DocumentCode :
2341220
Title :
Experimental study of helmet-mounted display attitude and flow cues on rotorcraft hover performance
Author :
Bachelder, E.N. ; Hansman, R. John, Jr.
Author_Institution :
Dept. of Aeronaut. & Astronaut., MIT, Cambridge, MA, USA
Volume :
2
fYear :
1997
fDate :
26-30 Oct 1997
Firstpage :
6.3
Abstract :
A study was conducted to investigate the use of visual flow and attitude cues as an aid to lateral drift awareness during helicopter flight while using night vision goggles (NVG´s). Four displays were compared: 1) NVG display: the baseline display simulating an NVG image of the cockpit and external environment; 2) NVG/Attitude display: NVG image with an overlay of an attitude symbol and a surrounding earth-referenced wire-frame globe; 3) Rate display: NVG image with an overlay of a flow cue field; 4) Rate/Attitude display: NVG image with the Rate and NVG/Attitude display overlays. The task objective was to null out lateral rates in the presence of lateral gusts while in a hover (the yaw, longitudinal, and vertical axes of motion were stabilized with an auto-pilot). This task was conducted in a fixed-based helicopter simulator using a helmet-mounted virtual reality device. Three pilots were used in this preliminary study. Cooper Harper subjective ratings (handling qualities) for the aircraft/display combination favored the Rate/Attitude display using an intermediate cube separation, which was consistent with the performance and frequency metric results
Keywords :
aircraft control; aircraft displays; attitude control; helicopters; image sensors; infrared imaging; Attitude display overlays; Cooper Harper subjective ratings; NVG display; Rate display; attitude cues; attitude symbol; earth-referenced wire-frame globe; flow cues; frequency response; helicopter flight; helmet-mounted display; lateral drift awareness; lateral gusts; lateral rates; mean RMS drift rate error; night vision goggles; protocol; rotorcraft hover performance; virtual reality device; visual flow; Attitude control; Degradation; Displays; Eye protection; Feedback loop; Helicopters; Night vision; Space technology; Stability; Virtual reality;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Digital Avionics Systems Conference, 1997. 16th DASC., AIAA/IEEE
Conference_Location :
Irvine, CA
Print_ISBN :
0-7803-4150-3
Type :
conf
DOI :
10.1109/DASC.1997.636188
Filename :
636188
Link To Document :
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