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Value-Driven Design
2
Extensive Attributes
Composition Function
Performance, Weight, Cost, and -ilities
Value-Driven Design
3
Analysis
Evaluate
Definition
Design Variables(Length, Displacement)
Attributes (Weight, Eff., Cost)
Configuration
Value
Design Optimization
Value-Driven Design = Optimization
ImproveObjective Function Optimizer
Physical Models CAD System
Value-Driven Design
4
Optimization
Extensive Attributes
ThrustDragEfficiencyWeightManufacturing CostMaint. CostReliabilityMaintainabilityRadar Cross Section
Objective Function
Value
Value-Driven Design
5
Engine Inlet
Status Gradient Value
Efficiency 90% 150,000 135,000Weight 700 -130 -91,000
Manufacturing Cost 700 -1 -700
Maintenance Cost 500 -0.5 -250
Reliability 1500 2.3 3,450
Design Value $ 43,478
Maintainability 7.8 -340 -2,652
Support Equipment 12 -15 -180Radar Cross-Section 0.1 -1200 -120
InfraRed Signature 1.4 -50 -70
VDD Vision: Pervasive use of Optimizationin Engineering Design
Technical detail on distributed optimization can be found at http://www.dfmconsulting.com/opt.pdf
What?
Value-Driven Design
6
Staus Quo: Requirements Flowdown
Turbine Design
TurbineBlade
Design
Propulsion Control System
TemperatureSensor Design
FADECDesign
ServovalveDesign
Wing Design Cockpit Design
Avionics Systems
Radar Design Heads-UpDisplay Design
Landing Gear Systems
Aircraft Systems
Requirements Methodpromises Functionality
Propulsion Systems
If each module meets its requirements, the overall system will meet its requirements
Value-Driven Design
7
VDD Vision: Distributed Optimal Design
Turbine Design
TurbineBlade
Design
Propulsion Control System
TemperatureSensor Design
FADECDesign
ServovalveDesign
Wing Design Cockpit Design
Avionics Systems
Radar Design Heads-UpDisplay Design
Landing Gear Systems
Aircraft Systems
Propulsion Systems
If each component is optimized,
the overall system will be optimized
If you design the best components,
you will realize the best system
Value-Driven Design
8
Distributed Optimal Design
• Overview
• Design Attribute Spaces
• Composition Function
• Objective Function
• Linearization and Decomposition
Value-Driven Design
9
Distributed Optimal Design Overview
Status Gradient Value
Efficiency 90% 150,000 135,000Weight 700 -130 -91,000
Manufacturing Cost 700 -1 -700
Maintenance Cost 500 -0.5 -250
Reliability 1500 2.3 3,450
Design Value $ 43,478
Maintainability 7.8 -340 -2,652
Support Equipment 12 -15 -180Radar Cross-Section 0.1 -1200 -120
InfraRed Signature 1.4 -50 -70
Component Attributes
System Attributes
System Value
Composition Function
Value Model Effect of Component Attribute on System Value
Value-Driven Design
10
• Coordinate Axes are Design Attributes
• Different Space for – Whole Product: x1, x2, ... xm
– Each Component: yk1, yk2, ... ykn (describes component k)
• Super attribute space composed of all attributes of all components: = [y11, y12, ... y21, ... ypn]
• describes whole product; describes all components
Uni
t Pro
fit
Horsepower Relia
bilit
y
x
z
z
z
Intake ManifoldWeight 6.0Cost 12.0Life 20000.0
Intake ValveWeight 0.1Cost 2.0Efficiency 0.9
Cylinder HeadWeight 0.5Cost 42.0Efficiency 0.9Life 10000.0
Design Attribute Spaces
Value-Driven Design
11
• For distributed optimization,– h is the composition function
• Extensive attributes in affect collectively– no other attributes matter for global optimization
• Example elements:
x h z
z
x
Weightchassis
Weighttransmission
Weightengine
. . .
+
+= Weighttractor
component systemmodel
1 1
MTBF MTBFtractor component
The Composition Function
Value-Driven Design
12
Objective Function (Value Model)
The objective function is for the whole system x
We want local objective functions, vj for components j = 1 to n
such that when v y v y y j x x xj j * *
x x* An optimum point is where for all
xx*
That is, when the components are optimized, the product is optimized
Value-Driven Design
13
Objective Function with Local Attributes
• Since value = and , then value , a function of local attributes
• This gives us global value in terms of local attributes, but does not give an independent objective function for each component
• For independence, we must linearize
• Thus each component has its own goal
x
x h z h z
h z
Value-Driven Design
14
Validity of Linearization
Given smoothness of and h, the linear approximation is reasonable for small changes (< 10% of whole system value) near the preliminary design
Value-Driven Design
15
• Start with a reference design (preliminary design) with attributes x* and z*
• Generate the Taylor expansion of around z* :
• O2 represents second order and higher terms that we can ignore in the vicinity of z*
• Without O2, the Taylor series is linear
Linearizing the Objective Function
h z
h z x J z z Ox h z
* *
* *2 h z
Value-Driven Design
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Solving the Taylor Expansion
• is the gradient of
• Jh is the Jacobian Matrix of h:
x x x x1 2 3 4
, , , ,
x
z
x
z
x
z
x
zx
z
x
z
x
z
x
zx
z
x
z
x
z
x
z
x
z
x
z
x
z
x
z
p
p
p
m m m m
p
1
1
1
2
1
3
1
2
1
2
2
2
3
2
3
1
3
2
3
3
3
1
1 2 3
Value-Driven Design
17
Solving the Taylor Expansion
h z h zx
x
zz z
i
i
ji
m
j
p
j j
* *
11
Objective functions are used for ranking—they are not changed by the addition or subtraction of a constant. Thus, the expression above can be simplified by dropping all terms that use the constant z*:
h zx
x
zz
i
i
ji
m
jj
p
11
Linear objective functions have the property that can be maximized by maximizing each zj term or any group of zj terms independently
Value-Driven Design
18
Component Optimization
For a group of zj’s that correspond to a single component, we can relable them y1 though yn and determine the component objective function (in the vicinity of the preliminary design):
component
i
i
k xi
m
k
n
kx
x
yy
*11
Value-Driven Design
19
Value landscape in parameter space
Value landscape in property space
Analysis
SearchEvaluate
Definition
Objective Function Optimizer$Parameters (Length, Displ.)
Properties (Weight, Eff., Cost)
Configuration
Value
Physical Models Design Drawing
“But you can’t DO that!”
Value-Driven Design
20
Component Design Value is Commensurate
with System Design Value
Partial Derivatives of the Objective Function
Implementing Distributed Optimal Design
Engine Inlet
Status Gradient Value
Efficiency 90% 150,000 135,000Weight 700 -130 -91,000
Manufacturing Cost 700 -1 -700
Maintenance Cost 500 -0.5 -250
Reliability 1500 2.3 3,450
Design Value $ 43,478
Maintainability 7.8 -340 -2,652
Support Equipment 12 -15 -180Radar Cross-Section 0.1 -1200 -120
InfraRed Signature 1.4 -50 -70
Value-Driven Design
21
Other Benefits of VDD
• Optimization Finds a Better Design
• Requirements Cause Preference Conflicts
Value-Driven Design
22
Optimization Finds a Better Design
Requirements
< $30 M unit mfg cost
< 30,000 lbs. w
eight
Cost
Weight(0,0)
Best
Cost
Weight(0,0)
Increasing Score
Traditional Spec Method Optimal Design
Limit of Feasibility
Value-Driven Design
23
Brake Material + $11,000 - 90 lbs.Rudder - $10,000 + 190 lbs.
Net Impact + $ 1,000 + 100 lbs.
Differences in revealed values within a design team lead to choices that, taken together, are clearly lose-lose
Requirements Cause Preference Conflicts
Value-Driven Design
24
Design Potential
Distributed Optimal Design
Requirements Method
Val
ue A
Value B
Conflicts: Folding in Attribute Space
Value-Driven Design
25
Extensions of VDD beyond Detailed Design
• Conceptual Design
– Develop a Value Model for system optimization
• Technology Development
– Develop a Value Model / Composition Function for technology insertion and evaluation
• Risk Management
– Quantitative valuation of consequences
• Test Planning
– Value of Information
Value-Driven Design
26
Summary
• VDD can improve system value by tens of billions of dollars for complex aerospace systems– versus flowing down requirements for extensive attributes
• Value-Driven Design in a nutshell– Optimization is used to design all components
– Extensive variables are incorporated into the objective function
– Component objective functions are coordinated with the system objective function for distributed optimal design
• We must transition VDD to practice
Value-Driven Design
27
Future Steps
• What is necessary to mature the VDD concept– pilot application
• University research project - simulated prototype
• Small DoD application (too small means low value, but proof of concept)
• evaluate scalability - to more complex systems and across life cycle
– test theory formally on an existing program• derive falsifiable hypotheses, collect data, assess hypotheses
• use the Abbas-Matheson model to quantify results
• three programs, working from small to large
• How should VDD be introduced into the Community?– Guidebook ...
• What needs to be done prior to PDR to make VDD feasible?– Value model development (need a process)
– Concept optimization (closer to practice)
• What does the govt need to do to make this happen?