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