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Helmet-Mounted Displays: - USAARL - The - U.S. Army

Helmet-Mounted Displays: - USAARL - The - U.S. Army

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Image Sources 41<br />

AMLCDs employ an array of individual pixels, each controlled by an<br />

electronic switch (Tannas, 1985). <strong>The</strong> most successful active matrix<br />

approach to addressing pixels uses thin film transistors (TFTs). In this<br />

approach, a TFT and a capacitor are used to switch each LC cell on and off.<br />

LCDs can be monochrome or full color. Monochrome LCDs usually<br />

use a backlight consisting of one or more fluorescent lamps, a reflector, and<br />

a diffuser. Less frequently used is a backlight where the light source is an<br />

electroluminescent panel. [See following section.] Approaches to<br />

achieving color LCDs are numerous and increasing every day. One<br />

approach is similar to the additive color method employed in modern CRT<br />

displays. In this approach, pixels are composed of three or more color<br />

subpixels. By activating combinations of these subpixels and controlling<br />

the transmission through each, a relatively large color gamut can be<br />

achieved.<br />

Backlighting is an important issue with LCDs and even more important<br />

for HMD designs based on LCDs. In general, backlights must be efficient<br />

(> 40 lumens/watt), produce high luminance (> 20,000 fL) (critical due to<br />

the poor through-put of LCDs), have high luminance uniformity (< 20%<br />

variation), have long life (>30,000 hours), and have a wide dimming range<br />

(> 5000:1) (Allen et al., 1995). Research is ongoing to achieve and/or<br />

exceed these requirements for military aviation applications (Altadonna,<br />

1996; Jiang, 1996; Kalmanask and Sundraresan, 1996). For HMDs, two<br />

options are possible: (a) <strong>The</strong> backlight is physically located away from the<br />

LCD, i.e., elsewhere in the aircraft or (b) a miniature backlight must be<br />

used. Mounting the backlight in the aircraft places additional luminance<br />

requirements on the backlight and the aircraft designers, since space,<br />

weight, and power demands must be addressed. Integrating the backlight<br />

with the display requires the development of subminiature (

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