2.00 x WL 50% 2 15% None
11 2 1.0/ww 0.75 1.33 x WL 100% 3 30% 45deg
12 2 1.0/ww 1.00 1.67 x WL 75% 1 0 45deg
13 2 1.5/ww 0.50 1.67 x WL 50% 1 30% 45 deg
14 2 1.5/ww 0.75 2.00 x WL 100% 2 0 45deg
15 2 1.5/ww 1.00 1.33 x WL 75% 3 15% None
16 2 2.0/ww 0.50 2.00 x WL 75% 3 0 45deg
17 2 2.0/ww 0.75 1.33 x WL 50% 1 15% 45deg
18 2 2.0/ww 1.00 1.67 x WL 100% 2 30% None
17. Data for Runs 5 and 15
2.5
2
Time (sec)
1.5
Run 5
1 Run 15
0.5
0
0 2 4 6 8 10
Height (ft)
18. Step 6: Conduct Data Analysis 1/7
• Calculate signal-to-noise-ratio (S/N) and Mean
• Complete and interpret response tables
• Perform two step optimization
– Reduce Variability (minimize the S/N ratio)
– Adjust the mean
• Make predictions about most robust configuration
19. Step 6: Conduct Data Analysis 2/7
• Calculate signal to noise ratio, S/N, a
metric in decibels variability
S/N gain reduction
Useful output 3 27%
S/N =
Harmful output 6 50%
12 75%
Effect of Mean
= Variability around mean
y2
= 10 log 2 Note: This is one of many
s
forms of S/N ratios.
20. Step 6: Conduct Data Analysis 3/7
Results of the parameter optimization experiment
1 2 3 4 5 6 7 8 slope S/N
Run WL WW BL Size B_Fold Gussets (sec/ft)
1 1 1.0/ww 0.50 1.33 X WL 100% 1 0 None 0.25 6.94 dB
2 1 1.0/ww 0.75 1.67 X WL 75% 2 15% 45deg 0.25 2.67 dB
3 1 1.0/ww 1.00 2.00 X WL 50% 3 30% 45deg 0.19 -0.24 dB
4 1 1.5/ww 0.50 1.33 X WL 75% 2 30% 45deg 0.22 0.69 dB
5 1 1.5/ww 0.75 1.67 X WL 50% 3 0 None 0.26 9.04 dB
6 1 1.5/ww 1.00 2.00 X WL 100% 1 15% 45deg 0.25 3.81 dB
7 1 2.0/ww 0.50 1.67 X WL 100% 3 15% 45deg 0.26 -1.95 dB
8 1 2.0/ww 0.75 2.00 X WL 75% 1 30% None 0.29 4.73 dB
9 1 2.0/ww 1.00 1.33 X WL 50% 2 0 45deg 0.26 2.64 dB
10 2 1.0/ww 0.50 2.00 X WL 50% 2 15% None 0.24 2.81 dB
11 2 1.0/ww 0.75 1.33 X WL 100% 3 30% 45deg 0.19 0.76 dB
12 2 1.0/ww 1.00 1.67 X WL 75% 1 0 45deg 0.24 3.87 dB
13 2 1.5/ww 0.50 1.67 X WL 50% 1 30% 45deg 0.24 1.62 dB
14 2 1.5/ww 0.75 2.00 X WL 100% 2 0 45deg 0.28 0.87 dB
15 2 1.5/ww 1.00 1.33 X WL 75% 3 15% None 0.23 -3.96 dB
16 2 2.0/ww 0.50 2.00 X WL 75% 3 0 45deg 0.27 9.04 dB
17 2 2.0/ww 0.75 1.33 X WL 50% 1 15% 45deg 0.28 4.88 dB
18 2 2.0/ww 1.00 1.67 X WL 100% 2 30% None 0.31 2.99 dB
23. Step 6: Conduct Data Analysis 6/7
Two Step Optimization
• Reduce Variability (minimize the S/N ratio)
– look for control factor effects on S/N
– Don’t worry about mean
• Adjust the mean
– To get desired response
– Use “adjusting factors”, those control factors
which have minimal effect on S/N
24. Step 6: Conduct Data Analysis 7/7
• For gyrocopter
– wing width = .75in
– wing length = 2.00/0.75 = 2.67 in
– body length = 2.00 x 2.67 = 5.33 in
– size = 50%
– no body folds Predicted Performance
– no gussets S/N = 9.44 dB
Slope = .31 sec/ft
25. Step 7: Conduct Conformation Run
• To check validity of results
• To check for unforeseen interaction effects
between control factors
• To check for unaccounted for noise factors
• To check for experimental error
Predicted Confirmed
S/N 9.44 dB 9.86
Slope .31sec/ft .32 sec/ft
26. How Taguchi’s Method Differs from an
Ad-hoc Design Process
• Organized Design Space • Concurrently Addresses
Search Manufacturing Variation
• Clear Critical Parameter • Concurrent Design-Test
Identification Not Design-Test-Fix
• Minimize Development
• Focus on Parameter
Time (Stops Fire Fighting)
Variation (Noise)
• Corporate Memory
• Clear Stopping Criteria Through Documentation
• Robustness centered not • Encourages Technology
Failure Centered Development Through
• Reusable Method System Understanding
27. How Taguchi’s Method Differs from
Traditional Design of Experiments
• Focused on reducing the • Tries to reduce interaction
impact of variability between control factors
rather than reducing rather than study them
variability Requires little skill in
• Focused on noise effects statistics
rather than control factor • Usually lower cost
effects
• Clearly focused cost
function - maximizing the
useful energy
28. How Taguchi’s Method Differs from
Shainin’s Method
• Focused on both Product • Widely Used
and Process Design rather Internationally
than Primarily on Process
• Fire prevention rather than
• Oriented to developing a
fire fighting
robust system not finding
a problem (Red X). • Accessible
Taguchi tells what • Many Case Studies
parameter values to set to Available
make system insensitive to
parameter Shainin
identifies as needing
control.
29. Plan for Application at Tektronix
• Select a parameter design problem
• Design the experiment
• Perform the experiment
• Reduce data
• Report results to Company
• Assuming success
– design more experiments
– train more engineers
– Plan for student-run experiments