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Derivation and Application of a Cost Model for Systems Engineering
Cost Estimation
(Derivación y Aplicación de un Modelo de Estimación de Costos para
la Ingeniería de Sistemas)
Prof. Ricardo Valerdi
Systems & Industrial Engineering
University of Arizona 9 Enero 2017
Academia de Ingeniería
Palacio de Minería
México DF
2
Principle #1
A solution that is too expensive, is not a solution.
Principle #2
Cost of products are a function of complexity and size.
Project Management Triangle
3
Performance
CostSchedule
4
5Nota: Producto Bruto Interno en Mexico para proyectos militares = 0.7%
http://data.worldbank.org/indicator/MS.MIL.XPND.GD.ZS
6
7
8
How is Systems Engineering
Defined?
• Acquisition and Supply
– Supply Process
– Acquisition Process
• Technical Management
– Planning Process
– Assessment Process
– Control Process
• System Design
– Requirements Definition Process
– Solution Definition Process
• Product Realization
– Implementation Process
– Transition to Use Process
• Technical Evaluation
– Systems Analysis Process
– Requirements Validation Process
– System Verification Process
– End Products Validation Process
EIA/ANSI 632, Processes for Engineering a System, 1999.
9
COSYSMO Data Sources (2002-present)
Boeing Integrated Defense Systems (Seal Beach, CA)
Raytheon Intelligence & Information Systems (Garland, TX)
Missile Systems (Tucson, AZ)
Northrop Grumman Mission Systems (Redondo Beach, CA)
Lockheed Martin Transportation & Security Solutions (Rockville, MD)
Integrated Systems & Solutions (Valley Forge, PA)
Systems Integration (Owego, NY)
Aeronautics (Marietta, GA)
Maritime Systems & Sensors (Manassas, VA;
Baltimore, MD; Syracuse, NY)
General Dynamics Maritime Digital Systems/AIS (Pittsfield, MA)
Surveillance & Reconnaissance Systems/AIS
(Bloomington, MN)
BAE Systems National Security Solutions/ISS (San Diego, CA)
Information & Electronic Warfare Systems (Nashua, NH)
SAIC Army Transformation (Orlando, FL)
Integrated Data Solutions & Analysis (McLean, VA)
L-3 Communications Greenville, TX
11
COSYSMO Scope
• Addresses first four phases of the
system engineering lifecycle (per
ISO/IEC 15288)
• Considers standard Systems Engineering
Work Breakdown Structure tasks (per
EIA/ANSI 632)
Conceptualize Develop
Oper Test
& Eval
Transitio
n
to
Operatio
n
Operate,
Maintain,
or
Enhance
Replace
or
Dismantle
EIA/ANSI 632, Processes for Engineering a System, 1999.
ISO/IEC 15288, System Life Cycle Processes, 2008
12
COSYSMO
Size
Drivers
Effort
Multipliers
Effort
Calibration
# Requirements
# Interfaces
# Scenarios
# Algorithms
+
3 Adj. Factors
- Application factors
-8 factors
- Team factors
-6 factors
COSYSMO Operational Concept
Valerdi (2005)
13
Software Cost Estimating Relationship
cSaMM e
⋅⋅=
cKDSIMM ⋅⋅= 05.1
)(4.2
Boehm, B. W., Software Engineering Economics, Prentice Hall, 1981.
MM = Man months
a = calibration constant
S = size driver
E = scale factor
c = cost driver(s)
KDSI = thousands of delivered source instructions
14
COSYSMO Model Form
∏∑ =
⋅





Φ+Φ+Φ⋅=
14
1
,,,,,, )(
j
j
E
k
kdkdknknkekeNS EMwwwAPM
Where:
PMNS = effort in Person Months (Nominal Schedule)
A = calibration constant derived from historical project data
k = {REQ, IF, ALG, SCN}
wx = weight for “easy”, “nominal”, or “difficult” size driver
= quantity of “k” size driver
E = represents diseconomies of scale
EM = effort multiplier for the jth cost driver. The geometric product results in an
overall effort adjustment factor to the nominal effort.
xΦ
Valerdi (2005, 2008)
15
UNDERSTANDING FACTORS
– Requirements understanding
– Architecture understanding
– Stakeholder team cohesion
– Personnel experience/continuity
COMPLEXITY FACTORS
– Level of service requirements
– Technology Risk
– # of Recursive Levels in the Design
– Documentation Match to Life Cycle Needs
OPERATIONS FACTORS
– # and Diversity of Installations/Platforms
– Migration complexity
PEOPLE FACTORS
– Personnel/team capability
– Process capability
ENVIRONMENT FACTORS
– Multisite coordination
– Tool support
Cost Driver Clusters
Valerdi (2005)
16
Stakeholder team cohesion
Represents a multi-attribute parameter which includes leadership, shared vision,
diversity of stakeholders, approval cycles, group dynamics, IPT framework, team
dynamics, trust, and amount of change in responsibilities. It further represents the
heterogeneity in stakeholder community of the end users, customers,
implementers, and development team.
1.5 1.22 1.00 0.81 0.65
Viewpoint Very Low Low Nominal High Very High
Culture Stakeholders
with diverse
expertise, task
nature,
language,
culture,
infrastructure
Highly
heterogeneous
stakeholder
communities
Heterogeneous
stakeholder
community
Some similarities
in language and
culture
Shared project
culture
Strong team
cohesion and
project culture
Multiple
similarities in
language and
expertise
Virtually
homogeneous
stakeholder
communities
Institutionalized
project culture
Compatibility Highly
conflicting
organizational
objectives
Converging
organizational
objectives
Compatible
organizational
objectives
Clear roles &
responsibilities
Strong mutual
advantage to
collaboration
Familiarity and
trust
Lack of trust Willing to
collaborate, little
experience
Some familiarity
and trust
Extensive
successful
collaboration
Very high level of
familiarity and trust
Valerdi (2005)
Technology Risk
The maturity, readiness, and obsolescence of the technology being
implemented. Immature or obsolescent technology will require more Systems
Engineering effort.
Viewpoint Very Low Low Nominal High Very High
Lack of
Maturity
Technology
proven and
widely used
throughout
industry
Proven through
actual use and
ready for
widespread
adoption
Proven on pilot
projects and
ready to roll-out
for production
jobs
Ready for pilot use Still in the
laboratory
Lack of
Readiness
Mission
proven (TRL 9)
Concept qualified
(TRL 8)
Concept has
been
demonstrated
(TRL 7)
Proof of concept
validated (TRL 5 &
6)
Concept defined
(TRL 3 & 4)
Obsolescen
ce
- Technology is
the state-of-the-
practice
- Emerging
technology
could compete
in future
- Technology is
stale
- New and better
technology is on
the horizon in the
near-term
- Technology is
outdated and use
should be avoided
in new systems
- Spare parts
supply is scarce
17
Valerdi (2005)
Migration complexity
This cost driver rates the extent to which the legacy system affects the migration
complexity, if any. Legacy system components, databases, workflows,
environments, etc., may affect the new system implementation due to new
technology introductions, planned upgrades, increased performance, business
process reengineering, etc.
Viewpoint Nominal High Very High Extra High
Legacy
contractor
Self; legacy system is well
documented. Original team
largely available
Self; original
development team not
available; most
documentation
available
Different
contractor; limited
documentation
Original contractor
out of business; no
documentation
available
Effect of legacy
system on new
system
Everything is new; legacy
system is completely
replaced or non-existent
Migration is restricted
to integration only
Migration is related
to integration and
development
Migration is related
to integration,
development,
architecture and
design
18
Valerdi (2005)
19
Cost Drivers Ordered by Effort Multiplier Ratio (EMR)
Valerdi (2005)
Benefits of Local Calibration
Before local calibration
After local calibration
SystemsEngineeringEffort(SEHours)
System Size (eReq)
SystemsEngineeringEffort(SEHours)
System Size (eReq)
20
Wang, G., Valerdi, R. and Fortune, J., “Reuse in Systems Engineering,” IEEE Systems Journal, 4(3), 376-384, 2010.
21
Prediction Accuracy
PRED(30)
PRED(25)
PRED(20)
PRED(30) = 100% PRED(25) = 57%
Valerdi (2005)
Academic
prototype
Commercial Implementations
Proprietary Implementations
COSYSMO-R
SECOST
SEEMaP
Impact
Academic Curricula
Intelligence Community
Sheppard Mullin, LLC
Policy & Contracts
Model
∏∑ =
⋅





Φ+Φ+Φ⋅=
14
1
,,,,,, )(
j
j
E
k
kdkdknknkekeNS EMwwwAPM
COSYSMO
23
20June 2004
Example:
Company “Lockheed Grumman” is building a system that has:
COSYSMO
Size
Drivers
Effort
Multipliers
36 Person
Months of
systems
engineering
effort
Calibration
100 easy, 50
nominal, 75
difficult
requirements
2 easy, 3 difficult
interfaces
4 easy algorithms
5 nominal
operational
scenarios
High requirements und
High tech risk
High process capability
192
24
Contact
Ricardo Valerdi
rvalerdi@arizona.edu
http://rvalerdi.faculty.arizona.edu/

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Derivación y aplicación de un Modelo de Estimación de Costos para la Ingeniería de Sistemas

  • 1. 1 Derivation and Application of a Cost Model for Systems Engineering Cost Estimation (Derivación y Aplicación de un Modelo de Estimación de Costos para la Ingeniería de Sistemas) Prof. Ricardo Valerdi Systems & Industrial Engineering University of Arizona 9 Enero 2017 Academia de Ingeniería Palacio de Minería México DF
  • 2. 2 Principle #1 A solution that is too expensive, is not a solution. Principle #2 Cost of products are a function of complexity and size.
  • 4. 4
  • 5. 5Nota: Producto Bruto Interno en Mexico para proyectos militares = 0.7% http://data.worldbank.org/indicator/MS.MIL.XPND.GD.ZS
  • 6. 6
  • 7. 7
  • 8. 8 How is Systems Engineering Defined? • Acquisition and Supply – Supply Process – Acquisition Process • Technical Management – Planning Process – Assessment Process – Control Process • System Design – Requirements Definition Process – Solution Definition Process • Product Realization – Implementation Process – Transition to Use Process • Technical Evaluation – Systems Analysis Process – Requirements Validation Process – System Verification Process – End Products Validation Process EIA/ANSI 632, Processes for Engineering a System, 1999.
  • 9. 9
  • 10. COSYSMO Data Sources (2002-present) Boeing Integrated Defense Systems (Seal Beach, CA) Raytheon Intelligence & Information Systems (Garland, TX) Missile Systems (Tucson, AZ) Northrop Grumman Mission Systems (Redondo Beach, CA) Lockheed Martin Transportation & Security Solutions (Rockville, MD) Integrated Systems & Solutions (Valley Forge, PA) Systems Integration (Owego, NY) Aeronautics (Marietta, GA) Maritime Systems & Sensors (Manassas, VA; Baltimore, MD; Syracuse, NY) General Dynamics Maritime Digital Systems/AIS (Pittsfield, MA) Surveillance & Reconnaissance Systems/AIS (Bloomington, MN) BAE Systems National Security Solutions/ISS (San Diego, CA) Information & Electronic Warfare Systems (Nashua, NH) SAIC Army Transformation (Orlando, FL) Integrated Data Solutions & Analysis (McLean, VA) L-3 Communications Greenville, TX
  • 11. 11 COSYSMO Scope • Addresses first four phases of the system engineering lifecycle (per ISO/IEC 15288) • Considers standard Systems Engineering Work Breakdown Structure tasks (per EIA/ANSI 632) Conceptualize Develop Oper Test & Eval Transitio n to Operatio n Operate, Maintain, or Enhance Replace or Dismantle EIA/ANSI 632, Processes for Engineering a System, 1999. ISO/IEC 15288, System Life Cycle Processes, 2008
  • 12. 12 COSYSMO Size Drivers Effort Multipliers Effort Calibration # Requirements # Interfaces # Scenarios # Algorithms + 3 Adj. Factors - Application factors -8 factors - Team factors -6 factors COSYSMO Operational Concept Valerdi (2005)
  • 13. 13 Software Cost Estimating Relationship cSaMM e ⋅⋅= cKDSIMM ⋅⋅= 05.1 )(4.2 Boehm, B. W., Software Engineering Economics, Prentice Hall, 1981. MM = Man months a = calibration constant S = size driver E = scale factor c = cost driver(s) KDSI = thousands of delivered source instructions
  • 14. 14 COSYSMO Model Form ∏∑ = ⋅      Φ+Φ+Φ⋅= 14 1 ,,,,,, )( j j E k kdkdknknkekeNS EMwwwAPM Where: PMNS = effort in Person Months (Nominal Schedule) A = calibration constant derived from historical project data k = {REQ, IF, ALG, SCN} wx = weight for “easy”, “nominal”, or “difficult” size driver = quantity of “k” size driver E = represents diseconomies of scale EM = effort multiplier for the jth cost driver. The geometric product results in an overall effort adjustment factor to the nominal effort. xΦ Valerdi (2005, 2008)
  • 15. 15 UNDERSTANDING FACTORS – Requirements understanding – Architecture understanding – Stakeholder team cohesion – Personnel experience/continuity COMPLEXITY FACTORS – Level of service requirements – Technology Risk – # of Recursive Levels in the Design – Documentation Match to Life Cycle Needs OPERATIONS FACTORS – # and Diversity of Installations/Platforms – Migration complexity PEOPLE FACTORS – Personnel/team capability – Process capability ENVIRONMENT FACTORS – Multisite coordination – Tool support Cost Driver Clusters Valerdi (2005)
  • 16. 16 Stakeholder team cohesion Represents a multi-attribute parameter which includes leadership, shared vision, diversity of stakeholders, approval cycles, group dynamics, IPT framework, team dynamics, trust, and amount of change in responsibilities. It further represents the heterogeneity in stakeholder community of the end users, customers, implementers, and development team. 1.5 1.22 1.00 0.81 0.65 Viewpoint Very Low Low Nominal High Very High Culture Stakeholders with diverse expertise, task nature, language, culture, infrastructure Highly heterogeneous stakeholder communities Heterogeneous stakeholder community Some similarities in language and culture Shared project culture Strong team cohesion and project culture Multiple similarities in language and expertise Virtually homogeneous stakeholder communities Institutionalized project culture Compatibility Highly conflicting organizational objectives Converging organizational objectives Compatible organizational objectives Clear roles & responsibilities Strong mutual advantage to collaboration Familiarity and trust Lack of trust Willing to collaborate, little experience Some familiarity and trust Extensive successful collaboration Very high level of familiarity and trust Valerdi (2005)
  • 17. Technology Risk The maturity, readiness, and obsolescence of the technology being implemented. Immature or obsolescent technology will require more Systems Engineering effort. Viewpoint Very Low Low Nominal High Very High Lack of Maturity Technology proven and widely used throughout industry Proven through actual use and ready for widespread adoption Proven on pilot projects and ready to roll-out for production jobs Ready for pilot use Still in the laboratory Lack of Readiness Mission proven (TRL 9) Concept qualified (TRL 8) Concept has been demonstrated (TRL 7) Proof of concept validated (TRL 5 & 6) Concept defined (TRL 3 & 4) Obsolescen ce - Technology is the state-of-the- practice - Emerging technology could compete in future - Technology is stale - New and better technology is on the horizon in the near-term - Technology is outdated and use should be avoided in new systems - Spare parts supply is scarce 17 Valerdi (2005)
  • 18. Migration complexity This cost driver rates the extent to which the legacy system affects the migration complexity, if any. Legacy system components, databases, workflows, environments, etc., may affect the new system implementation due to new technology introductions, planned upgrades, increased performance, business process reengineering, etc. Viewpoint Nominal High Very High Extra High Legacy contractor Self; legacy system is well documented. Original team largely available Self; original development team not available; most documentation available Different contractor; limited documentation Original contractor out of business; no documentation available Effect of legacy system on new system Everything is new; legacy system is completely replaced or non-existent Migration is restricted to integration only Migration is related to integration and development Migration is related to integration, development, architecture and design 18 Valerdi (2005)
  • 19. 19 Cost Drivers Ordered by Effort Multiplier Ratio (EMR) Valerdi (2005)
  • 20. Benefits of Local Calibration Before local calibration After local calibration SystemsEngineeringEffort(SEHours) System Size (eReq) SystemsEngineeringEffort(SEHours) System Size (eReq) 20 Wang, G., Valerdi, R. and Fortune, J., “Reuse in Systems Engineering,” IEEE Systems Journal, 4(3), 376-384, 2010.
  • 22. Academic prototype Commercial Implementations Proprietary Implementations COSYSMO-R SECOST SEEMaP Impact Academic Curricula Intelligence Community Sheppard Mullin, LLC Policy & Contracts Model ∏∑ = ⋅      Φ+Φ+Φ⋅= 14 1 ,,,,,, )( j j E k kdkdknknkekeNS EMwwwAPM COSYSMO
  • 23. 23 20June 2004 Example: Company “Lockheed Grumman” is building a system that has: COSYSMO Size Drivers Effort Multipliers 36 Person Months of systems engineering effort Calibration 100 easy, 50 nominal, 75 difficult requirements 2 easy, 3 difficult interfaces 4 easy algorithms 5 nominal operational scenarios High requirements und High tech risk High process capability 192