Abstract
Wright Laboratory's Variable-Stability In-Flight Simulator Test Aircraft (VISTA) NF-16D is the newest in-flight simulator in the USAF inventory. This unique research aircraft will perform a multitude of missions: evaluate flight characteristics of new aircraft that have not yet flown, perform research in the areas of flying qualities, flight control design, pilot-vehicle interface, weapons and avionics integration, and train test pilots and engineers. The VISTA is being upgraded to enhance its simulation fidelity and its research capabilities through the addition of a programmable Helmet-Mounted Display (HMD) and Head-up Display (HUD) in the front cockpit. The programmable HMD system consists of a GEC Marconi Avionics Viper II Helmet- Mounted Optics Module integrate with a modified Helmet Integrated Systems Limited HGU-86/P helmet, the Honeywell Advanced Metal Tolerant tracker, and a GEC-Marconi Avionics Programmable Display Generator. The monocular HMD system is designed for growth to stroke-on-video, binocular capability. Lessons-learned in the VISTA HMD development are reviewed. An outline of the proposed VISTA HMD demonstration flight is given to highlight the VISTA programmable display system capabilities.
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