DocumentCode :
3598163
Title :
Visual-motion cueing in the control of altitude
Author :
Johnson, Walter W. ; Schroeder, Jeffery A.
Author_Institution :
NASA Ames Res. Center, Moffett Field, CA, USA
Volume :
3
fYear :
1995
Firstpage :
2676
Abstract :
The vertical motion simulator at the NASA Ames Research Center was used to examine how platform motion and visual level-of-detail (LOD) cueing affected altitude repositioning and vertical rate control in two tasks utilizing a simulated AH-64 Apache helicopter. The LOD manipulation caused optical density to change across altitudes by a small, moderate, or large amount. The platform motion manipulation resulted in platform motion being either present, and 1:1 (full), or totally absent. Both small optical density changes and platform motion improved altitude judgements in the altitude repositioning task, while platform motion improved performance in a vertical rate control task. These findings show that: 1) vertical platform motion mitigates the tendency of pilots to mistake optical flow rate (angular visual speed) as proportional to vehicle speed during altitude change, and contributes to the perception of movement amplitude; and 2) maintaining nearly constant optical density across altitudes improves altitude judgements
Keywords :
aerospace simulation; aircraft control; attitude control; human factors; motion estimation; visual perception; AH-64 Apache helicopter; NASA Ames Research Center; altitude control; movement amplitude perception; optical density; optical flow rate; platform motion; vertical rate control; visual level-of-detail cueing; visual-motion cueing; Acceleration; Aerospace simulation; Helicopters; Image motion analysis; Layout; Motion control; NASA; Optical control; Postal services; Technology management;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Systems, Man and Cybernetics, 1995. Intelligent Systems for the 21st Century., IEEE International Conference on
Print_ISBN :
0-7803-2559-1
Type :
conf
DOI :
10.1109/ICSMC.1995.538187
Filename :
538187
Link To Document :
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