Design Considerations and Preliminary Evaluation for an off-the-visor wide field of view HMD - PowerPoint PPT Presentation

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Design Considerations and Preliminary Evaluation for an off-the-visor wide field of view HMD

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Design Considerations and Preliminary Evaluation for an off-the-visor wide field of view HMD Russell S. Draper, Charles D. Balogh Night vision Electronic Sensors ... – PowerPoint PPT presentation

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Title: Design Considerations and Preliminary Evaluation for an off-the-visor wide field of view HMD


1
Design Considerations and Preliminary Evaluation
for an off-the-visor wide field of view HMD
  • Russell S. Draper, Charles D. Balogh
  • Night vision Electronic Sensors Directorate
  • Steven J. Robbins
  • Kaiser Electronics, San Jose, CA

2
Introduction
  • Purpose
  • Performance evaluation of a prototype binocular,
    WFOV, off-visor HMD
  • Armys interest in a Jet Fighter HMD?
  • Directed development for Objective Force Warrior
  • Multi-spectral head worn sensor system
  • Possible form binocular/see through vision
    system
  • Maintain expertise in state-of-the-art HMD
    technology

3
Introduction
  • Purpose
  • Test key performance attributes
  • FOV
  • Resolution
  • Test key ergonomic attributes
  • Eye box
  • Binocular alignment/stability
  • Head borne weight/CG

4
Introduction
  • Test Methods
  • NVESD Near Eye Display Test Station employed for
    all tests except system weight and CG
  • Weight/CG
  • CG determined by analysis

5
WFOV HMD Goals
  • Risk mitigation effort
  • Binocularoff-visor
  • Stability/alignment
  • Profile
  • 4.1 lbBinocular
  • Stability/alignment
  • Eye reliefFOV
  • Profile/CG
  • Platform demo of emerging technology
  • LCD vs. CRT

6
System Evaluation
Display unit
Helmet unit
  • Description
  • Display unit (DU)
  • Binocular optical support structure (BOSS)
  • Relay optics assemblies
  • Visor/combiner
  • Helmet unit (HU)
  • Electronics Unit (EU)

7
System Evaluation
  • Description- Display unit

BOSS
Visor/combiner
Relay optic assembly(right)
8
System Evaluation
  • Description- Helmet unit

LCD cables
Retention/retraction
Interface PCB
Helmet shell
Suspension fit latches
Main cable
9
System Evaluation
  • Performance test results FOV
  • Methods
  • Display active area driven to full on condition
  • Digital image frame captured with NEDTS WFOV CCD
    array sensor
  • Unique edge detection algorithm applied to
    captured image
  • Edge detection starts at center and propagates
    outward
  • Edge pixel values converted to angle space using
    NEDTS WFOV lens mapping.
  • Test performed on right and left channels, 3 IPD
    settings each with sensor located at IPD setting
    design eye position.

10
System Evaluation
  • Performance test results
  • FOV

11
System Evaluation
  • Performance test results
  • FOV
  • Inscribed rectangular areas

12
System Evaluation
  • Performance test results Resolution
  • Methods
  • Maximum contrast measured with NEDTS PMT sensor.
  • Display active area driven with 50 duty cycle
    square wave grid at Nyquist sample rate, ½, ¼,
    1/8 Nyquist rate
  • Digital image frame captured with NEDTS NFOV CCD
    array sensor
  • Localized distortion correction (3rd order
    warping horizontal or vertical) applied to
    captured image.
  • Row/column averaging performed.
  • Average cycle Michelson contrast computed for all
    viewable cycles.

13
System Evaluation
  • Performance test results Resolution
  • Methods

Raw data
Distortion correction applied
14
System Evaluation
  • Performance test results Resolution

Right channel
Left channel
15
System Evaluation
  • Performance test results Eye box
  • Methods
  • 2D scan of eye left and right side design eye
    location /-12 mm vertical and /-15 mm
    horizontal
  • 3 parameters measured at each scan position
  • Luminance
  • On/off contrast
  • Nyquist rate contrast
  • Plotted 50 contour of normalized data

16
System Evaluation
  • Performance test results Eye box

Units in mm Luminance DC contrast Nyquist
contrast
17
System Evaluation
  • Performance test results Alignment/Stablity
  • Methods
  • Visor removal/replacement
  • Single 5 mr spot at approximately 0,0 field
    position displayed in each channel
  • Visor removed and replaced 20 times
  • Field location of test spot measured with each
    trial
  • Relative change between right and left channels
    recorded.

18
System Evaluation
  • Performance test results Alignment/Stablity
  • Methods
  • IPD adjustment
  • Single 5 mr spot at approximately 0,0 field
    position displayed in each channel
  • IPD adjusted on single channel through all three
    settings for 10 trials
  • Field location of test spot measured with each
    trial for each channel
  • Relative change between right and left channel
    recorded

19
System Evaluation
  • Performance test results Alignment/Stablity
  • Methods
  • Eye position shift
  • 2-D Grid of 5 mr points displayed at
    approximately 4 increments
  • Sensor position moved in eye box from design eye
    location at nominal IPD /- 2 mm horizontally and
    vertically
  • Field location of test spot measured with each
    trial for each channel
  • Relative change between right and left channel
    for corresponding spots within the binocular
    overlap region recorded

20
System Evaluation
  • Performance test results Alignment/Stablity
  • Methods
  • Visor See through deviation
  • Collimated plus symbol generated with bright
    line theodolite outside of visor at specific
    field angle relative to DU.
  • NEDTS sensor with digital cross hair oriented to
    view collimated image until digital cross hair
    overlaped plus symbol
  • Visor removed
  • Theodolite adjusted to re-position plus symbol
    on cross hair
  • Theodolite change in azimuth/elevation recorded

21
System Evaluation
  • Performance test results Alignment/Stablity

22
System Evaluation
  • Performance test results Weight/CG
  • Methods
  • Shell, fit system, electronics,1 ft. cable
    weighed
  • Display unit weighed with visor and relay optics
  • Visor weighed separately
  • Right channel relay optics weighed separately
  • Total head borne weight computed from actual
    component weights
  • CG estimated from CAD data and actual component
    weights.

23
System Evaluation
  • Performance test results Weight/CG

24
Conclusions
  • WFOV prototype HMD incorporates several
    innovative design elements
  • Flexible optical mounts for durability
  • 3-point visor interface for improved visor
    positional repeatablity
  • Bifurcated v-shaped visor for narrow profile and
    visor stability
  • Integrated small footprint binocular optical
    support for stability
  • 3 position IPD adjustment with kinematic interface

25
Conclusions
  • WFOV promising performance attributes
  • FOV gt40 horizontal and 30 vertical for
    binocular viewing with approximately 30 overlap
  • Resolution nominally 0.75 cy/mr (currently
    display source limited)
  • Stability of binocular alignment better than 0.75
    mr RMS and 2.5 mr worst case.

26
Conclusions
  • WFOV performance concerns
  • Notable FOV vignetting occurs for narrow IPDs
  • IPD adjustment mechanism has no apparent effect
    on eye box position.
  • Notable resolution loss over small area of design
    eye box
  • Visor bifurcation causes small amount of image
    doubling at joint
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