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 Introduction • Purpose – Performance evaluation of a prototype binocular, WFOV, “off-visor” HMD – Army’s 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 Introduction • Purpose – Test key performance attributes • FOV • Resolution – Test key ergonomic attributes • Eye box • Binocular alignment/stability • Head borne weight/CG Introduction • Test Methods – NVESD Near Eye Display Test Station employed for all tests except system weight and CG – Weight/CG • CG determined by analysis WFOV HMD Goals • Risk mitigation effort • Parmeter – Binocular+off-visor Display presentation • Stability/alignment Combination technique Head borne weight • Profile Obscurations – 4.1 lb+Binocular IPD Range • Stability/alignment Monocular eye box Eye relief – Eye relief+FOV FOV • Profile/CG Minimum overlap Resolution Platform demo of Binocular divergence emerging technology Binocular dipvergence – LCD vs. CRT Goal Binocular/Biocular Off-visor 4.5 lbs w/O2 mask minimized 59-74 mm 15 mm 75 mm >40° horizontal >30° 0.5 cy/mr -0.5 to +0.2 prism diopters +/- 0.1 prism diopters System Evaluation Display unit • Description – Display unit (DU) • Binocular optical support structure (BOSS) • Relay optics assemblies • Visor/combiner – Helmet unit (HU) – Electronics Unit (EU) Helmet unit System Evaluation • Description- Display unit BOSS Visor/combiner Relay optic assembly(right) System Evaluation • Description- Helmet unit LCD cables Retention/retraction Interface PCB Helmet shell Suspension fit latches Main cable 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. System Evaluation • Performance test results Elevation Angle (degrees) – FOV 20 ELNomR 20 10 ELNomL ELWidR ELWidL 0 ELNarR ELNarL 10 20 20 30 30 20 10 0 10 20 AZNomR AZNomL AZWidR AZWidL AZNarR AZNarL Azimuth Angle (degrees) 30 30 System Evaluation • Performance test results – FOV • Inscribed rectangular areas Elevation Angle (degrees) 20 ELNomR 20 10 ELNomL ELWidR ELWidL 0 ELNarR ELNarL 10 20 20 30 30 Test Condition IPD Setting Sens IPD Nominal 66 mm Wide 74 mm Narrow 59 mm 20 10 0 10 20 AZNomR AZNomL AZWidR AZWidL AZNarR AZNarL Azimuth Angle (degrees) 30 30 Binocular 16X9 Binocular 4X3 R-Mono16X9 R-Mono4X3 Horiz.(°) Vert.(°) Horiz.(°) Vert.(°) Horiz.(°) Vert.(°) Horiz.(°) Vert.(°) 48.5 27.3 39.0 29.3 39.0 21.9 35.0 26.3 46.8 26.3 38.8 29.1 38.7 21.8 34.6 26.0 42.8 24.1 38.0 28.5 35.2 19.8 33.9 25.4 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. System Evaluation • Performance test results: Resolution – Methods Raw data: Distortion correction applied: System Evaluation • Performance test results: Resolution Right channel 1 Left channel 1 1 0.75 Modulation Modulation 0.75 M odRH M odRV 0.5 M odLH M odLV 0 0.5 0.25 0.25 0 1 0 0 0 0.2 0.4 FreqRH FreqRV Cycles/ mr 0.6 0 0.8 0 .8 0 0.2 0.4 FreqLH FreqLV Cycles/ mr 0.6 0.8 .8 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 System Evaluation • Performance test results: Eye box Units in mm Luminance DC contrast Nyquist contrast 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. 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 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 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 System Evaluation • Performance test results: Alignment/Stablity Test parameter Visor removal/replacement IPD adjustment right channel (center) IPD adjustment right channel (wide) IPD adjustment right channel (narrow) +/- 2 mm shift in eye box Visor see-through deviation samples 20 10 10 10 86 10 RMS (mr) Peak-to-peak (mr) Divergence Dipvergence Divergence Dipvergence 0.62 0.55 1.14 1.21 0.54 0.75 1.28 2.01 0.91 0.42 2.43 1.30 0.76 0.53 2.66 1.90 0.29 0.24 1.71 1.59 0.19 0.29 0.55 1.04 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. System Evaluation • Performance test results: Weight/CG Description WFOV BOSS assembly HGU-56P special Helmet (includes fit and pads) Video board, cover, 1' cable wt (lb) 1.63 1.63 109 0.24 MEASURED SUBTOTAL ESTIMATED SUBTOTAL O2 mask MBU-12/P TOTAL 1593 2088 273 1866 3.51 4.60 0.60 4.11 Misc Subassemblies Visor Optics assy (includes backlight,IF board) wt (g) 96.3 130.2 wt (lb) 0.21 0.29 mm 41 54 in 1.63 2.14 estimated Center of Gravity from Tragion Center1 forward (z) above (y) 1 wt (g) 741.9 741.7 Uses measured weights, does NOT include Head wt./CG CG from pupil center y (in) z (in) 2.46 -1.33 -3.50 1.44 1.59 -0.92 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 Conclusions • WFOV promising performance attributes: – FOV >40° 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. 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