Accession Number : AD0857276
Title : Predictor Displays for Low-Altitude High-Speed Flight.
Descriptive Note : Final rept. Jan 66-Apr 68,
Corporate Author : RITCHIE INC DAYTON OH
Personal Author(s) : Williams, W. L.
Report Date : FEB 1969
Pagination or Media Count : 49
Abstract : Three fixed-based simulation studies were conducted to determine the applicability of the predictor display concept to Low Altitude High Speed (LAHS) information display. Only pitch axis information (three degrees of freedom) was considered. Three airspeeds--Mach 0.6, 0.9, and 1.2--were used in all three studies. A preliminary study was conducted to determine appropriate display scale factors. Using a fixed prediction span of 10 seconds, vertical scale factors of 250, 500, and 1,000 ft/cm and horizontal scale factors of 2,000, 4,000, and 6,000 ft/cm were evaluated. A vertical scale of 500 ft/cm and a horizontal scale of 2,000 ft/cm were selected for further studies. The first experimental study compared pilot performance using a predicted flight-path display with pilot performance without a predicted flight-path display. The second experimental study investigated the effect of prediction span on pilot performance. Spans of 0.25 sec, 3.5 sec, and 6.75 sec were evaluated. (Author)
Descriptors : *RECONNAISSANCE AIRCRAFT, *FLIGHT CONTROL SYSTEMS, *TERRAIN AVOIDANCE, *DISPLAY SYSTEMS, LOW ALTITUDE, PREDICTIONS, JET FIGHTERS, FLIGHT SIMULATORS, AVIATION SAFETY, FLIGHT PATHS, PILOTS, PERFORMANCE(HUMAN).
Subject Categories : Attack and Fighter Aircraft
Patrol and Reconnaissance Aircraft
Distribution Statement : APPROVED FOR PUBLIC RELEASE