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oaioai:casi.ntrs.nasa.gov:19820017391

Conceptual design study for an advanced cab and visual system, volume 2

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Publication date
1980
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Abstract

The performance, design, construction and testing requirements are defined for developing an advanced cab and visual system. The rotorcraft system integration simulator is composed of the advanced cab and visual system and the rotorcraft system motion generator, and is part of an existing simulation facility. User's applications for the simulator include rotorcraft design development, product improvement, threat assessment, and accident investigation

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This paper was published in NASA Technical Reports Server.

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