Stereopsis cueing effects on hover-in-turbulence performance in a simulated rotorcraft
By: Russell V. Parrish, Steven P. Williams.
Contributors: Williams, Steven P.; Langley Research Center.; United States. Army Aviation Research and Development Command.; United States. Army Aviation Systems Command.
Series: NASA technical paper -- 2980.; AVSCOM technical report -- 90-B-002.
Publisher: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division; For sale by the National Technical Information Service
Published: 1990
Place of publication: Washington, D.C; Springfield, Va
Language: eng
Format: Microform
Number of pages: 59
Subjects: Aeronautical instruments -- Display systems.; Three-dimensional display systems.; Stereoscope.; Helicopters -- Aerodynamics -- Computer simulation.; Helicopters -- Piloting.; Helicopter flight simulators.; Cues.; Display devices.; Flight simulation.; Hovering.; Pilot performance.; Rotary wing aircraft.; Turbulence.
Notes: Prepared at Langley Research Center and the Joint Research Programs Office, USAAVRDA-AVSCOM.

Includes bibliographical references (p. 13).

Also available via Internet from the NASA Technical Report Server web site. Address as of 4/20/06: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19900011688%5F1990011688.pdf ; current access is available via PURL.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1990]. 1 microfiche : negative.