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

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

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Introductory Overview 11<br />

aviator to perform a certain number of complex tasks. <strong>The</strong> performance of<br />

these tasks is impacted by aviator skills and capabilities (user properties),<br />

and by the characteristics of the HMD. <strong>The</strong> operational environment may<br />

include high speed, low level flight, during low illumination and/or adverse<br />

weather conditions. Eggleston (1997) developed a model which maps<br />

aviator tasks (e.g., navigation, unmasking maneuver, etc.), user properties<br />

(e.g., perception, organization, etc.), and HMD characteristics (e.g., FOV,<br />

resolution, etc.) for specific missions and mission elements. This type of<br />

analysis is essential in ensuring an optimal HMD design which meets the<br />

needs of the aviator and the mission.<br />

In summary, the design specifications for any system must be guided<br />

by these criteria convolved with hardware limitations, human performance<br />

strengths and weaknesses, and good human factors engineering practices.<br />

[Note: This book does not tackle the complex, and still unresolved, issue<br />

of HMD imagery information content, which includes the selection of types<br />

and quantity of data to be presented, the symbols used, or their placement<br />

within the displayed imagery. Interested readers may find information in<br />

these areas in Craig, Marshall, and Jordan (1997), Drewery, Davy, and<br />

Dudfield (1997), and Murray (1997).]<br />

<strong>Helmet</strong>-<strong>Mounted</strong> <strong>Displays</strong> Overview<br />

Melzer and Moffitt (1997) describe an HMD as minimally consisting<br />

of “an image source and collimating optics in a head mount.” For the<br />

purpose of this book, we expand this description to include a visual<br />

coupling system, which performs the function of slaving head and/or eye<br />

positions and motions to one or more aircraft systems. Figure 1.5 presents<br />

the basic <strong>Army</strong> aviation HMD as a block diagram in which there are four<br />

major elements: image source (and associated drive electronics), display<br />

optics, helmet, and head/eye tracker. <strong>The</strong> image source is a display device<br />

upon which sensor imagery is produced. <strong>The</strong>se sources typically have been<br />

miniature CRTs or I 2 tubes. Other miniature displays based on FP<br />

technologies rapidly are becoming alternate choices. <strong>The</strong> display optics<br />

are used to couple the display imagery to the eye. <strong>The</strong> optics generally<br />

magnify and focus the display image. <strong>The</strong> helmet, while providing the<br />

protection for which it was designed originally, serves additionally as a<br />

platform for mounting the image source and display optics. <strong>The</strong> tracking

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