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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 7<br />

<strong>The</strong> trend for increasing reliance on HMDs in aviation, as well as in<br />

other sectors of the <strong>Army</strong>, will continue. <strong>The</strong> U.S. <strong>Army</strong> Night Vision and<br />

Electronic Sensor Directorate (NVESD), Fort Belvior, Virginia, is<br />

developing an HMD under the Advanced Helicopter Pilotage (AHP)<br />

program (Perconti,1997). <strong>The</strong> AHP HMD is biocular, providing the same<br />

imagery to each eye. Its two optical channels each provide a 40º monocular<br />

circular FOV. When mounted on a helmet, the system provides a 30º (V)<br />

x 50º (H) total FOV with a 30º binocular overlap region.<br />

<strong>The</strong> United States and the United Kingdom of Great Britain and<br />

Northern Ireland have collaborated on the Covert Night/Day Operations for<br />

Rotorcraft (CONDOR) program. CONDOR is a research platform for<br />

demonstrating advanced visionics concepts and includes a variable FOV<br />

HMD based on high resolution miniature active matrix liquid crystal<br />

displays (AMLCDs) (Kanahele and Buckanin, 1996).<br />

<strong>The</strong> U.S. <strong>Army</strong> and the Defense Advanced Research Projects Agency<br />

(DARPA) have funded a number of additional aviation HMD concepts<br />

based on FP technologies (Girolamo, Rash, and Gilroy, 1997). <strong>The</strong>se<br />

include the Miniature Flat Panel for Aviation (MFP/A) program which has<br />

as its goal the investigation of using miniature FP technology displays in<br />

the development of an HMD for use in rotary-wing aircraft and the Aircrew<br />

Integrated <strong>Helmet</strong> System (AIHS) Comanche Compatibility program which<br />

has as its goal the development of an HMD design using the <strong>Helmet</strong> Gear<br />

Unit No. 56/P (HGU-56/P) flight helmet as the platform. A partial<br />

summary of current rotary-wing HMD programs (both fielded and under<br />

development) by Belt et al. (1997) is provided in Table 1.1. An excellent<br />

attempt to develop a taxonomy and philosophy of HMD systems has been<br />

made by Brindle, Marano-Goyco, and Tihansky (1995).<br />

This book is intended to serve as both a checklist and a guide for<br />

designers of such future integrated helmet and display systems for rotarywing<br />

aircraft. In this book: a) salient performance parameters of such<br />

systems are identified; b) recommendations for values of these parameters<br />

are suggested, based on past research and the opinions of subject matter<br />

experts; c) an analysis of potential health and safety hazards is provided;<br />

d) a human factors engineering assessment (HFEA) is provided; and e)<br />

lessons learned from previously fielded U.S. <strong>Army</strong> HMD systems are<br />

summarized. However, this book is not a cookbook for building an<br />

integrated helmet and display system. <strong>The</strong> design of such a system is<br />

strongly dependent on its purpose, user requirements, and the environment<br />

within which it is intended to operate.

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