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    XIX AIMAS December 7th 2006

    Operational Issues in

    Aided Night Vision Flight

    Pierandrea Trivelloni

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    XIX AIMAS December 7th 2006

    Night Vision DevicesNVGs vs FLIR

    Night vision goggles - reflected energy Image reflective contrast

    Require at least some illumination

    Penetrate moisture effectively

    Attenuated by smoke, haze and dust

    Forward Looking InfraRed - emitted energy

    Images thermal contrast

    Totally independent of light

    Penetrates smoke and haze

    Attenuated by moisture (humidity)

    B 10

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    XIX AIMAS December 7th 2006

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    XIX AIMAS December 7th 2006

    Light Sensitivity

    Wavelength (nanometres)InfraredInfraredInfraredVisible LightVisible LightVisible Light

    RelativeResponse(%)

    HumanEye

    GEN-IIINVG

    100

    80

    60

    40

    20

    0

    400 500 600 700 800 900 1000

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    XIX AIMAS December 7th 2006

    Light Sensitivity

    Night SkyIrradiation

    Wavelength (nanometres)

    RelativeResponse(%)

    HumanEye

    GEN-IIINVG

    100

    80

    60

    40

    20

    0

    400 500 600 700 800 900 1000

    InfraredInfraredInfraredVisible LightVisible LightVisible Light

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    XIX AIMAS December 7th 2006

    Image Intensification Process

    PhotocathodeMicrochannel Plate

    Electron MultiplierPhosphor Screen

    LightLight

    Secondary Electrons IndividualMultiplierTube

    InputElectron

    Voltage +-

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    XIX AIMAS December 7th 2006

    Visual Characteristicsof Night Vision Goggles

    Reduced visual acuity 7/10 under ideal conditions

    5/10 at best in aircraft

    May be 3/10 or worse at mean starlightand/or low contrast conditions

    Limited FOV - 40 degrees

    Monochromatic image - no color contrast

    Limits object detection and recognition

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    XIX AIMAS December 7th 2006

    Night Environment

    High light level (HLL): > 2.2 mluxEquivalent to 20% moon disc @ 30

    Best HLL: 50% moon disc @ 4080Skyglow: up to13 below the horizon

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    NVGs Visual Acuity

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    The Role of NVG CockpitLighting

    Spatial Disorientation - MH-60

    Spatial Disorientation - A/OA-10* Wire Strike - MH-60

    Spatial Disorientation - A/OA-10*

    Spatial Disorientation - F-16 Unknown / Mid-Air Collision - HH-60s

    Brown Out / Loss of Control - MH-53

    Loss of SA / Mid-Air Collision - F-16*

    Misperception / Hard Landing - HH-60

    Misperception / Tail Rotor Strike - MH-53

    * Significant lighting deficiencies

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    XIX AIMAS December 7th 2006

    Mishap Primary Cause Factors leading to NVG-related CFIT mishaps

    Task saturation

    Breakdown of crew coordination

    Poor judgment

    Fatigue & Workload

    Overconfidence/Complacency

    Training deficiencies/Inexperience

    The culminating event is

    breakdown in instrument crosscheck

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    XIX AIMAS December 7th 2006

    Goggle Effects on Unaided FOVand Scan Patterns

    NVGs are used to look outside the aircraft

    Cockpit Instruments and displays (except aHUD) are viewed by looking beneath oraround the goggles

    The goggle obstructs a +/- 45 degree coneof vision (40 degrees + 2.5 degreessurrounding the image)

    Pilots must modify their cockpit scan toaccommodate this obstruction of vision

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    XIX AIMAS December 7th 2006

    The Role of NVG Cockpit Lighting

    Incompatible or partially compatible lighting is aparticular hazard

    The natural tendency is to turn it down in order

    to reduce blooming and/or reflections However -- as a rule, an incompatible display

    cannot be made compatible by turning it down

    The result is a display that is less readable, orunreadable, AND still incompatible with NVGs

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    XIX AIMAS December 7th 2006

    The Role of NVG Cockpit Lighting

    Poor illumination of primary flight instrumentshas been a significant problem in NVGoperations (30% of mishaps)

    It can take up to 10 seconds (515) to adapt

    from a bright NVG image to a dim cockpitdisplay

    Howard CM, Riegler J T, Martin J JAviation Space and Envir. J ournal: J une 2001

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    The Role of NVG Cockpit Lighting

    Early Chromatic After-effects

    Transitory

    Grayish view of green and white targets

    Attenuated by increasing cockpitdisplaysluminance and/or reducing the ANVISdisplay luminance

    Moffitt K, Rogers SP, Cicinelli JAviation, Space and Envir. J ournal: February1988

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    XIX AIMAS December 7th 2006

    The Role of NVG Cockpit Lighting

    Early Chromatic After-effects

    Transitory

    Grayish view of green and white targets

    Attenuated by increasing cockpitdisplaysluminance and/or reducing the ANVISdisplay luminance

    Moffitt K, Rogers SP, Cicinelli JAviation, Space and Envir. J ournal: February1988

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    XIX AIMAS December 7th 2006

    Post-Flight Considerations Post-flight eye strain

    May reflect poor pre-flight focusing Temporary depth perception problems

    Due to incorrect IPD settings

    Fatigue due to several factorsPhysical

    Mental

    Sensory

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    Sensor Integration

    Effective visual perception through naturaland technological sensors

    Comparison between both perceptions

    Increase in sensorial and mental workload Integration among several technologies

    Computer generated imagery

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    Fusion Imagery

    Light Intensifier (NVGs)

    Infra-red (FLIR)

    Grey Fused (computer generated)

    Color Fused (computer generated)

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    XIX AIMAS December 7th 2006

    Training vs Demonstration

    Training implies that the trainee hasundergone a process resulting in an actualchange in behavior, performance, perceptionor response

    not just informedregarding some fact orprincipal

    Merely demonstrating something is NOT

    training

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    Next Generation Aircrew

    Information management skillsSituation awareness

    Spare mental capability

    Team-worker

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    In certain circumstancesSpatial Disorientation is

    a normal physiological responseWilliam E. Berkley, Col, USAF, MC,CFS

    AFRL, Mesa (AZ)