Accession Number : ADA194602
Title : Improvement of Head-Up Display Standards. Volume 5. Head Up Display ILS (Instrument Landing System) Accuracy Flight Tests.
Descriptive Note : Final rept. 1 Oct 84-15 Jun 87,
Corporate Author : CREW SYSTEMS CONSULTANTS YELLOW SPRINGS OH
Personal Author(s) : Newman, Richard L ; Bailey, Randall E
PDF Url : ADA194602
Report Date : Sep 1987
Pagination or Media Count : 45
Abstract : An in-flight investigation of the effect of head-up display symbol accuracy has been conducted using a variable stability T-33 aircraft. The results indicate that 100-200 ft lateral errors and 500-1500 ft longitudinal errors in locating a contact analog synthetic runway did not cause difficulties for the evaluation pilots. There was no apparent tendency for the subjects to follow HUD cues and ignore real world cues. Keywords: Head up display, Symbology, Instrument, Flight control, Flight tests, Accuracy, Display.
Descriptors : *FLIGHT CONTROL SYSTEMS, *HEAD UP DISPLAYS, *INSTRUMENT LANDINGS, ACCURACY, ANALOG SYSTEMS, FLIGHT TESTING, INFLIGHT, LANDING AIDS, PILOTS, RUNWAYS, STANDARDS, SYMBOLS, TEST METHODS
Subject Categories : Flight Control and Instrumentation
Distribution Statement : APPROVED FOR PUBLIC RELEASE