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Nationaal Lucht- en Ruimtevaartlaboratorium National Aerospace Laboratory NLR DXXX-1A The Free Flight Deck Society of Automotive Engineers (SAE) S-7, “Flight Deck and Handling Qualities Standards for Transport Aircraft” Amsterdam, 1 May 2000 Rob Ruigrok, Jacco Hoekstra, Ronald van Gent

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Page 1: Nationaal Lucht- en Ruimtevaartlaboratorium National Aerospace Laboratory NLR DXXX-1A The Free Flight Deck Society of Automotive Engineers (SAE) S-7, “Flight

Nationaal Lucht- en RuimtevaartlaboratoriumNational Aerospace Laboratory NLR

DXXX-1A

The Free Flight Deck

Society of Automotive Engineers (SAE)

S-7, “Flight Deck and Handling Qualities Standards for Transport Aircraft”

Amsterdam, 1 May 2000

Rob Ruigrok, Jacco Hoekstra, Ronald van Gent

Page 2: Nationaal Lucht- en Ruimtevaartlaboratorium National Aerospace Laboratory NLR DXXX-1A The Free Flight Deck Society of Automotive Engineers (SAE) S-7, “Flight

Nationaal Lucht- en RuimtevaartlaboratoriumNational Aerospace Laboratory NLR

DXXX-2A

Presentation Overview Introduction to Free Flight

Design of the Free Flight Deck– Starting points– Airborne Separation Assurance System

Using the Free Flight Deck:– NLR studies on Free Flight with Airborne

Separation Assurance

Conclusions and Recommendations

Future Plans

Demonstrations

Page 3: Nationaal Lucht- en Ruimtevaartlaboratorium National Aerospace Laboratory NLR DXXX-1A The Free Flight Deck Society of Automotive Engineers (SAE) S-7, “Flight

Nationaal Lucht- en RuimtevaartlaboratoriumNational Aerospace Laboratory NLR

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Introduction to Free FlightRTCA definition: zones

Protected zone:– spatial, according

operational separation standards

– expected to remain free of other aircraft

Alert zone:– spatial or time based

zone around the protected zone

– conflict alerts are issued to the pilot

Page 4: Nationaal Lucht- en Ruimtevaartlaboratorium National Aerospace Laboratory NLR DXXX-1A The Free Flight Deck Society of Automotive Engineers (SAE) S-7, “Flight

Nationaal Lucht- en RuimtevaartlaboratoriumNational Aerospace Laboratory NLR

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Introduction to Free FlightEurocontrol’s definition

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Nationaal Lucht- en RuimtevaartlaboratoriumNational Aerospace Laboratory NLR

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Design of the Free Flight DeckStarting points

Operational Concept (probe the limits)– No Air Traffic Control– Air crew responsible for traffic separation– Focus on Free Flight Airspace– Central Traffic Flow Management active– Managed Airspace near airports (TMA)

Cruise flight only– Direct routing– Optimal cruise altitude

Limited scope– No Special Use Airspace (SUA)– No weather

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Nationaal Lucht- en RuimtevaartlaboratoriumNational Aerospace Laboratory NLR

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Design of the Free Flight DeckWhat do we need ?

Aircrew has to:– “see” other traffic– determine conflicts with other aircraft– resolve conflicts with other aircraft– avoid new conflicts with other aircraft– be alerted

Airborne Separation Assurance System (ASAS)

Investigate minimum standard:– flight deck design based on, and close to current

implementation (EFIS, FMS, TCAS)

Page 7: Nationaal Lucht- en Ruimtevaartlaboratorium National Aerospace Laboratory NLR DXXX-1A The Free Flight Deck Society of Automotive Engineers (SAE) S-7, “Flight

Nationaal Lucht- en RuimtevaartlaboratoriumNational Aerospace Laboratory NLR

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Design of the Free Flight DeckASAS equipment

“See” other traffic– Automatic Dependent Surveillance - Broadcast

(ADS-B), Traffic Information Service - Broadcast (TIS-B)– Cockpit Display of Traffic Information (CDTI)

Determine and resolve conflicts with other aircraft– Conflict Detection and Resolution (CD&R)

Avoid new conflicts with other aircraft– Predictive ASAS (PASAS)

Be alerted– Alerting logic

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Design of the Free Flight DeckConflict definition

A conflict is defined as a potential intrusion of the protected zone in the near future

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Nationaal Lucht- en RuimtevaartlaboratoriumNational Aerospace Laboratory NLR

DXXX-9A

Design of the Free Flight DeckConflict Detection & Resolution

ownship

intruder

minimum distance

protected zone intruder

avoidance vector

advised vector

1. heading change

2. speed change

not shown: 3. vertical speed change

Page 10: Nationaal Lucht- en Ruimtevaartlaboratorium National Aerospace Laboratory NLR DXXX-1A The Free Flight Deck Society of Automotive Engineers (SAE) S-7, “Flight

Nationaal Lucht- en RuimtevaartlaboratoriumNational Aerospace Laboratory NLR

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Design of the Free Flight DeckCockpit Display ofTraffic Information

Navigation Display– Traffic Symbology– Conflict Detection– Resolution Advisories– Vertical Navigation

Display– Extra EFIS Control

Panel functionality

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Design of the Free Flight Deck Predictive ASAS

“no-go” bands for– track/heading– vertical speed– speed

Page 12: Nationaal Lucht- en Ruimtevaartlaboratorium National Aerospace Laboratory NLR DXXX-1A The Free Flight Deck Society of Automotive Engineers (SAE) S-7, “Flight

Nationaal Lucht- en RuimtevaartlaboratoriumNational Aerospace Laboratory NLR

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Using the Free Flight DeckNLR studies on Free Flight

Studies on Airborne Separation Assurance, the flight deck perspective:– Conceptual design and off-line validation– Safety analysis– 1997 human-in-the-loop experiment– Cost/benefit analysis– Avionics requirements study– Critical conflict geometry study– 1998 human-in-the-loop experiment

In co-operation with NASA, FAA and RLD

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Nationaal Lucht- en RuimtevaartlaboratoriumNational Aerospace Laboratory NLR

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Using the Free Flight Deck1997 human-in-the-loop experiment Traffic Densities:

– Single– Double– Triple

Level of Automation:– Manual– Execute Combined– Execute Separate

Non-Nominal:– Other aircraft failures/events– Own aircraft failures/events– Delay time increased

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Nationaal Lucht- en RuimtevaartlaboratoriumNational Aerospace Laboratory NLR

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Using the Free Flight Deck1997 human-in-the-loop experiment

Acceptability: – 91.5% (single), 83.0% (double), 78.7% (triple)

Safety: – 88.3% (single), 75.5% (double), 71.3% (triple)

Workload:– ratings less than 40, indicating “costing some effort”

Across all densities, across all sessions, across all subject pilots, including non-nominal events

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Using the Free Flight Deck1998 human-in-the-loop experiment

Goals– study the transition to Free Flight Airspace (in space) – study the transition towards Free Flight in time

Starting points:– equipping aircraft should be immediately beneficial to

the airlines– equipping should be economy driven in stead of

mandatory– benefit the equipped aircraft, without excluding the

unequipped aircraft

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Using the Free Flight Deck1998 human-in-the-loop experiment

Three ATM operational scenarios with Free Flight elements defined, implemented and tested:– Flight Level– Protected Airways– Full Mix

Experiment matrix– Traffic Density - low density versus high density– Equipage - 25% versus 75% ASAS equipped– ATM operational concept - Flight Level, Protected

Airways and Full Mix

Page 17: Nationaal Lucht- en Ruimtevaartlaboratorium National Aerospace Laboratory NLR DXXX-1A The Free Flight Deck Society of Automotive Engineers (SAE) S-7, “Flight

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Using the Free Flight Deck1998 human-in-the-loop experiment

> 85% of responses indicate FF acceptable or better

Acceptability, traffic density effect(Airways & Mixed procedure only)

0

20

40

60

80

100

Perfect Favorable Acceptable Undesirable Completelyundesirable

Per

cen

tag

e

Medium

High

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Using the Free Flight Deck1998 human-in-the-loop experiment

> 85% of responses indicate FF as safe or safer than ATC Safety, traffic density effect

(Airways & Mixed procedure only)

0

20

40

60

80

100

FF muchsafer

FF safer Same ATC safer ATC muchsafer

Per

cen

tag

e

Medium

High

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Using the Free Flight Deck1998 human-in-the-loop experiment

Workload measurement: – Subjective by means of

questionnaires with Rating Scale of mental Effort (RSME)

– Objective by means of Eye-Point-Of-Gaze measurements

Scan randomness (entropy) used as objective metric for workload

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Using the Free Flight Deck1998 human-in-the-loop experiment

Workload: sensitive to ATM operational scenario

Pilot objective workloadTwo-way interaction of ATC

procedure and equipage (p<0.048)

-1

-0.8

-0.6

-0.4

-0.2

0

0.2

0.4

0.6

0.8

1

Equipage 25% Equipage 75%

Equipage

Entr

opy

(Z-s

core

)

Protected AirwaysFull Mix

Pilot subjective workloadTwo-way interaction of ATC

procedure and equipage (p<0.076)

-1

-0.8

-0.6

-0.4

-0.2

0

0.2

0.4

0.6

0.8

1

Equipage 25% Equipage 75%

Equipage

RSM

E (Z

-sco

re)

Protected AirwaysFull Mix

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Conclusions and Recommendations

The feasibility of Free Flight with Airborne Separation Assurance could not be refuted , based on 7 NLR studies on Free Flight

The future ATM design has to be chosen very carefully, since the design itself affects pilot and controller workload considerably

The flightdeck crew was able to handle much higher traffic densities than the ground controller(distributed versus centrally organised nature)

Free Flight might be a solution for current airspace capacity problems

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Future Plans

Human Interaction Experiment, using Internet gaming facilities (scheduled June 2000)(we need many volunteering pilots for this, to register please contact [email protected] or [email protected])

Flight testing of ASAS equipment, using “real” data– using NLR and possibly NASA laboratory aircraft

Simulation experiments to study:– the effect of real ADS-B characteristics– the use of Free Flight equipment in Managed Airspace– the integration of traffic, weather and terrain information

in the cockpit

Page 23: Nationaal Lucht- en Ruimtevaartlaboratorium National Aerospace Laboratory NLR DXXX-1A The Free Flight Deck Society of Automotive Engineers (SAE) S-7, “Flight

Nationaal Lucht- en RuimtevaartlaboratoriumNational Aerospace Laboratory NLR

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Demonstrations Research Flight Simulator: Free Flight demo

NLR’s ATC Research Simulator NARSIM

NLR’s Research Flight Simulator - Next Generation

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Contact / More information

NLR Free Flight web site:http://www.nlr.nl/public/hosted-sites/freeflight

E-mail/phone:Rob Ruigrok: [email protected], +31 20 511 3595Jacco Hoekstra: [email protected], +31 20 511 3775Ronald van Gent: [email protected], +31 20 511 3760

Mail:Nationaal Lucht- en RuimtevaartlaboratoriumAnthony Fokkerweg 21059 CM AmsterdamThe Netherlands