ENHANCED FLIGHT VISION SYSTEMS: PRESENCE OF RUNWAY MARKINGS AND - - PowerPoint PPT Presentation

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ENHANCED FLIGHT VISION SYSTEMS: PRESENCE OF RUNWAY MARKINGS AND - - PowerPoint PPT Presentation

ENHANCED FLIGHT VISION SYSTEMS: PRESENCE OF RUNWAY MARKINGS AND VISIBILITY EFFECTS ON PILOT PERFORMANCE AN D R E W GR E E N H I L L S E P T E MB E R 1 5 T H , 2 0 1 7 AGENDA What is an Enhanced Flight Vision System (EFVS) Motivation


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SLIDE 1

ENHANCED FLIGHT VISION SYSTEMS:

PRESENCE OF RUNWAY MARKINGS AND VISIBILITY EFFECTS ON PILOT PERFORMANCE

AN D R E W GR E E N H I L L S E P T E MB E R 1 5 T H, 2 0 1 7

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SLIDE 2

AGENDA

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  • What is an Enhanced Flight Vision System (EFVS)
  • Motivation
  • Background
  • Millimeter wave radar (MMW)
  • Forward looking infrared (FLIR)
  • Light detection and ranging (LiDAR)
  • Situational awareness
  • Visual cues
  • Objective
  • Pilot performance
  • Research Plan
  • Anticipated Contributions
  • Proposed Timeline
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SLIDE 3

WHAT IS EFVS

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Enhanced Flight Vision Systems is defined as: “an installed aircraft system which uses an electronic means to provide a display of the forward external scene topography through the use of imaging sensors” (FAA AC 90-106A) Therefore, an EFVS must:

  • Use real time imaging sensor, like a FLIR
  • Use heads-up display
  • Be an installed system on the aircraft

EFVS is different from both synthetic vision and enhanced vision systems

Images from EFVS presentation by Terry King

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SLIDE 4

MOTIVATION

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  • New sensors have enabled EFVS to evolve
  • Millimeter Wave Radar
  • Light Detection and Ranging
  • Multispectral IR
  • EFVS has the ability to extend the capability of aircraft operations
  • Landing below weather minimums
  • Reducing delays while waiting for weather to clear
  • With advancements in EFVS, the FAA is trying to get a head start on operational

approvalof these systems

  • Not just setting sensor requirements
  • How they affect pilot performance
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SLIDE 5

MILLIMETER WAVE RADAR

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Capabilities

  • Penetration of various atmospheric

conditions due to frequencies in which it operates

  • Some weather phenomenon, such

as fog, light clouds, and some precipitation have shown to improve contrast

  • MMW Radar returns different

textures for different objects and terrain types Constraints

  • Low resolution and noisy signals

generated; clustering and filtering techniques could be required

  • Cannot detect and display runway

markings

  • Major trade-offs between sensitivity

and range of the sensors

Image from Yang, 1994

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SLIDE 6

FORWARD LOOKING INFRARED (FLIR)

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Capabilities

  • Thermal imaging sensor allows for

night vision and low-light scenarios

  • Specifically help with runway incursions
  • Provides distinction between

concrete and grass areas at most times

  • Can be beneficial in haze or smoke

Constraints

  • Dissipation rates are different for

materials, which causes thermal reversals and ghosting

  • Weather greatly affects the thermal

imaging capabilities

  • Solar Load
  • Precipitation
  • Wind speed
  • Some types of FLIR can create

contrast issues by using the iHot spot technique

Image from Doehler and Korn, 2006

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SLIDE 7

LIGHT DETECTION AND RANGING (LIDAR)

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Although many sensors can use a combination, LiDAR typically is utilized with an INS and GPS system Capabilities

  • Able to detect pavement markings
  • n roads and runways
  • LiDAR is typically more accurate

compared to MMW and FLIR sensors, could be due to INS/GPS Constraints

  • Laser scanning techniques pose a

safety vs. effectiveness tradeoff

  • Limitations with respect to

aerosol/cloud particles as well as weather

  • Databases for checking GPS/INS are

not fully implemented and could lead to extreme errors

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SLIDE 8

SITUATIONAL AWARENESS

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Situational Awareness is defined as a state of knowledge with three levels of perception, interpretation and prediction (Endsley) Level 1 - Perception

  • Flaps configuration
  • Gear configuration
  • Airspeed for flap and gear deployment
  • Power setting
  • Localizer deviation
  • Glideslope deviation
  • Visual of the runway centerline
  • Visual of the runway sides
  • Visual of top and bottom of the runway
  • Visual of the touchdown markers
  • Visual of the horizon

Level 2 - Interpretation

  • Correct configuration of gears and flaps
  • Appropriate speed and power settings
  • On the desired glide path, typically about 3°
  • On the extended centerline of the runway
  • Whether the landing will be made in the first

3rd of the runway

  • When to flare during landing

Level 3 - Prediction

  • Travel path of traffic and conflicts
  • Travel path of the aircraft and if it conflicts

with any obstacles or terrain

  • Location of touchdown spot on the runway
  • What the next objective of the mission is and

how to get there

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SLIDE 9

VISUAL CUES

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Visual cues for approach and landing mainly include:

  • Terrain
  • Airport Environment
  • Factors of a stabilized approach

The main visual cues of a stabilized approach are part of Level 1 situational awareness

Level 1 - Perception

  • Flaps configuration
  • Gear configuration
  • Airspeed for flap and gear deployment
  • Power setting
  • Localizer deviation
  • Glideslope deviation
  • Visual of the runway centerline
  • Visual of the runway sides
  • Visual of top and bottom of the runway
  • Visual of the touchdown markers
  • Visual of the horizon

Image from Marks, 2017

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SLIDE 10

SITUATIONAL AWARENESS AND VISUAL CUES

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In the figure, the Level 2 situational awareness tasks on the left To the right of each Level 2 task, are the Level 1 tasks that directly affect it Certain forms of EFVS have:

  • Range issues - Blue
  • No way of displaying runway

markings - Red

  • Glideslope deviation
  • Visual of top and bottom of

runway

  • Visual of the horizon

On the desired glide path, typically about 3°

  • Localizer deviation
  • Visual of the runway centerline
  • Visual of runway sides
  • Visual of the touchdown

markers

On the extended centerline of the runway

  • Visual of the touchdown

markers

  • Visual of top and bottom of

runway

Whether the landing will be made in the first 3rd of the runway

  • Visual of runway sides
  • Visual of top and bottom of

runway

  • Visual of the horizon

When to flare during landing

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SLIDE 11

OBJECTIVE

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The objective is twofold:

  • Find the effect of how the visibility range of an EFVS affects the pilot performance on

approach and landing

  • Find the effect that the absence of runway markings in EFVS has on the pilot

performance during approach and landing Situational Awareness Display Characteristics Visual Cues Sensor Properties

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SLIDE 12

FITTING IN PILOT PERFORMANCE

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Pilot performance for approach and landing can be measured primarily by a stabilized approach and some other factors A stabilized approach is when the following criteria are met:

  • Correct configuration of gears and flaps
  • Appropriate speed and power settings
  • On the desired glide path, typically

about 3°

  • On the extended centerline of the

runway

  • Whether the landing will be made in the

first 3rd of the runway

The stabilized approach criteria align with level 2 of situational awareness Sensor properties Visual cues (Level 1 situational awareness) Level 2 situational awareness (Stabilized approach criteria) Pilot performance

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SLIDE 13

EXPERIMENTAL SETUP

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Simulator Hardware

  • 4 separate monitors
  • Three make up the
  • utside view of the

environment

  • The fourth screen is

the instrument panel.

  • A yoke
  • Rudder pedals
  • Throttle control

system

  • Eye tracker
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SLIDE 14

INDEPENDENT AND DEPENDENT VARIABLES

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Independent Variables

  • Presence of runway markings in

EFVS

  • Binary true or false
  • Visibility range of EFVS
  • Fluctuates between 1, 3 or 12 statue miles

Dependent Variables

  • Stabilized approach criteria
  • Localizer/glideslope error
  • Altitude
  • Vertical speed
  • Airspeed
  • Heading
  • Latitude and longitude
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SLIDE 15

EXPERIMENT DESIGN

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Subjects

  • 21 pilots would be tested
  • Must be instrument rated and have

a minimum of 150 hours Base Conditions

  • Start at a 5 nautical mile approach
  • Be placed on the glideslope in a

cruise condition

  • No flaps added yet
  • The nav instruments would be

tuned into the localizer/glideslope Scenarios Each pilot would fly seven different approaches, listed below, these would be fully balanced using a Latin square

  • Basic approach, no EFVS
  • Approach with EFVS, runway markings and 12

sm visibility

  • Approach with EFVS, runway markings and 3

sm visibility

  • Approach with EFVS, runway markings and 1

sm visibility

  • Approach with EFVS, no runway markings and

12 sm visibility

  • Approach with EFVS, no runway markings and 3

sm visibility

  • Approach with EFVS, no runway markings and 1

sm visibility

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SLIDE 16

ANTICIPATED CONTRIBUTIONS

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  • Identify possible drawbacks or specific benefits of using EFVS
  • Specifically with respect to pilot performance during approach and landing
  • Results will be utilized in:
  • Issuing operational approvals for EFVS
  • Providing limitations for EFVS
  • The focus on specific visual cues, will hopefully allow the results to be more
  • perationally applied than sensor specific requirements
  • Planned papers
  • Previous literature review concerning the topic of EFVS
  • Paper summarizing the objective and results of the thesis
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SLIDE 17

SUMMARY

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Motivation: With EFVS able to extend the capability of aircraft operations, the implications these technologies have on pilot performance need to be investigated Background:

  • Each of these sensors have different capabilities and constraints
  • The situational awareness is in three levels: perception, interpretation and prediction
  • The visual cues and situational awareness of the pilot are intertwined since the

perception feeds into the interpretation of the stabilized approach Objective:

  • Find the effect of how the visibility range of an EFVS affects the pilot performance on

approach and landing

  • Find the effect that the absence of runway markings in EFVS has on the pilot

performance during approach and landing Research Plan:

  • Running a set of simulator trials with varying EFVS conditions
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SLIDE 18

NEXT STEPS

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  • 1. IRB Paperwork and approval – In process
  • Finalize consent form, invitations and debrief questionnaire
  • Hopefully submitted by next week
  • 2. Pilot testing – start after IRB submitted
  • Verify the experiment design and the data collection/analysis process
  • Notice any variables that should be added/removed
  • 3. Invite subjects to participate
  • Use YJFC and previous CEC pilot email lists to gather subjects
  • 4. Start subject testing and data analysis
  • 5. During the main portion of these experiments, writing the thesis will be done
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SLIDE 19

PROPOSED TIMELINE

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Week of 7 / 3 1 / 1 7 8 / 7 / 1 7 8 / 1 4 / 1 7 8 / 2 1 / 1 7 8 / 2 8 / 1 7 9 / 4 / 1 7 9 / 1 1 / 1 7 9 / 1 8 / 1 7 9 / 2 5 / 1 7 1 / 2 / 1 7 1 / 9 / 1 7 1 / 1 6 / 1 7 1 / 2 3 / 1 7 1 / 3 / 1 7 1 1 / 6 / 1 7 1 1 / 1 3 / 1 7 1 1 / 2 / 1 7 Written Proposal Proposal IRB Approval Invitations Subject Testing Data Analysis Conclusions Outline of Thesis Written Thesis Defense Week of 1 1 / 2 7 / 1 7 1 2 / 4 / 1 7 1 2 / 1 1 / 1 7 1 2 / 1 8 / 1 7 1 2 / 2 5 / 1 7 1 / 1 / 1 8 1 / 8 / 1 8 1 / 1 5 / 1 8 1 / 2 2 / 1 8 1 / 2 9 / 1 8 2 / 5 / 1 8 2 / 1 2 / 1 8 2 / 1 9 / 1 8 2 / 2 6 / 1 8 3 / 5 / 1 8 3 / 1 2 / 1 8 3 / 1 9 / 1 8 Written Proposal Proposal IRB Approval Invitations Subject Testing Data Analysis Conclusions Outline of Thesis Written Thesis Defense

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SLIDE 20

QUESTIONS

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Thank you all for your time

Questions