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Jim Armstrong - PPT Presentation

Industry Professor Stevens Institute of Technology Systems Integration What Are We Waiting For 2013 J Armstrong 1 Repeat Errors Part I Fire Engine Too Big Florida New truck to long for station ID: 301181

armstrong 2013 system integration 2013 armstrong integration system interface model gun early readiness bullets control delivered repeat amp scientist

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Slide1

Jim ArmstrongIndustry ProfessorStevens Institute of Technology

Systems Integration: What Are We Waiting For

© 2013 J. Armstrong

1Slide2

Repeat Errors, Part I

Fire Engine Too Big

FloridaNew truck to long for station

Added to front of station

Not enough clearance to access street

Others:

Boston – didn’t fit in historic stationTuscumbia, Alabama – too tallDunfermline, Scotland – too big for streetsSaranac Lake NY – too tall & too heavyMontcuq in the Lot, France – too big for streetsTarentum, PA – too tall & too heavyElkville, Ill – New station not built yetLondon, Ontario, Canada – too tall (measurement error)Edmondson, AR – too wideMorant Bay Jamaica – too wide for streets

Arched doors in Boston

Integration of Full System

© 2013 J. Armstrong

2Slide3

Repeat Errors, Part IIF-16 Guns

Shotgun spread due to motion & time between shots

Improvements in flight control and Gatling gun – one misses, all miss!Fix – shaker, then flexible mount

Others with same or similar: F-104, B-52 Tail Gun, A-10, Cobra gunship, Roman arrow catapult

Integration of Technologies

© 2013 J. Armstrong

3Slide4

Repeat Errors, Part III

Satellite Failure

Small satellite failed on launchFailure analysis unable to reproduce failure during single parameter test

Combined thermal and vibration test revealed cause

Decade later, same organization repeats same mistake!

Integrated Approach to Testing

© 2013 J. Armstrong4Slide5

Can We Learn?

It is said that only a fool learns from his own mistakes, a wise man from the mistakes of others.

– Otto von Bismarck

Vasa

© 2013 J. Armstrong

5Slide6

Do We Learn?

Spain’s S-80 series submarine

100 tons overweight

Will submerge

Won’t surface

Isaac

Peral

© 2013 J. Armstrong6Slide7

Repeat ErrorsConclusion

“It’s not that we shoot ourselves in the foot that surprises me…

…it’s how fast we reload!”

- Anonymous

© 2013 J. Armstrong

7Slide8

Better Ideas

So what can be done…Strategy Early actionsConway’s Law

Model-based integrationConsider multiplesAllocate and track

Integration Readiness Levels

Cross-path Integration

External EnvironmentHuman Systems IntegrationDeployment

© 2013 J. Armstrong8Slide9

Integration Strategy

Common: Assemble components as built

SimpleReactive

Risky

Better: Identify integration and deployment risks and mitigate in advance

More early activities

Proactive reduces risksNote: CMMI says to define integration strategy, formerly said to define the assembly sequence

Risks

© 2013 J. Armstrong

9Slide10

Start Early

Integration starts here!Start of assembly is too late

Design

Engineering

Systems Engineering

Operational Concept

Originating Requirements

System Requirements

Element Specs

Segment Specs

Component Specs

CI Specs

System Delivered

Elements Delivered

Segments Delivered

Components Delivered

CIs Delivered

Operational

Validity

Stakeholders’

Needs

Acceptability

Developmental

Verification

© 2013 J. Armstrong

10Slide11

Conway’s Law

Any organization that designs a system (defined broadly) will produce a design whose structure is a copy of the organization's communication structure.

Example: Mars Climate Orbiter

Ground model used metrics - JPL

Spacecraft expected

‘English’ (feet) - LMCO

Lesson: Integrate the enterprise first© 2013 J. Armstrong11Slide12

Integration Management Methods

Interface Control Working Groups (ICWG)Members from both (all) sides of the interfaceAddresses interface issues

Systems Engineering Interface Team (SEIT)Members from IPTs on a programAddresses interface issues

Maintains commonality of discipline approaches

Configuration Management of ICDs

Specific process for interface related changesInterface Design ReviewBetween PDR and CDR

Focus on only the interfaces© 2013 J. Armstrong12Slide13

Model-based IntegrationExecutable models are valuable for interfaces

: Scientist

: ScientistInterface

: DataSet

: Sample

: EnvironmentInterface

MAIN SCENARIO:

Steps 1 and 2 may be in

any order...

1. Scientist selects data

set

2. Scientist selects

analysis

3. Scientist receives

analysis results (data set)

Select data set

Select analysis

return results

Analyze

Get samples

Get samples

Get sample data

n.1

Request

Withdrawal

n.5

Process

Request

n.6

Confirm

OK

n-1 (Ref)

Prior

Function

n.8

Determine

If OK

Y

N

n+1 (Ref)

Next

Function

Withdrawal Request

Cash

OK or reject

Approval/disapproval

Withdrawal Notice

n.7

Pay

n.3

Decide

Retry

n.2

Read

Response

n..4

Collect

Cash

Y

N

Y

N

IT

IT

ATM

Customer

Bank

Interface

Interface

© 2013 J. Armstrong

13Slide14

Model-based Integration

Comanche HelicopterFull model of gun operationsIncluded:Equipment – new and old

Pilot – fresh and tiredMissionsNavy ATC Communications

Full model

Identified protocol errors in switch from 4-ship to individual aircraft

Components integrated into model as developed

© 2013 J. Armstrong14Slide15

Multiple Copies

US Advanced Automation SystemNew video recording functionFull update every 12 seconds

Worked fine on single scopeLaboratory Established6 full size scopes

94 emulated

Crashed all four networks

Why not found by modeling early?

© 2013 J. Armstrong15Slide16

Allocate and Track

Know which parts contribute to performance and howAllocate critical parameters carefullyTrack frequently and at design levelTechnical Performance Parameters (TPMs)

© 2013 J. Armstrong

16Slide17

Allocation Example© 2013 J. Armstrong

17

Function

Requirement

Component

Destroy Target

X% damage/hit

Bullets

Go to Target

+/- X degrees

Bullets

Propel Bullets

+/- X fps

+/- X bullets/second

+/- X degrees

Gun

Stabilize Bullets

+/- X RPM

Gun

Aim Gun

+/- degreesMount/airframe

Control Aircraft

+/- stability

Flight control

Find and Display Target

+/1 accuracy

Radar

Guide Aircraft

+/- control accuracy

Pilot

Provide Aerodynamics

+/- stability & response

AirframeSlide18

Integration Readiness Level

Have these technologies been used together before?

SRL = IRL x TRL

IRL = Integration Readiness Level

Technology Readiness Levels

Integration Readiness Levels

sse.stevens.edu/

fileadmin

/

cser

/2006/papers/126-Sauser-TRL%20SRL.pdf

© 2013 J. Armstrong

18Slide19

Early Cross-Path Integration

InternalBetween componentsExternal

Other systemsLegacyOperations

People

Environment

Internal

External

© 2013 J. Armstrong

19Slide20

External

Environment

Sydney Morning Herald – 10/13/97

Cars exhibit problems

Brakes jam on

Doors lockEngines shut down

SourcesTraffic light sensorsTaxi and police radiosBroadcast transmittersUnderground power lines© 2013 J. Armstrong20Slide21

Human System Integration

Downing of Iranian airlinerWashington Post headline: “System works, operator makes error”But the operator is part of the system!

Air France Flight 447Automation turns offQuick reaction required

Questionable data

Human response as expected?

Therac-35Operators faster than anticipated

Software didn’t accept inputPatients died© 2013 J. Armstrong21Slide22

DeploymentWill it fit?

Is support ready?Transportation?Training?Local customs?

Environment?Schedule?Geography?Does it work for the user in their operations?

© 2013 J. Armstrong

22Slide23

England’s High Speed 2

Considering integration withExisting railAirWhere you live

Where you are goingINCOSE Presentation, IS 2012, Rome, Italy

© 2013 J. Armstrong

23Slide24

ConclusionYes, we can do better with…

Early startContinued effort

Systems thinking

© 2013 J. Armstrong

24

There is a lot of integration to do

before and after putting the pieces together!Slide25

Questions?

1-

25