Effects of Inboard Horizontal Field of View Display Limitations on Pilot Path Control During Total In-Flight Simulator (Tifs) Flight Test

By National Aeronautics and Space Administration

A flight test was conducted aboard Calspan's Total In-Flight Simulator (TIFS) aircraft by researchers within the External Visibility System (XVS) element of the High-Speed Research program. The purpose was to investigate the effects of inboard horizontal field of view (FOV) display limitations on pilot path control and to learn about the TIFS capabilities and limitations for possible use in future XVS flight tests. The TIFS cockpit windows were masked to represent the front XVS display area and the High-Speed Civil Transport side windows, as viewed by the pilot. Masking limited the forward FOV to 40 deg. horizontal and 50 deg. vertical for the basic flight condition, With an increase of 10 deg. horizontal in the inboard direction for the increased FOV flight condition. Two right-hand approach tasks (base-downwind-final) with a left crosswind on final were performed by three pilots using visual flight rules at Niagara Falls Airport. Each of the two tasks had three replicates for both horizontal FOV conditions, resulting in twelve approaches per test subject. Limited objective data showed that an increase of inboard FOV had no effect (deficiences in objective data measurement capabilities were noted). However, subjective results showed that a 50 deg. FOV was preferred over the 40 deg. FOV.Kramer, Lynda J. and Parrish, Russell V. and Williams, Steven P. and Lavell, Jeffrey S.Langley Research CenterFIELD OF VIEW; FLIGHT TESTS; IN-FLIGHT SIMULATION; PILOT PERFORMANCE; FLIGHT CONTROL; HIGH SPEED; VISIBILITY; VISUAL FLIGHT RULES; COCKPITS; HEAD-UP DISPLAYS; EXPERIMENT DESIGN; FLIGHT CONDITIONS; AIRPORTS

• Format: Paperback
• Language: English
• ISBN: 1723721980
• ISBN13: 9781723721984
• Release Date: January 1
• Publisher: Independently Published
• Length: 40 Pages
• Weight: 0.26 lbs.
• Dimensions: 0.1" x 8.5" x 11.0"